|nasa-cb-17j. 99) cabso i depositi °n i £ i 183-2820q ......phase diagram for nickel-catalyzed...

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|NASA-CB-17J._99) CABSO_i DEPOSITI °N I_ £_i_ 183-2820q, J_OSCH P_OCESS glTbl _OTi-iEblIUlq AMD _UT_iUM-I_O_ ALLOY CAT&LXSTS M.S. _=s_.s. Finai RepoEt, Jan. 1981 - Jul. 1982 gnclas {Massachusetts Inst. oi Tech.) 122 p G J/26 03991 UTILIZATION OF RUTHENIUM AND RUTHENIUM-IRON ALLOYS AS BOSCH PROCESS CATALYSTS by CHARTSIRI SOPHONPANICH B.S., Worcester Polytechnic Institute (1980) ff if: % SUBMITTED TO THE DEPARTMENT OF CHEMICAL ENGINEERING IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE IN CHEMICAL ENGINEERING at the MASSACHUSETTS INSTITUTE 0F TECHNOLOGY December 1982 _) Massachusetts Institute of Technology, 1982 # Signature of Author Certified by Accepted by Department of Chemical Engineering December 27, 1982 Professor Michael P. Manning Thesis SuperviSor ki, / Professor Robert C. Reid Thesis Supervisor ., tilL, _/ _/ _ . Professor Glen C. Williams Chairman, Department Committee

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Page 1: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

|NASA-CB-17J._99) CABSO_i DEPOSITI °N I_ £_i_ 183-2820q,J_OSCH P_OCESS glTbl _OTi-iEblIUlq AMD_UT_iUM-I_O_ ALLOY CAT&LXSTS M.S. _=s_.s.

Finai RepoEt, Jan. 1981 - Jul. 1982 gnclas

{Massachusetts Inst. oi Tech.) 122 p G J/26 03991

UTILIZATION OF RUTHENIUM AND RUTHENIUM-IRON ALLOYSAS BOSCH PROCESS CATALYSTS

by

CHARTSIRI SOPHONPANICH

B.S., Worcester Polytechnic Institute (1980)

ff

if:%

SUBMITTED TO THE DEPARTMENT OF CHEMICAL ENGINEERING

IN PARTIAL FULFILLMENT OF THE REQUIREMENTS

FOR THE DEGREE OF

MASTER OF SCIENCE IN CHEMICAL ENGINEERING

at the

MASSACHUSETTS INSTITUTE 0F TECHNOLOGY

December 1982

_) Massachusetts Institute of Technology, 1982

#

Signature of Author

Certified by

Accepted by

Department of Chemical EngineeringDecember 27, 1982

Professor Michael P. ManningThesis SuperviSor

ki, /Professor Robert C. Reid

Thesis Supervisor

., tilL, _/ _/ _ .Professor Glen C. Williams

Chairman, Department Committee

Page 2: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

ORIGINAL PAGE Ig

OF PoOR QUALITY

UTILIZATION OF RUTHENIUM A_{D RUTHENIUM-IRON ALLOYS

AS BOSCH PROCEZS CATALYSTS

by

CHARTSIR! SOPHONPAN!CH

Submitted to the Department of Chemical Engineering on

December 27, 1982, in partial fulfillment of the requirements

for the Degree of Master of Science inChemical Engineering

at the Massachusetts Institute of Technology

Abstract

The Bosch process has been considered as a means to

recover oxygen from metabolic carbon dioxide through the

catalytic production of water. Previous investigations haveshown that the oxide formation accounts for the limited

activity of the iron catalyst. On the other hand, the maximumwater concentrations achievable in the nickel and cobalt

systems have been shown to correspond to the carbideformation. This thesis presents the results of an experimen-

tal study carried out to determine the effectiveness of

ruthenium and its unsupported alloys with iron -- namelv,

50RuSOFe and 3_Ru67Fe -- as alternative Bosch catalysts.

Carbon deposition boundaries over the unsupported alloys are

reported.Experiments have also been carried out over 50RuSOFe

and 97Ru3Fe catalysts supported on Y-alumina to determine

their performance in the synthesis of low molecular weightolefins. High production of ethylene and propylene would be

beneficial for an improvement of an overall Bosch process, as

a gas phase containing high o]efin content would enhance

carbon deposition in a Bosch reactor.

THESIS SUPERVISORS: Professor Michael P. Manning

Professor Robert C. Reid

Page 3: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

9

_cknow!ed_emen_

ORIGINAL PAG_ ISOF POOR QUALITY

I would like to acknowledge the support of the Nqtion,_!

Aeronautics and Spqce Administration in sponsor in:, this

research, including the assistance of the NASA officer, Dr.

Phillip D. Quattron_. My sincere appreciation is also gra-

ciously extended to Professors Michael P. Manni,'_ and _obert

C,. Reid for their v_luable guidance and expertise. _nd most of

all. their unfailing patience.

Also _cknow! edged is the contributions of Dou_

Borowski. Evnn Morris, Brian Moroney, Br_d ,_,_ckett and ,T_m_s

Willard from their pqrticip_tiou in the 10.26 Chemicn_ En_i-

neerina L_bor,,_tory course. Brad ,qqck_tt and J_mes Will_%rd

further %sz[sted in th_s thesis through their invo!vemeDt in a

URO? projmct. Help wa_ also provided by Rhondq Wilson at the

initial stage of this research as q UROP student.

Special thanks are due to ,Iv colleagues from the

Lab, particularly

Nenniger, Mi ch_,el

Puel

Their freindship, encouragemeat and support were much

Michael Snow and Bhakorn Vanuptiku] provided their

helping me prepare most of the

thesis.

Finally, I would like to

figures presented

encouragement and support they have

education.

needed.

skills

in this

thank my fmmily for their

given me throughout my

Cheng-Shiou Ch_%ng. 9teve Chiu Kin Lai, John

A. Serio, Michael Snow, and William Sun.

Page 4: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

T'_bl_' of Couten+,: -_OF POOR QUALITY

Abstract .................................................... I

Acknowled_ment_ .............. *iIemImattt.IeJt...eoI*ooo''''_

Tgble of Content_ ...........................................

List

List

I.

of FL_ures ............................................. 5

of Tables .............................................. 8

!ntrodu:tion ............................................. g

. Literature

2.1

_

Review ...................................... 16

The Iron System ................................... 16

The Nickel an_ Cobalt $ystemm ..................... 18

Ruthenium nn_ Ruthenium-Iron A_loys ............... 21

o _ I Ruthenium ......................... 21

_ _ Ru_ T A! 26.... ,.._en_urn-_ron Ioy_ ......................

and

Experimentn! Apparatus ...........

_.I.1 Peed-G%s Delivery _y_t@m...

_.I.2 Thermo_ravimetric Resctor.

Procedure ............................... Xl

............... Xl

.............. _I

............... _8

_.I .2.1

X.1 .2.2

Z.I .2.3

x.1 .2.4

3.1 .x Gas

Preheater and bower R,actor

Support Tube ......................... _8

Top Section of Reactor Support Tube..41

Catalyst Assembly .................... 42

Furnace .............................. 42

Samplin_ and Analytical System ........ 44

C_talvot, Preparation ............................. 4q

Experiment R_. Approach ............................ 51

Page 5: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

4

Table of Contents Continu_d_

•Results and Discussion ................................. 55

A.I Results ........................................... 55

4.1.1 Preliminary Experiments .................... 55

4.1.2 Equilibrium _tudies ........................ 56

4.1.2.1 50RuSOFe Alloy ....................... 58

4.1.2.2 33Ru67Fe Alloy ....................... 6_

4.2 Discussion ........................................ 79

4.2.1 Ruthenium .................................. 80

4.2.2 Ruthenium-Iron Alloys ...................... 81

4.2._ Preliminary 9tudy on _ynthesis of

Lower 01efins .............................. 8_

A.2._.I 50RuSOFe 9upported Catalyst .......... 92

4.2._.2 97RuSFe Supported C_t_lyst ........... 96

4.2._._ Secondary Reactions ................. 103

5. Application of the Results ........................... 108

6. Conclusions ......................................... 115

References .................. '.............................. 117

Page 6: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

5

List of Figures

Figure Title Page

1.1

1.2

2.3

3.1

3.2

3.3

3.4

3.5

3.6

3.7

4.1

4.2

Inhibition of Carbon Deposition by _304

at Various 0/H Ratios (8) ........................... 12

Phase Diagram for Nickel-Catalyzed Bosch

Process (9) ......................................... 13

Iron-Ruthenium Phase Diagram (42) ................... 27

Hydrocarbon Selectivity in 3.3 H2/CO at I at_

an_ 573K for Freshly Reduced FeRu Catalysts

as a Function of Bulk Composition (14) .............. 29

Relative Selectivity of FeRu Catalyst to

Unsaturated Products in 3.3 H2/C0 at I atm

and 573K ............................................ 29

Schematic Digram of Experimental System (9) ......... 32

Dry Feed Gas Delivery System

Water Vapor Delivery System

Reactor Assembly in Furnace

(7)....................33

(9).....................37

(7).....................39

Top and Lower Reactor Sections with

Preheaters (7) ...................................... 40

Catalyst Carrier in Support Tube (7) ................ 43

Gas Sampling and Analysis System .................... 46

Carbon Deposition on 50Ru5OFe and 33Eu67Fe

Alloy Catalysts from a H2:C0 (1:1) Mixture .......... 57

Rate of Carbon Deposition as a Function of

AGc for an 0/H Ratio of 0.5 ......................... 59

Page 7: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

OF. POOR QUALITY

List of Figures (Continued]

Figure Title Page

4._

4.4

4.5

4.6

4.7

4.9

4.9

4.10

4.11

4.12

4.13

Rate of Carbon Deposition as a Function of

AG c for an 0/H Ratio of 0.5 ......................... 60

Rate of Carbon Deposition as a Function of

AG for an 0/H Ratio of 0.5 ......................... 61c

Rate of Carbon Deposition as a Function of

AG for an 0/H Ratio of 1.5 ......................... 64c

Rate of CaTbon Deposition as a Function of

_'_ • oo•.oeIO.OooJc for an 0/H Ratio of 1 5 ............. 65

Rate of Carbon Deposition as a Function of

AG for an 0/H Ratio of 1.5 ......................... 66c

Rate of Carbon Deposition as a Function of

uc for an 0/H Ratio of 0.17 ............ 67

Carbon Deposition Boundary for Various 0/H

Ratios over 50Ru5OFe Catalyst ....................... 68

Rate of Carbon Deposition as a Function of

AG c for an 0/H Ratio of 0.5 ......................... 69

Rate of Carbon Deposition as a Function of

AGc for an O/H Ratio of 0.5 ......................... 70

Rate of Carbon Deposition as a Function of

AGc for an O/H Ratio of 0.5 ......................... 71

Rate of Carbon Deposition as a Function of

AG c for an O/H Ratio of 0.5 ......................... 72

Page 8: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

2

i

i

Figure

4.14

4-15

4.16

4.17

4.18

4.19

4.20

4.21

4.22

4.23

4.24

5.1

7

List of Figures (Continued)

Title Page

Rate of Carbon Deposition as a Function of

AG c for an 0/H Ratio of 1.5 ......................... 74

Rate of Carbon Deposition as a Function of

AG c for an 0/H Ratio of 1.5 ......................... 75

Rate of Carbon Deposition as a Function of

AGc for an 0/H Ratio of 1.5 ......................... 76

Carbon Deposition Boundary for O/H Ratios of 0.5

and 1.5 over 33Ru67Fe Catalyst ...................... 77

Schematic Diagram of Experimental System

(CSTR Mode) ......................................... 89

Product Distribution for

Catalyst Distribution for

Overall Reaction Rates of

50Ru50Fe Catalyst

97Ru3Fe Catalyst

97Ru3Fe Catalyst

(43) ..... 93

(43) ..... 94

at

(43) ..... 97

at

V_rious Temperatures an_ H2/C 0 Feed Ratios

Product Distributions over 97Ru3Fe Catalyst

Varying Feed Gas Ratios (43) ........................ 99

Selectivity towards C2 and C 3 Hydrocarbons ......... 100

Schematic Diagram of Experimental System

(Pulse Mode) ....................................... 105

Equilibrium Water Concentration of a Bosch

Reactor for Various Catalyst System ................ 109

Bosch Recycle Reactor (9) .......................... 112

Gas Recycle Ratio for a Bosch Recycle Reactor ...... 114

Page 9: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

S

OF POOR QUALITY

Table

List of Tables

Title Page

2.1

3.1

3.2

3.4

4.1

5.1

Standard Heats of Formation of Metal Oxides (13) .... 23

Feed-Gas Analysis ................................... 34

Gas Chromatograph Operating Conditions .............. 48

Composition of Certified Primary Standard ........... 50

Surface Areas of Unsupported Catalysts .............. 52

Gc as a Function of Temperatures and O/H Ratios

for the 50Ru5OFe and 33Ru67F_ Systems ............... TS

Maximum Water Concentrations and Minimum Recycle

Ratios for Various Bosch Catalysts ................. 111

Page 10: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

9

........... -T<

L

:!

I. Introduction

A reliable regenerative life support system is required

for future long-duration sp_ce missions. An important step in

the life support system is the reduction of metabolic carbon

dioxide to oxygen, the carbon dioxide being concentrated from

ambient spacecraft atmospheric concentrations with an electro-

chemical concentration cell. This regeneration of o_ygen can

be accomplished by several techniques, including the Bosch,

the Sabatier and the Solid-Electrolyte process (I). Of

interest in this investigation is the Bosch process, in which

carbon dioxide reacts catalytically with hydrogen to form

carbon and w_ter, with the carbon depositing on the catalyst.

The w_ter produced is electrolyzed to oxygen and hydrogen, the

latter being recycled to the Bosch reactor. The overall

process can be summarized by the following reactions.

Bosch Reaction: C0 2 + 2H 2 _ C + 2H20(1.1)

Electrolysis: 2H20 . 2H 2 + 02 (I .2)

Overall: CO 2 ÷ C + 0 2(I.3)

Several prototype recycle Bosch reactors have been

investigated by NASA, utilizing ordinary steel wool as the

catalysts (2,3,4). The reactor is typically run in a recFcle

Page 11: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

I0OF POGR ,_,_...,'....

mode in a temperature range of 800-I000K,

efficiencies through the reactor are less

formation of carbon monoxide and methane also

as single pass

than I0_. The

occurs. W_ter

is continuously condensed from the effluent stream, while the

remaining effluent gas is recycled and mixed with the inlet

C02 and H 2.

A major problem associated with the transition

iron catalyst was that the

obtained in the reactor had

expected from thermodynamic

Previous investigations at the Massachusetts Institute of

Technology have shown that the low water yield was related to

the formation of iron oxides, which were noncatalytic to the

carbon deposition (5,6,7,8). The oxidation of the iron

catalyst occurs, in addition to the other reactions taking

_!ace in the gas mixture consisting of hydrogen, carbon

dioxide, carbon monoxi&,_, methane and water.

At T < 860K 3.T_ + 4H20

metal

effluent w_ter concentration

been significantly less than

equilibrium considerations.

Fe304 + 4ff 2 (1.4)

3Fe + 4C02 Fe304 + 4C0 (I .5)

At T > 860K Fe + H20 _ Fe0 + H 2 (I .6)

Fe + C02 _ Fe0 + CO (I .7)

Manning and Reid (6) suggested, with further experimen-

tal confirmation by Sacco and Reid (8), that the Bosch process

Page 12: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

!

11 _ V_j 4- _

OF POOR

should be operated in the carbon depositing region

iron-iron oxide-ga3 equilibrium line in the C-H-O

diagram, as shown in Figure 1.1. The iron catalyst

in a metallic form in this region.

Consequently, in the search for an

catalyst, consideration must be made of the

trations of water or carbon dioxide in

above the

tr iangul ar

would be

alternative Bosch

limiting concen-

the system before

catalyst oxidation occurred. Theoretical calculations for

b_th the nickel and cobalt systems indicated that the inter-

ference of oxide formation would not exist under operating

Bosch gas compositions (9,10). As shown in Figure 1.2 for the

nickel system, the metal-metal oxide-gas equilibrium line was

below the graphite-gas equilibria boundary, and thus no

limitation on carbon depostion in the form of an oxidized

catalyst was to be expected. The experimental investigation

by Garmirian et al. (10) confirmed the above postulate for

both nickel _ and cobalt systems. Their results, however,

showed strong evidence that carbon deposition occurred via a

metal carbide intermediate, with subsequent decomposition to

carbon, in region X of Figure 1.2 and ceased upon reaching the

metal-metal carbide-gas equilibrium line. In region Y, where

the formation of a metal carbide would not be thermodynami-

cally favored, no carbon deposition was observed.

Page 13: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

12ORtGI._t,_.L :_.": ,.,,,OF POOR QUALITY

" " t!

CARBON

TEMPERATURE =800 KPRESSURE =1.00 BAR

A WEIGHT GAIN

8 SLOW WEIGHT GAIN

NO WEIGHT LOSS OR GAIN

CO

CH ,O4

a-Fe,

a-Fe (: 17 HzO 50 t.50

UPPER CURVE: IRON-IRON OXIDE-GAS EQUILIBRIALOWER CURVE: GRAPHITE-GAS EQUILIBRIA

Figure 1.1 Inhibition of Carbon Deposition by Fe304 at

Various O/H ratios (8)

Page 14: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

13

OF PCO_

C or b on

Pressure :I.0

,,, 700 K

------ 800K

At rn

:O

/_ CO_

CH

\

Hydrogen

UPPER CURVEMIDDLE CURVE

LOWER CURVE

H20 Ox ygen

METAL -METAL CARBIDE-GAS EOUILIBRIA

GRAPHITE - GAS EOUILIBR.tA

METAL-METAL OXIDE-GAS EQUILIBRIA

Figure 1.2 Phase Diagram for Nickel-Catalyzed Bosch Process (9)

Page 15: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

14ORIGINAL PAGE IS

OF POOR QUALITY

Studies on iron, nickel and cobalt as catalysts in the

Bosch process have led to the conclusion that the catalyst

performance is limited by the formation of oxides or carbides.

Similar to Fe, Ni and Co, ruthenium (Ru) has been shown to

catalyze reactions between carbon monoxide _nd hydrogen

through dissociative adsorption of carbon monoxide at elevated

temperatures (11). Although ruthenium does form an oxide,

thermodynamic data for the formation of ruthenium oxide (RuO 2)

(12) are such that the metal-metal oxide-gas boundary is

removed from the graphite-gas equilibrium line, as is the case

for nickel an_ cobalt. Consequently, ruthenium oxide is not

expected to form under typical conditions of the Bosch

process. In addition, the carbides of ruthenium have been

reported to be unstable or of very lim!ted stability in

comparison to thc_e of iron, nickel and cobalt (13). Thus, as

the rate of carbon deposition on nick

be limited by the decomposition rate

carbon deposition rate on ruthenium m

faster than that on nickel or cobalt.

and cobalt appears to

metal carbides, the

,_t be expected to be

Interesting results have been reported with the use of

unsupported ruthenium-iron alloys in the investigation of

Fischer-Tropsch reactions (14). High product ratios of

olefinic species to paraffinic compounds have been observed

for the alloy catalysts of intermediate composition. The high

olef!n content is expected to enhance the rate of carbon

deposition on the Ru-Fe alloys, as has been observed for

Page 16: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

15

similar systems by Baker C15).

The above evidence seems

Ru-Fe alloys to be superior to

to indicate ruthenium and

the previously investigated

Bosch catalysts. Hence, a study on ruthenium and Ru-Fe alloys

has been cazried out to determine their effectiveness as

catalysts for the Bosch process.

Page 17: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

16C,F _:<..,".'-<_L;.;,LJTY

2. Literature Review

The Bosch process consists of a complex set of reac-

tions occurring in both parallel and series combinations. The

overall stoichiometry of the process can be represented by the

equation below, where carbon

converted to solid carbon

hydrogen.

C02 + 2H 2

dioxide can be visualized as

and water by the reaction with

C + 2!-I20 (2.1)

The process is catalyzed by transition metals in a temperature

range of 700-IOOOK.

Iron, nickel and cobalt have been investigated in the

Bosch process by Manning (5), Sacco (7) and Garmirian (9).

The results of their studies are summarized below. Following

will then be a review of related studies of ruthenium and

ruthenium-iron alloys, which possess several prominent featu-

res that could lead to promising applications in the Bosch

process.

2.1 The Iron System

The water concentration significantly below that

expected from thermodynamic considerations was observed in the

effluent stream of a NASA prototype Bosch recycle reactor

utilizing an iron catalyst. A thermodynamic analysis and an

experimental study of the iron-catalyzed Bosch process were

Page 18: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

17

carried out by Manning (5) in investigatin-

iron. His study has shown good evidence of

catalyst oxidation in the Bosch process. In

the behavior of

interference of

one experiment,

C0/C02 gas mixtures of different compositions were passed over

an iron wool catalyst at 823K. While no weight

observed for a 50:50 CO:CO2 mixture, a rapid rate

deposition was noted for a 66:34 C0:CO 2 mixture.

tions involved in the

iron,

3Fe + 4C0

experiment include the

chan£e was

of carbon

The reac-

oxidation of

and the disproportionation of carbon monoxide,

2C0 ÷_ C02 + C (2.3)

The CO equilibrium concentrations for the two reactions at

823K are 53 and 13 mole percent, respectively. Based upon

thermodynamic considerations, the disproportionation reaction

should have proceeded to the right, resulting in carbon

deposition. However, with a 50:50 CO:C02 mixture, the oxida-

tion of iron was favored and thus no carbon deposition was

observed. On the other hand, when a C0:C02 mixture of 66:34

was used, iron oxide was converted to its elemental form, at

which point carbon deposition took place.

Further verification of the interference of iron oxides

in the Bosch process was made by Sacco (7). In the determina-

tion of carbon deposition boundaries, equilibrium studies

I employing gas mixtures of H2, CO, CH 4, C02 and H20 were

Fe304 + 4C0 (2.2)

Page 19: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

OF PO_R QUALi_

_n,_ he then de_.re_._,d the C/H r_tto_ at" the inlet R_._ mixt_r_.

The e_rbon depo_ttlon boun,_ry w_:_ 4_termlned by tho point

wher. no e_rbon _positlon be_n. A tYl_te_ _- ex_i)le of hls

exp_rlment_T resul_ts I) mhovn gr_phte,l)_y in )$_&_re I.I. which

a+_on._trntes ,n _xeellent ,greement between the exp_rlment._llY

_eter_tne_ phase boQn4_ry _n.l tb_ theoreile,l Iron-lron

oxl_e-R_ equITtbrtum llne.

Th_ result._ of :_¢co'_ Inve._t_t_on _re very _LAnlft-

c),_nt _u that th_,y pro\'I_e further _v i_len,_ ._upp,_rt In6l

M_nnLn_'._ hyI',_th_:_ ,_ of the inhlbitiv+_ role of Iron oXt,1_._ tn

l,_w w_+,cr ,','u,','utr;*t(,on:_obt,_inod in B,_:_,'h ree.v,-le r.,_:tor._.

in the Iron ox l,_,_tIon inelu,le the

At T _ ,_6,_K

At T _ S60K

xpe. 4C0 2 .* P_.,O 4 + 4C0 (2. r','_

Pc+ ,q_O "* PeO + N 2 (2.65_, MP"

" ?e._ + CO (2,7>

" " Th_ N_,-k,_l sn_1 Cobslt 9vstem,_

pro,-em_ w,_._ ._ub.._r.qu_n:_ly _nrrie,l out by Oarmlrian (cl_ In th_

search for an a_t,ern,_ttv_ Bo._h eat,_ly._t. Like iron, th_

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19OF POOR _;_L_:: :_"'

transition metals nickel and cobalt have been known to cata-

lyze all the reaction systems involved in the Bosch process.

However, a significant difference of these two metals from

iron is that the interference of oxide formation would not

exist under operating Bosch gas compositions. A thermodynamic

analysis indicates that the metal- metal oxide-gas equilibrium

line for either the nickel or cobalt system lies below the

graphite-gas equilibrium boundary in a C-E-0 trian_ular

diagram, such as the one shown in Figure 1.2 for the nickel

catalyzed Bosch process. Although his experimental study

indeed verified the noninterference of catalyst oxidation,

Garmirian (9) observed that there existed a region where the

expected carbon deposition would not occur.

This phenomenon is not unsurprising. For carbon

deposition reactions, the solid phase in equilibrium with the

gas phase can range from B-graphite to a solid phase having a

Gibbs energ_ significantly greater than B-graphite. Dent et

al. (16) and Rostrup-Nielsen (17) carried out equilibrium

studies of the decomposition reactions of both methane and

carbon monoxide over nickel catalysts in the temperature

ranges of 600-1200K and 700-I00OK, respectively. Garmirian

(9) performed Bosch equilibrium studies on nickel and cobalt

catalysts covering temperatures of 700-9OOK. Below certain

temperatures, experimental equilibrium measurements of all

three investigations showed deviation from the calculated

values of equilibrium constants based upon the solid carbon

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2O

phase of 8-graphite. The deviation from the 6-graphite

equilibrium was pronounced at low temperatures. When extra-

polated to lower temperatures, these experimental results were

in good agreement with equilibrium measurements made by

Browning and Emmett (18) in the Ni3C-Ni-CH4-H 2 system in the

temperature range of 500-600K and in the Co2C-Co-CH4-!_2 system

at 460-7201(.

It should be noted that a number of studies

(19,20,21,22) have indicated the metastable existence of both

nickel an_ cobalt carbides at temperatures between 600 and

80OK. In explaining the results of his Bosch equilibrium

studies, Garmirian (9) attributed the difference in Gibbs

energies involving the formation of experimental carbon and

B-graphite to the metal carbide intermediates in the carbon

deposition process. At low temperatures, the formation of

carbide intermediates could occur by reactions such as

4-CH 4 +nMe MenC + 2H2 (2 8)

H 2 + CO + nMe _ Me n + H20 (2.9)4-

2C0 + rime ÷ MenC + CO 2 (2.10)g-

with a subsequent carbide decomposition to free carbon,

÷ C + nMe (2.11)RenC ÷

X-ray diffraction analyses were performed on the used cobalt

catalysts but failed to detect cobalt carbides. It was very

likely that the cobalt carbides decomposed during the cooldown

period after the experiments had been completed, as the

decomposition of Co2c and Co3C has been reported to occur at

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21 OF POOR QUALITY

temperatures in a range of 723-743K and 753-763K, respectively

(22).

2.3 Ruthenium and Ruthenium-Iron Alloys

The investigations on iron, nickel and cobalt as

catalysts in the Bosch process have pointed to two important

features: that at high temperatures the maximum water yield

achievable is confined to graphite-gas equilibria, and that at

low temperatures the catalyst performance is limited by the

formation of oxides or carbides. Consequently, a good Bosch

catalyst should not be oxidized under operating conditions,

nor should carbon deposition reactions be limited by the

decomposition of metal carbides. Thermodynamic considerations

and other experimental studies for closely related reactions

show ruthenium and ruthenium-iron alloys to be of significant

promise as effective Bosch catalysts. Positive indications of

the performance of ruthenium and its alloys with iron are

cited below.

L -

)

oxide.

2.3.1 Ruthenium

As reviewed by Shunk (23), ruthenium does

However, according to thermodynamic data by

fo rm an

Bell and

Tagami (12), interference of the ruthenium oxide (RuO 2)

formation under Bosch operating conditions is not expected.

In other words, the metal-metal oxide-gas boundary is removed

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!

22C,_C_MAE P_C_E TS

OF POOR QUALITY

from the graphite-gas equilibrium line, as is the case for

nickel and cobalt. In addition, the standard heats of forma-

tion of metal oxides shown in Table 2.1 (I 3) indicate that the

ease of reduction of metal oxides should be in the order of

Ru, Co, Ni and Fe, with ruthenium being the easiest to reduce.

Although definite verification of ruthenium carbides is

yet to be confirmed (23), the carbides, if they exist, have

been reported to be unstable or of very limited stability as

compared to those of iron, nickel and cobalt (13).

Consequently, if carbon deposition on ruthenium occurs by way

of the decomposition of metal carbide

been postulated for the nickel and

intermediates, as has

cobalt systems, carbon

deposition on ruthenium in the Bosch process would then be

expected to proceed until approaching the graphite-gas equili-

brium boundary.

Carbon deposition on ruthenium has been observed in a

number of investigations (11,24,25,26). Singh _,:_ Grenga (24)

studied the catalytic decomposition of carbon monoxide on

single crystalline ruthenium at 823K and 760 Torr for times

varying from 6 to 96 hours. Reflection high energy electron

diffraction (RHEED) was used to identify the solid products nf

the decomposition reaction. It was found that carbon monoxide

had decomposed catalytically to produce graphite, which

deposited very slowly at low- index poles of the unsupported

ruthenium crystalline surface. Neither oxides nor carbides

were observed.

Page 24: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

2_OF POOR QUALITY

Table 2.1 Standard Heats of Formation of Metal Oxides (13)

Standard Heats of Formation ( -_lJ/_)" of Select Oxides and Sulfides

Oxkka

Oai_a

_lfala

Oxides

,_1_1_

Ozidcs

Sulfides

TiO 123._' VO 103.2"

"rio, 112.4" VaO, 98.1" CrzO_ 90*TiS 78.8" Cr$ 46.7'

TiSa 64'

7-'Oz 130.8" NbO 9r MoOj 70.4"

NbO, 94._ MoOj 60.P

ZrSa 84.4* NbSz 51.8" MoS: 48.3"

WO, 70.5"WO, 66 9*HfOj 133" Ta2Os 97.7*

La:O 3 143.2"

La:S_ 112.7_

LaS 2 89.9'

TaS, 57.7" WS, 46"

AI:O) 133.4' SiO_ M.YAS=S, 73"

MnO 92._' FeO 63.2"MayO, 8Z'P Fe,O, 65._MnS 66.4* Fe$ 39.4*

M_ a 42.1 FeS s 35._F

Tc

ReO z' 51"

CoO $7.1"Co30, 51.0'cos. _0.rCoSz 33.1"

RhO 22"

iluOn 36" lib,O, 22.11"RuS M._* PdS 32.3"

RuS z 40" itbzS , 36._' - PdSj 24ff

irzO, 227*

IrOz 26.$"OrS 40.9d irzS, 32.1" PtS 35.3*

Or_, 33.0' ' ira, 31.3" PtS a 23.6"

ReO, 45.7 ° OsOj 31b

ReS a 36.8"

NiO _ ;./ CuO 37.1"

Cu:O 39.8"Ni$ 3"7.9' CeS 27.9"

NO 22.9" AI_O 72"

._,S 27

A%O, 0.3"

"6 in kcal (gm atom nonmetal)" _ at 298°K.t Samsonov (1973L• Mills (1974).

• McDonald (1962).* Se.arcy (1970).

Standard Heats of Formation (- AH o), of Select Nitrides and Carbides _

INStr.;Lie_, TiN 80.4 VN 52 CraN 27.3 Mn,,N 30.S

Carbides TiC 4_.1 VCp 24.5 • C%C z 2.8 MnsC 4

Nitrid_ ZrN 87.3 NbN 57 M%N 16.6 TcCarbides ZrC.9_ 47.0 NbC 33.6 MoC _3

Hitrides l:.fN 88.2 TaN 59 Low stab. UnstableCarbides |ifC.est -_0.1 TaC 34.1 WC 97 Unstable

Nit,ides LaN 71

Fe, N 3 Co,N -2 Ni_N 0Fe_C -$ Co,C -4 Ni_C --9

Unstable Unstable UnstableLow Stab. Unstable Unstable

Unstable Unstable UnstableUnstable Unstable Unstable

C%N - 18Unstable

UnstableUnstable

UnstableUnstable

•&He" in kcal {gm atom nonmetal}" t at 298°K._' Data from $carcy (1970).

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24

ORIG!NAL PAGE IS

OF POOR QUALITY

Carbon deposition on silica-supported ruthenium has

also been reported by Rabo et al. (11) in their investigation

of the reaction mechanism involved in hydrocarbon synthesis.

Pulses of carbon monoxide were introduced over the catalyst

surface at temperatures ranging from 296K to 573K, followed by

hydrogen pulses at various temperatures. Effluent streams

were analyzed by gas chromatography- The adsorption of C02 on

ruthenium at 573K was shown to be largely dissociative,

resulting in CO disproportionation to CO and surface carbon,

the species which was readily hydrogenated even at room

temperature. The degree of CO disproportionation increased

when the reaction temperature was raised to 673K. At room

temperature, however, disproportionation of CO was absent and

the adsorbed CO was inert to H 2. Ni, Co and Pd supported on

silica gel were also used in the study, and the adsorption

behavior of the first two supported metals was shown to be

very similar to that of Ru. In contrast, the adsorption of

carbon monoxide on Pd at 573K was found to be nondissociative,

and the chemisorbed CO was less reactive to H 2 than the

surface carbon species formed on Ni, Co or Ru.

The temperature-programmed desorption (TPD) of CO and

temperature- programmed reaction (TPR) of chemisorbed CO in _2

has been studied on a Ru/A1203 catalyst by Low and Bell (25).

The investigation was aimed at identifying

present on Ru, the conditions under which

tion takes place, and the reactivity of

the forms of CO

CO disproportiona-

the surface carbon

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25OF POOR QU._LiTY

formed. Carbon monoxide was shown to-be molecularly adsorbed

at 303K to produce methane and ethane. The following reaction

sequence has been proposed for carbon deposition on the

surface of ruthenium (25,26).

CO + S ÷_ CO s (2.12)

CO s + S _ C s + 0s (2.13)

0 s + CO $ CO 2 + S (2.14)

Low and Bell (25) and Ekerdt and Bell (26) have noted the

importance of CO 2 formation of the last reaction in shifting

the balance of the highly endothermic reaction (2.13) toward

carbon deposition. When H2 is present in addition to CO, the

removal of surface oxygen is further enhanced, as shown by the

following reaction.

0s + H2 _ H20 + S (2.15)

In their study of hydrocarbon synthesis from CO and H 2 over

silica-supported ruthenium, Eke,'_t and Bell (26) have reported

that the amount of carbon _ _posited on the ruthenium

catalyst at 464K was an order of _agnitude higher when both CO

and H 2 were present together than when CO was used alone. In

addition, the amount of carbon deposited was shown to increase

with the reaction temperature. Consequently, as the stoi-

chiometric ratio of O/H for the Bosch process is normally kept

at 0.5, equivalent to a H2/C0 ratio of 1.0, and since opera-

ting temperatures of the Bosch process are in the range of

700-900K, several hundred degrees higher than the

Fischer-Tropsch temperatures, the results for a ruthenium

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26

OR:G_', ,-" ...........OF POOR QLi_L |'i=Y

catalyst in

interesting.

the Bosch process are expected to be very

2.5.2 Ruthenium-Iron Alloys

The phase diagram of ruthenium-iron binary alloys is

shown in Figure 2.1. As can be seen from the phase diagram,

for temperatures below 773K ruthenium and iron form a continu-

ous series of solid solutions in the region ranging from 23.5

to 100 atomic percent of ruthenium, with Fe atoms substituted

into the hcp Ru lattice. A two-phase region exists between

4.8 and 23.5% Ru. Below 4.8g Ru, solid solutions are formed,

with Ru atoms substituted into the bcc crystal structure of

Fe.

Recent Fischer-Tropsch studi:;s of ruthenium-iron alloys

by Ott et al. (14) and Vannice et al. (27) have indicated

potential applications of these alloys to the Bosch process.

In the investigation of CO hydrogenation, 0tt et al. (14) used

unsupported RuFe powders prepared from th_ hydrazine reduction

of aqueous salt mixtures, the alloy powders having the surface

areas of 7-10 m2/g. A gas mixture of 3.3 H2/CO was applied at

I atm and 573K over the alloy catalysts having atomic composi-

tions of 97RuSFe, 75Ru25Fe and 33Ru67Fe. Differential kinetic

measurements were made over the alloy catalysts, and the

results were compared with those of unsupported Ru and Fe

metals. A spectrum of carbon-containing species ranging from

2 and methane through C4 hydrocarbons were observed, as

! °

Page 28: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

I

27

OF pOSR F",,:....

IO 80 IO 40

UI_MT P[m (|i_ IUTMI_IUU

SO GO 70 O0 O0

1400

tl40

lifO0 -- " • *

....4...8000 I " lYltfO!tlJO II-Pel i IO l

OoI nU¥_ilil IUIIliD©

810©

_. _l_._ _"_- _'"

0400

1

" //IIOC -- IY- FoIwo,,

CO0©

.._ / /

..°\\/ rS_

lls4| DI

"°° t I,o. (ill *Fit

,. I ]• I0 IO

h

IIv! ,

i

I0 40 IO IO 1tO OO IO IO0

ATOII¢ Pl! ¢ilT |_IN|ilUl |w

Fe.-Ru

Fi@ure 2.1 Iron-Ruthenium ?base Dia@ram (42)

Page 29: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

,% OF POOR QUALIFY

to r_th_nI_m, %h_

tow_rd¢ h_hCr

Oft o_ '_. _14 _ _I._,_ p_rt'orm_,_

Page 30: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

29

OF POOR QUALFrY

Figure 2.2

A

::kSr._ J _C,

O.o_4 CZ%0_

O. --O. 0 0.2 0.4 O.S O.ll IO

Melee Irrlll:11O m Ire I_ file Julk

Hvdrc_csrbon selrcti.ity in 3.3Hi/CO st ! stm sud 573 K lOT ireshly reduced i:'eRu

cs_slysLSS._s funclion of bulk composition. C. i-dicsttMJ Dumber of carbon atoms in the produc:

mo]t.cul_(14)

Figure 2.3

IO

O.i

06

Re;,

R c_*Rc;

0.4

0.1

O.tt I 1 I0.O 0.2 0.4 O&

liiol@ FtlIcllllll FII Ol_ tlIMI JvIJl

1 J

O.8 i.o

Relsti_e selectivity of FeRu cstslyets to uns,tursted producta ie 3.3H,/CO st ) slm

tad s73 K. (14)

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3O

ORIGINAL PA_}_ _

OF POOR QUALITY

lengthened residence time of carbon intermediates would thus

account for an increase in the production of unsaturated

higher hydrocarbons, namely ethylene and propylene.

High olefin yields have also been reported for

silica-supported RuFe Fischer-Tropsch catalysts (27).

However, selectivities of these catalysts towards olefins are

not as high as those of unsupported RuFe alloys, thus sugges-

ting the influence of support interaction and metal particle

size on reaction products (14).

The prominently high olefin yields in CO hydrogenation

over RuFe alloy catalysts could have several beneficial

effects in their applications to the Bosch process. The high

production of olefinic compounds indicates that carbon deposi-

tion on the alloy would be enhanced when the system is opera-

ted at high temperatures. In other words, the appearance of

significant amounts of ethylene and propylene in the hydrocar-

bon synthesis i_ undoubtedly a kinetic rather than an equili-

brium phenomenon. Consequently, in approaching the equili-

brium state of the system, the rate of carbon deposition from

a gas phase containing olefins, rather than paraffins, would

expectedly be enhanced, as has been observed for similar

systems by Baker (15). This enhancement of carbon deposition

activity coupled with the low temperatare synthesis activity

of a ruthenium- iron catalyst is expected to lead to an

improved catalyst for the Bosch process.

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5. Apparatus and Procedure

3.1 Experimental Appara tusl

Figure 5.1 shows a block diagram of the

system. It consists of three basic elements: the

delivery system, the thermogravimetric reactor, and

analytical system. Details of each section are

below.

experimental

feed-gas

the gas

described

were

compositions. If required, water was then added to the

mixture as steam before the feed was sent to the reactor.

requisite rate of steam w_s produced by metering liquid

5.1.1 Feed-Gas Delivery System

In the feed-gas delivery system, chemically pure gases

individually metered and mixed to give desired dry gas

gas

dry reactant

It consisted of

and vaporizing it.

The delivery system of

schematically in Figure 3.2.

cylinders, two-stage gas regulators, and

systems which included mass flow regulators,

The

w_ter

gases is shown

a set of gas

flow controlling

capillary tubes

and U-tube manometers. Table 5.I lists suppliers and purities

of reactant gases used in this experimental study. The

I. The original apparatus was designed and built by Manning(5),with further improvement made by Sacco(7) and Garmirian(9).

Minor modifications were also made in this study.

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I

32

J

Carrier

Gas

Precision

Temp_ratur e

Controller

Analytical

Balance

Gas

Chromoto -

graph _i

- i

I °n_ IllntegrotOrJ

J Water System

Capillary

- Fiowmeter

"_"_ M a s s Flow

Regulator

co co_

Gas Cylinders

m

H 2

l Dessicant

?ower

Figure 3.1 Schematic Diagram of Experimental System (9)

nnmmmmm m |iJii

Sampl_

Valve

System

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OF POOR QJ;_.i'_"Y

I

o o

v

c_

od

im

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34

OF PO0_ Q_.-':_ J '

Table 3.1 Feed-Gas Analysis

Gas Supplier CO 2 02 N 2 Dew Point

AircoHydrogen

(Prepurified

Grade)

Methane Matheson

(CP Grade)

Carbon Dioxide Matheson

(Bone Dry Grade)

0.2

mole

99.95

mole %

< 2O

ppm

O.OO5

mole

0.05

mole %

213.6K

23S.6K

Carbon Monoxide

(CP Grade)

Matheson 50

ppm

600

ppm

1500

ppm

Helium Ai rco I

(High Purity ppmGrade)

I

ppm

14

ppm

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35OF POOR QUALITY

upstream pressure of each gas component was maintained at 3.45

x 105 N/m 2 (50 psig) by the two-stage regulators. The gases

were individually fed to Brooks Model 8944 mass flow regula-

tors equipped with digital settings and inlet line filters

capable of removing entrained particles larger than 2 m. The

gases then passed through 91.5-cm precision bore capillary

tubes with capillary diameters between 1.0 and 1.4 mm

(tolerance of capillary diameter:+ 0.0007 mm). The pressure

drops across the tubes were measured by U-tube manometers

filled with Meriam high vacuum indicating fluid (density: 1.04

g/cm3). The capillary tubes were calibrated for gas flow

rates using soap film flow meters. As would be expected, a

linear relationship between flow rate and pressure drop was

observed, since the capillary tubes used for each gas were

selected so that the flow in the capillary tubes would remain

laminar for experimental flow rates anticipated. This pheno-

menon was in accordance with the Poiseuille's Law, stating

that the gas flow r_te is directly proportional to the pres-

sure drop for laminar flow, as shown mathematically in the

following equation.

where

Q ..

Q =

d =

AP =

=

L =

(w d4 AP)/(128_ L)

volumetric flow rate

capillary diameter

pressure drop across the capillary tube

gas viscosity

capillary length

(3.1)

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36C_INAL PAGE 19

OF POOR QUALITY

The gases exiting the capillary tubes were mixed and

dried in a Kimax U-tube packed with indicating silica gel

dessicant. At this point the gas mixture could either be fed

to the reactor, with or without steam added, or diverted to

the vent.

The water vapor delivery system is shown in Figure 3.3.

The desired rate of steam flow was produced by metering liquid

water and vaporizing it. A l-liter cylindrical water reser-

voir was pressurized at 2.07 N/m 2 (30 psig). The water flow

rate was controlled by a Nupro bellow metering valve. A

precision bore capillary tube with an i.d. of 0.2 mm, in

combination with a mercury manometer, allowed the calibration

of the flow system. A 15-_m filter was installed to prevent

the blocking of the capillary tube. The metered water flow

was then fed to the vaporizer made from a 0.4-m length of 0.64

cm (I/4 inch) stainless stee_ tubing. The tube was packed

with O.5-mm borosilicate bea_ to enhance heat transfer, and

Nichrome wire served as the ating element. The wire was

wound between two layers of _lectrically insulating Sauereisen

cement, which was coated on the external surface of the

tubing. The power input to the Nichrome wire was controlled

by a Variac.

The steam exiting the vaporizer was then fed to a 1-m

length of 0.64 cm (I/4 inch) stainless steel tubing, which

I served to eliminate any surges in the water vapor line. The

tubing was wrapped with Briskeat heating tapes and insulated

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_7C'__r_._'-_ F._,.._¸OF POOR _._'_;-,_u'

t,.

i .N "o

0 t.. LL

,> 3>,

;; Eo_o T c

;E :: _ ;E£°_[l_° !! "

X._. -- u

0 _,

E

O}

¢:)3

f..,Q)

e-4

t.,0

p-

L.

L..

g

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_- ,_, _ '._.. 'L_._' , ,

with a Kaowool blanket. Like the vaporizer, the heated line

was maintained at approximately 400K. Provisions were made at

the end of the tubing so that the steam could either be added

to the dry gas mixture before delivery to the reactor, or be

bypassed to the atmosphere.

3.1.2 Thermogravimetric Reactor

The thermogravimetric reactor and

components consisted of the following: lower

its supporting

reactor support

tube, the top section of the reactor support tube, the catal-

yst assembly, and the heating furnace. A basic configuration

of the reactor assembly is shown in Eigure 3.4. Entering the

inlet tube, the gas mixture from the feed preparation section

passed through the helical preheating coil to the base of the

reactor support tube. The gas mixture then flowed upwar_ over

the catalyst, leaving the system by way of either the weighing

port or the sample line. Details of each reactor part are

provided below.

3.1.2.1 Preheater and Lower Reactor Support Tube

Figure 3.5 features the preheater and both the lower

and upper sections of the reactor support tube. The preheater

and the lower reactor support tube served as the base of the

quartz reactor. The preheater was constructed from a 6-m

length of 7-mm o.d. quartz tubing closely wound into a helical

coil of 60 mm in diameter. The base of the preheater termina-

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!

GRCGLASSJOINT

39

e_ q el

OF POOR (_L;_LiTY

QUARTZ TUBE SUSPENSION "T"

f WEIGHING PORT

/-

SAMPLE LINE

INLET GASES

ATALYST ASSEMBLE

HEATER COIL

FIRE BRICK

REACTOR SUPPORT TUBE

ASBESTOS BOARD

TRANS ITE

rtERMOCOUPLE WELL

Figure 3.4 Reactor Assembly in Furnace (7)

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!:"

4O

EXHAUST_

PORT

34/45 GROUND GLASS

JOINTI

JOINT

(CATALYST SUPPORT) _,,,_

OOOOOOOOOOOOOOOOOO

WEIGHING PORT

TOP SECTION REACTORSUPPORT TUBE

_ SAMPLE LINE

INLET GAS STREAM

0

o/_

/o000

i 00

PREHEATER COIL

LOWER REACTORSUPPORT TUBE

THERMOCOUPLE WELL

Figure 3.5 Top and Lower Reactor Sections with Preheater (7)

Page 42: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

41ORIGINAL P:'_j_ _."

OF POOR QUALITY

ted in the lower reactor support tube, a 2B-am o.d. quartz

tube of 28 cm in height, mounted concentrically with the

preheater coil. Also provided at the base of the support tube

was a 110-mm quartz thermocouple gell, which housed a two-

hole Alundum thermocouple sheath

(type K) thermocouples. A 34/45

joint was attached to the upper

holding two

tapered male ground

end of the lower

support tube. In addition, on the inside wall of the

support tube, a 19/_8 inner ground glass Joint w_s

upw%rd to support the catalyst assembly•

chromel-alumel

glass

reactor

reactor

mounted

Z I 2 o Top Section of Reactor Support Tube

In addition to supporting the reactor within the

furnace, the top reactor section w_ designed to allow the

s_mpling and exhausting of outlet gases, and to facilitate the

weighing of the catalyst sample. The

consisted of a 2_-mm i.d. quartz tube,

fitted with a female 34/45 ground glass

end, which Joined with the lower

upper support tube

15.2 cm in height,

Joint on its lower

reactor support tube.

reactor

as a

were

One

Connected concentrically on the upper end of this top

support tube was a 8-mm i.d. quartz tube, which served

weighing port. Two additional 8-mm i.d. quartz tubes

mounted perpendicularly to the support tube centerline•

of these extensions was sealed and served only to hold the top

reactor section in place; the other was connected to the gas

sampling line for the analysis of outlet gases.

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42

OF POOR O__.',_'"'r

3.1.2._ Catalyst Assembly

Illustrated in Figure _.6 is the catalyst assembly in

the reactor support tube. The catalyst was held in place

between plugs of quartz wool inside the catalyst carrier,

which was constructed out of a 20-mm i.d. quartz tube, 120 mm

in length, with one end fitted with a 19/38 female tapered

ground glass joint. This joint allowed the reactor carrier to

be connected to the lower reactor support tube, thus permit-

ting the gas mixture from the preheating coil to pass over the

catalyst. Attached concentrically to the top of the catalyst

carrier was a quartz rod, _ mm in diameter and approximately

25 cm in length. The quartz rod allowed weight measurements

to be taken by periodically suspending it from an overhead

Sartorius balance, sensitive to an accuracy of ± I rag.

_.I.2.4 Furnace

As shown in Figure 5.4, all the reactor units described

above were housed in a heating furnace. The central component

of the furnace was the cylindrical heating surface, consisting

of two Thermcraft Model RH254 semicylindrical ceramic heating

elements which formed a heated cavity 75 mm in diameter and

30.5 cm in length. Capable of delivering a maximum power

output of 2300 watts, these heating elements were wired in

parallel to a 220-volt electrical line. The reactor tempera-

ture was controlled by a Thermolyne Dubuque III solid state

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43

QUARTZ TUBE

SUSPENSION "T"

CATALYST CARRIER

CATALYST

120 mmQUARTZ WOOL

19/38 5"GROUND GLASS

JOINT

NOT TO SCALE

REACTOR SUPPORT

TUBE

Figure 3.6 Catalyst Carrier in Support Tube (7)

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l•!!

44ORIGINAL PP.(_E 19

OF POOR QUALITY

proportional controller. The sensor of the temperature

controller was an Omega Inconel sheathed chromel-alumel

thermocouple located directly below the catalyst assembly in

the quartz thermocouple well. A similar thermocouple, also in

the thermocouple well, was connected to an Omega Engineering

200 digital pyrometer, thus allowing a continuous monitor of

the reactor temperature.

The ceramic heating elements were enclosed by Babcock

and Wilcox Type K-30 insulating firebrick, forming a square

structure about the cylindrical heaters. The firebrick was

further enclosed by an asbestos board, 6.5 mm thick, and the

entire furnace was structurally supported by a layer of 6.5-mm

thick Transite, an asbestos-concrete composite.

3.1.3 Gas Sampling and Analytical System

Designed to determine the compositions of inlet and

outlet gas mixtures, the data acquisition system included two

basic components: a gas sampling s_stem and an on-line

Hewlett-Packard Model 700 gas chromatograph equipped with a

thermal conductivity detector.

Housed in the gas chromatograph oven, the gas sampling

system consisted of a Hewlett-Packard Model 19020 sample valve

equipped with 0.25-ml s_mple loops, a series of four toggle

shut-off valves for different choices of gas sampling, and a

toggle valve connected to a vacuum system allowing for the

evacuation of sample loops and the drawing of gas samples. A

Page 46: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

}

!

45

ORIGINAL PACE _3

OF POOR QUALITY

representation of the gas sampling system is shown schemati-

cally in Figure 3.7.

During normal operation, a vacuum would be drawn on the

sample valve system. Consequently, with the desired toggle

valve open, the sample loop was flushed with a sample gas.

When the vacuum toggle valve was closed, the sample gas

continued to flow into the system until the pressure in the

sample loop equaled the barometric pressure. The sample

injection into the gas chromatograph then followed. The

sample loop pressure was determined by using a U-tube mercury

manometer, one leg of which was open to the atmosphere.

The analysis of gas samples was accomplished by a

series of GC columns packed with Porapak QS (mesh 50/80) and

molecular sieve 5A (mesh 50/60). (Refer to Figure 3.7.) A

Carle Model 2014 micro-volume valve allowed the gas sample to

be directed, for further separation, to either a Porapak QS or

a molecular sieve 5A column. In a normal analyst _ for a gas

mixture of H 2, CO, CH 4, CO 2 and H20, the Carle micro-volume

valve was positioned such that the gas mixture would flow

through both the 5.O-m and the 2.0-m Porapak QS columns.

However, periodic checking for a possible air leak into the

thermogravimetric reactor was desirable. As carbon monoxide

and air could not be separated by a Porapak QS column at

ambient temperature or above, the analysis was carried out by

a series of the 5.0-m Porapak QS column and the 2.O-m molecu-

lar sieve 5A column. The former separated the gas components

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ORIG]NAL: P'_.A_ i3

"_ OF POOR Q'J._'_ ; ,'

..... I- ._Z__:..,I,'__ .__ I ........... _>/_O_ /

" / _° / !oo

I ._oL..... L.L._ I _ ==

_&, _. _ _!_

"_'i "g

! _E. ,2" i oi '_i ! "

• __

• I,, ,11.4 I _ I _'_' I I::

I-I _:> I ""9 _

/\

A

l',4

Ill III

I_ I.II1 II1

I.I I.tI.I 1.4I_ III

IIIP-, Xttl

Z0

/_'r _'__/i _

=:T:',1"_'

:. I o

iiiiiiI

I

I

iiiiIi

J_ o m ....

"1

iiiIIiI

iI

"1

%1

Illr_

I0iii

ID

I,-i

Ii.,

Page 48: |NASA-CB-17J. 99) CABSO i DEPOSITI °N I £ i 183-2820q ......Phase Diagram for Nickel-Catalyzed Bosch Process (9) ..... 13 Iron-Ruthenium Phase Diagram (42) ..... 27 Hydrocarbon Selectivity

T

47OF PCOR QU,_..._I

into the following sequence: H2, CO and air, CH4, C02 and H20.

Separation of light gases up to methane was further accom-

plished at ambient temperature by the molecular sieve

housed outside the GC oven. As carbon dioxide and water

hazardous to the M5A column, a valve switching was made at an

appropriate time to divert these two remaining gas components

to the 2.0-m Porapak column.

To reduce the severe tailing of a w_ter peak,

Teflon-coated stainless steel tubing was used for GC columns,

as suggested by Hollis and Hayes (28).

stainless steel tubing with no Teflon

with heating tapes.

column

were

The sample loops and

coating were wrapped

A major effort was put forth to obtain good gas analy-

tical results. Optimization was made concerning gas flow

rates, oven and detector temperatures, column lengths as well

as integrating parameters used in an Autolab Model 6300

digital integrator. Ch matograph operating conditions are

shown in Table 3.2.

The Autolab digiial integrator was used in conjunction

with a Honeywell chromatograph recorder to give a quantitative

as well as a visual record of all samples analyzed. An

external standard was used to determine response factors of

the thermal conductivity detector for the five gas components.

These results were then used to calculate component

compositions, except for H2, by the procedure described by Dal

Nogare and Juvet (29). For the determination of hydrogen

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48OF POOR QUALITY

Table _.2 G_s Chromatograph Operating Conditions

Filaments

Sample Size

Carrier Gas Flow Ra_2

Column Operating Temperature

Detector Operating Temperature

Detector Filament Current

GOW-MAC Rhenium Tungsten

Code 13.002 (wx)

0.25 cc

35 cc/min

418 K

473 K

200 mA

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49OF POOR QUALITY

content, the method recommended by Purcell and Ettre (30) was

applied. Direct measurement of hydrogen was made possible as

the result of using a special gas mixture of 91.5% He and 8.5%

H 2 supplied by Matheson Gas Products.

Three standards typically used in calibrating the

thermal conductivity detector were: (I) pure hydrogen, (2) a

certified primary gas standard containing a mixture of

hydrogen, carbon monoxide, methane and carbon dioxide (see

Table 3.3), and (3) a gas mixture of known water vapor content.

The raw data obtained from the GC

alyzed using a modified computer program

originally developed by Manning (5).

analysis were an-

for data reduction

3.2 Catalyst Preparation

The unsupported

ruthenium metal and Ru-Fe alloys. These were

precipitation method, wherein an aqueous

(RuC13/FeC12) solution of the predetermined

chemically reduced by sodium borohydride I (51).

a salt solution of 0.1-0.2 M was prepared and

catalysts under investigation were

prepared by a

metal chloride

composition was

Specifically,

added to an

I • Anhydrous iron (III) chloride and sodium tetraborohydride

(98%) were supplied by Alfa Products, a Ventron division.

Anhydrous ruthenium (III) chloride was supplied byStrem Chemicals.

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5O _.: POOR QUALITY

Table 3. Composition of Certified Primary Standard

G_s

Mole Percent

Hydrogen

Carbon Monoxide

Carbon Dioxide

Methane

Ethylene

Propy!ene

22.10 -+ 0.02

25.00 -+ 0.O2

25.03 +- 0.02

Balance

1.95 +- 0.02

2.00 -+ 0.02

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OF POOR QU_LII"Y

51

excess amount of reducing N_BH 4 solution.

instantly reduced with the formation of

divided solid. The solid precipitate was

The salt was

a black, finely

filtered, w_shed

several times with distilled water, and air dried.

sample was then treated overnight at 773K under

atmosphere, to increase crystal size and to remove

the chlorides.

Three types of unsupported catalysts were

the method described above. They were pure

The solid

a hydrogen

traces of

prepared by

ruthenium,

50Ru5OFe (atomic Ru:Fe = 1:1) and 33Ru67Fe (atomic Ru:Fe =

1:2). X-ray diffraction analysis was performed on the samples

to confirm the formation of the expected alloy catalysts. The

surface areas of activated samples were determined by the

BET/N 2 method using a Quantasorb sorption system. The results

are shown in Table 3.4.

3.3 Experimental Approach

Although represented stoichiometrically by the overall

reaction (1.3), the Bosch process consists of a complex set of

reactions, involving not only the gas phase reactions among

the five major components -- hydrogen, carbon monoxide,

methane, carbon dioxide and water -- but also the gas-solid

interactions. As discussed earlier, the latter includes, for

instance, oxidation of the metal as in the case of

iron-catalyzed Bosch equilibrium studies and carbide formation

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!

52

ORIGINAL P_,CE _S

OF POOR QUALITY

Table z.4 Surface Areas of Unsupported Catalysts

SampleSurface Area (m2/g _

Rs

50£u5OFe

X3Ru67Fe

V.O7

I .83

5.69

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53OF poOR q _'L_'(?

as in the nicke_ and cobalt systems. These

interactions have been found to account for the

water yield lower than predicted from the

gas-catalyst

experimental

gas-graphite

equilibrium. The objectives of this investigation have been

to evaluate the effectiveness of Ru and Ru-Fe alloys as Bosch

catalysts. This is tantamount to the determination of carbon

deposition boundary lines for these proposed catalysts.

Results from previous investigations (9,10,16,17,18)

have pointed out the necessity to account for the possible

existence of a different form of carbon other than E-graphite

in determining the carbon deposition equilibrium boundarF.

The approach taken in this Bosch equilibrium study was similar

to the one used by Garmirian (9)- AG c was defined as the

difference in the Gibbs energy changes involving the formation

of experimental carbon and B-graphite as illustrated below.

AG c AGexperimental carbon - AG__graphit e

-RT In Kpexperimenta I carbon

+ RT In K

P_-graphite

Based upon phase rule considerations, the determination of gas

equilibrium compositions can be accomplished as follows. For

a given temperature, pressure and gas phase 0/H ratio, any

three independent reactions can be chosen, one being a carbon

desorption reaction. Three such reactions and their equili-

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54

OF POOR QUAL|TY

brium constants are shown below.

PH20Pco (3.3)

H 2 + C02 _ CO + H20 Kpl Pco2PH2

PCH4PH20 (3.4)3H 2 + CO ÷ CH 4 + H20 Kp2 =

Pc0PH2_

2

CH 4 C + 2H 2 PH2 (3.5)

Kp3 = PCH4

By allowing the equilibrium constant of reaction (3-5) to vary

as

(3.6)

each gas component were then set

values of AG c. A computer program

determination of run conditions.

accordingly for desired

was developed for the

Kp3 = KP3_.graphite exp (-AGc/RT)

to account for the possibility of the formation of experimen-

tal carbon other than B-graphite, equilibri&m gas compositions

were then determined for a given temperature, pressure and gas

phase 0/H ratio, thus varying the values of the parameter AG c

from -10.0 kcal/mole to +10.O kcal/mole. The flow rates of

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55 OE POOR _UAL;_qf

4. Results and Discussion

4. I Results

Two types of experiments were performed on the ru-

thenium catalyst and the two Ru-Fe alloyJ. The first type was

carried out to see whether the powder samples catalyzed the

Bosch reaction, which results in carbon deposition on the

samples. The other experiments were the equilibrium studies,

from which carbon deposition boundaries were determined.

4.1.1 Preliminary Experiments

To determine the catalytic activities of unsupported

ruthenium and Ru-Fe alloys toward carbon deposition, a gas

mixture of hydrogen and carbon monoxide w_s employed. Perio-

dic weight measurements were made to monitor the extent of

carbon deposition as a function of time. For the ruthenium

catalyst, no carbon deposition was observed. In one instance,

a gas mixture of equimolar H 2 and CO was passed over 0.19972

grams of the unsupported ruthenium catalyst at the flow rate

of 20 cc/s (STP) and at the temperature of 8OOK for 2 3/4

hours; no change in the weight of the catalyst was noted.

However, in the analysis of outlet gas compositions small

amounts of methane and carbon dioxide (<1.O mole percent) were

found. The detection of CH 4 and CO 2 w_s indicative that the

ruthenium sample was catalytically active. The observation of

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56

OF POOR Q_AL_ITy

methane is consistent with a number of investigations carried

out at lower temperatures, which have shown ruthenium as a

good methanation catalyst (_2,33).

Figure 4.1 shows the accumulated

carbon as a function of time for the

amount of deposited

reactions of a 1:1

mixture of hydrogen and carbon monoxide over the 50Ru5OFe and

33Ru67Fe catalysts at 80OK. While the amount of carbon

deposited over long periods was a linear function of time for

the 5ORu5OFe alloy, this was not the case for the 35Ru67Fe

catalyst. The latter exhibited an increasing rate of carbon

deposition.

4.1.2 Equilibrium Studies

In the equilibrium studies, the catalyst was reduced

under a hydrogen flow for 2.5 - 3 hours prior to every experi-

mental run. About 2.0 g carbon/g catalyst was then deposited

f_,om an equimolar mixture of hydrogen and carbon monoxide at

the reaction temperature of an experimental run. Six or more

weight measurements were normally taken at 30-minute intervals

for each gas composition corresponding to the desired AG c. In

cases where the rate of weight change was very small, experim-

ents were run at an increased period of time to ensure ac-

curate data acquisition. The carbon deposition boundary was

determined at the point where the deposition ceased when it

was approached from the carbon depositing region.

Since no detectable carbon deposition was observed on

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_7

ORIGINAL F'AC_' I'S

OF POOR QUALITy

"ieL

Iw

lad0---

60O

5OO

400

300

EO0

100

800 K. t ate

Catalyst:

& 0.10100 g 50RuSOFe

13 O.10024 g 33Ru67FeFlow Rate:

He t0 cc/sCO t0 cc/s

0.) 20 40 60 80 100

TIME (minutes)

lEO 140

Figure 4.1 Carbon Deposition on 50Ru_OPe an,_ 5_Ru67Fe Alloy

Catalysts from a H2:CO (I :I) Mixture

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58

oF pOOR QUALt'P/

unsupported ruthenium, as evidenced from the preliminary

experiments presented earlier in Section 4.1.1, the unsup-

ported metal was ruled out as an effective Bosch catalyst.

Equilibrium studies were carried out on the two alloy

catalysts, and the results are presented below.

4.1.2.1 5ORu5OFe Alloy

Shown in Figures 4.2, 4.3 and 4.4 are results from

Bosch equilibzium studies at 700, 800 and 9001< and a pressure

of I atm over the 50Ru5OFe catalyst. Multicomponent gas

mixtures of H2, CO, CH 4, C02 and H20 were used with an O/H

ratio of 0.5. This 0/H ratio corresponds to the steady state

value at which a typical Bosch reactor would be operated with

a stoichiometric 2:1 feed mixture of hydrogen and carbon

dioxide. The figures show experimental rates of carbon

deposition plotted a_ a function of AG c, the parameter reflec-

ting the gas phase ( mposition in equilibrium with a carbon of

the corresponding G bs energy. These gas phase compositions

are represented in ne diagrams.

Observed in this equilibrium study is a phenomenon

similar to the one previously reported by Garmirian (9) and

other investigators (16,17,18). The rate of carbon deposition

became zero before the graphite-gas equilibrium was reached,

and the deviation from the graphite equilibrium was pronounced

at low temperatures. Specifically, carbon deposition ceased

at an increasing value of AG c as the reaction temperature was

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59

ORIGi)_AL "' ...... .... "

OF POOR QUALIFY

e-

E

E

Z

I--4I-"I-4¢nc_c1.LUC_

Z

CDrr

(.3

LL0

L_J

,¢Eor

700 K. t armO. 07 Catalyst: 50Ru5OFe• 0.25013 g

0.06 _ • 0.25014 gH20 O/H Ratio: 0.5Flow Rate:

0.05 • 25 cc/s

• 30 cc/s0.04

0.03

0.02

0.00

H2

C0

1 1

-0.02 -2.0 0.0 2.0 4.0

GIBBS ENERGY DIFFERENCE [Kcal/mo]e)

.00

0.50

0.25

0.00

E-6J¢D

W

LUor

¢D¢nLUorQ.

E,¢[CL

Figure 4.2 Rate of Carbon Deposition as a Function of AG c

for an 0/H Ratio of 0.5

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6O

.... _ .. _--o'_._. _j

C

IE

atE

ZOI-4I--I-403¢30.Lg0

Z¢3II]rr

¢J

U-0

LU

CE

05

0.4

0 °. 3

0.2

0.1

0.0

800 K. t ate

Catalyst: 50Ru5OFe

• 0.25017 g

• 0.250t3 g• 0.24996 g

O/H Ratio: 0.5

F10w Rate:• 20 cc/s

II 25 cc/s

zOcc/s

H2

COz

CH,

t t-O.1 -2.0 0.0 .0

GIBBS ENERGY DIFFERENCE

i.00

0.75

0.50

0.25

4.0

(Kcal/mole)

0.00

S

Io

UJK=

0303UJKEa.

k--rr

0-

Figure 4.3 Rate of Carbon Deposition as a Function of AG c

for an 0/H Ratio of 0.5

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iI_ !

¢-

E

1=

Z0I-4I-1-.If_0Q.1,1.10

Z0en

I.I.0

U.II,---

0.8

0.7

O.B

61

900 K. J ate

Cata]yst: 50Ru5OFe,k O.25013 0

O/H Ratio: 0.5

Flow gale:• 25 cc/s

0.4Hz

0.3

H20

0.2COz

0.1

0.0A

A

1_ I I-0._ -2.0 -1._') 0.0 1.0 2.0

GIBBS ENERGY DIFFERENCE (Kcal/mo]e)

i .00

0.25

0.00

E

lID

UJ

t_

.J

I,-,-r'r

0..

Figure 4.4 Rate of Carbon Deposition as a Function of AG c

for an O/H Ratio of 0.5

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___.I

62

lowered. As can be seen in Figures 4.2, 4.3 and 4.4, carbon

stopped depositing on the 50Ru5OFe catalyst at the approximate

AG c values of 0.6, 2.1 and 4.0 kcal/mole for the temperatures

of 900, 800 and 7OOK, respectively. The result indicates that

gas equilibrium with S-graphite over the unsupported 50Ru5OFe

alloy could not be attained under the reaction conditions

studied.

Another phenomenon also observed by Garmirian (9) is

with regard to carbon removal. Although the data concerning

carbon removal in this study are not complete, it can still be

pointed out that carbon removal did not always occur right at

the point where AG c was less than O.0 kcal/mole. In other

words, in many cases carbon removal was not observed until gas

mixtures with AGc values much less than zero were passed over

the catalyst. For instance, while carbon removal was recorded

for the gas mixture with AGc of -_ 0 kcal/mole at 90OK, no

weight change was detected at 800K yen for the AG c value of

-1.8 kcal/mole. The existence of region where no carbon

deposition nor removal was obse_ _d possibly reflects the

difference in reacticn mechanisms involved in the process of

carbon deposition and carbon removal.

Equilibrium studies were also performed at other O/H

ratios over the 50Ru5OFe alloy. Specifically, gas mixtures

with an 0/H ratio of 1.5 were employed at reaction tempera-

tures of 700, 800 and 90OK. The carbon deposition equilibrium

boundary was also studied at 800K using a gas mixture with an

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...... f"

63ORIGIHA_ PA_ 1_OE pOOR QUALITY

The results are presented in Figures 4.5,

earlier

0/H ratio of 0.17.

4.6, 4.7 and 4.8 in a similar fashion as those shown

for an O/H ratio of 0.5.

As with the O/H ratio of 0.5, the results of carbon

deposition equilibrium boundary at 0/H = 0.17 and 1.5 show

that carbon stopped depositing before reaching the graphite

equilibrium and that the deviation from the graphite equili-

brium was large at low temperatures. Furthermore, the carbon

deposition boundary at a given temperature was essentially

independent of the 0/5 ratio of a gas mixture employed, as

evidenced in Figure 4.9 where the value of _G c at which carbon

deposition started is plotted against the reaction

temperature. In other words, at a given temperature, the

Gibbs energy of the deposited carbon was independent of gas

phase composition.

4.1.2.2 33Ru67Fe Alloy

The results of Bosch equilibrium studies on the

33Ru67Fe catalyst are shown in Figures 4.10, 4.11, 4.12 and

4.13 for gas mixtures with an O/H ratio of 0.5 and at tempera-

tures of 700, 750, 800 and 90OK, respectively. This alloy

catalyst showed a promising result. In contrast with the

50Ru5OFe system, the investigation on the 33Ru67Fe catalyst

indicated that at 800 and 900K carbon deposition ceased as AG c

approached zero, which corresponded to a gas phase in equili-

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F..... I

64

OF POOR _L;AL!Ty

r'-

E

Ev

ZK_

I--

030O.LU

Z0a)13:

U.0

0.07

O.OS

0.05

0.04

0.03

0.02

0.0_

'" 0 O0I--

CE

-O.OJ

700 K, J atm

" Catalyst: 50Ru5OFe

• O.J500 g- O/H Ratio: J.5

Flow Rate: COzD

HzO

1----- 1.00

0.75 _

====

0.50 ,.=,,T._,J,==ZI,,-II,-t1"

0.25 .¢13.

0.00

-0.02 _L 1 t-2.0 0.0 2.0 4.0 6.0

GIBBS ENERGY DIFFERENCE (Kca]/mo]e)

Figure 4.5 Rate of Carbon Deposition as a Function of AG c

for an O/H Ratio of 1.5

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65ORIGINAL PAGE IS

OF POOR QUALITY

e-

E

E

Z

I--I

I-,4

U_0OLUJ

Z(:3ODO:

h0

bJ

rr

0.05

0.04

0.03

I 1 I I I I

B00 K, I atm

Catalyst: 50Ru50Fe

A 0.J500 g0/H Ratio: J.5

F]ov Rate:

4, 25 cc/si

,, COz

1.0

0.8E

IJJ

o s ==m

13.

0.4I-,I

0.02 -

& c°__o.; ' <=0.01 _ CH4

0.00 _ 0.0

-0.01 t I i i i e-2.0 -1.0 0.0 J.O 2.0 3.0 4.0

GIBBS ENERGY DIFFERENCE (Kcal/mo]e)

Figure 4.6 Rate of Carbon Deposition as a Punction of AG c

for an O/H Ratio of 1.5

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• =_

66 ORIOINAE PAGE ISOF POOR QUALITY

C

E

E

ZC3l--II--

U_0nLU0

Z0mrr

U.O

LUI--

rr

_.0 T

O.9-

O.B-

0.7-

0.6--

C02

F-_ I------1

900 K. I otm

Catalyst: 50Ru5OFe

• 0.J500 gO/H Ratio: J.5

Flow Rate:

• 25 cc/s

T 1"--'--"

A

H2

I 1 L

0.0 0.5 J.O J.5 2.0 2.5

1.00

0.80

0.60

0.40

0.20

0.00

GIBBS ENERGY DIFFERENCE (Kca]/mo]e)

E

mw

LU

tr3I,iJrr

-J

HI--rr"

n

Figure 4.7 Rate of Carbon Deposition as a Function of AG c

for an 0/H Ratio of 1.5

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!I I

67

5.0

4.0

i_ 3.o

5 2.o

N

_ t.o

_ 0.0M

I I I I I

Catalyst: 50Ru5OFe

Pressure: I ata

OIH Ratio: -@ 0.t7

• 0.5i

-J.O ' I I I I700 750 BOO 850 900

TENPERATURE (K)

Figure 4.8 Rate of Carbon Deposition as a _unction of AG c

for an 0/H Ratio of O.17

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i ....... .

i i

.!

68

OF POOR _UA__

C

E

E

ZC_

ft.

r_

ZC_rn_r

(.3

0

UJ

_r

0.20

0.15 -

0.10 -

0.05

I I

HzO

J I

800 K, t arm

Catalyst: 50Ru5OFe

& 0.1500 gO/H Ratio: 0.17F]o_ Rate:

• 25 cc/s

I |

CH4

O. O0 CO

A

j - 1.00

m

- 0.75

al

0.50

0.25

0.00

E

w

W

W

n

-0.05

-2.0 -J.O 0.0 J.O 2.0 3.0 4.0

GIBBS ENERGY DIFFERENCE (Kca]/mo]e)

Figure 4.9 Carbon Deposition Boundary for Various O/H Ratios

over 50Ru5OFe Catalyst

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y

69

OF POOR QUALITY

t'-.e,,,l

E

I=w

ZC)I,,-I

I'--I--4

U'J¢313.IJJ

ZC}IX3er-,,¢f.3

LI-C]

0.14

0.12

O..JO

O.OB

O.OB

0.04

0.02

"' 0 00I,--<¢el-

-0.02

-0.04

l T---l_r----r--_F_-r-700 K. J arm

_ Cata]yst: 33RuB7Fe _• 0.J5002 g• 0.t4998 g

O/H Ratio: 0.5

F]owPate: A .& 2S cc/s

II 25 cc/s A

4

CO

-2.0 0.0

GIBBS ENERGY DIFFERENCE (Kca]/mo]e)

.00

0.75

0.50

0.25

0.00

S

¢Dw

IJJIZ

MJ¢I:Q.

-J

I,-4

i---a:

¢L

Pigure 4.10 Rate of Carbon Deposition as a Punction of

AG c for an O/H Ratio of 0.5

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70

OF POOR QjAL_TY

E

Z0Mp-

0D.IJJ

Z0mmmr

0

LU

mr

0._.4

0.t2

T

750 K. i arm

Catalyst: 33Ru67Fe

• O.J5002 g

• 0.t4998 gO/H Ratio: 0.5

0.20 _ Flow Rate:

• 25 ce/s

O. OB • 25 eels

C02O.OB

0.04 H2

CO0.02

0.00

•-0.02 L-':;. 04 1

" -2.0 -2.0

L__-..J L-0.0 l.O 2.0 3.0 4.0 5.0

GIBBS ENERGY DIFFERENCE (Kcal/mole)

.00

0.75

0.50

0.25

0.00

E

Io

rr

rJ'JuJer

I,,-II---rr

D.

Figure 4.11 Rate of Carbon Deposition as a Function of

AG c for an O/H Ratio of 0.5

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71

0.5

r-

S

ZZq_

ZC3I--II--I-I(/10O.

0

Z0

_r

h

LU

O:

0.4

0.2

O.1

0.0

-O.l

H20

B00 K. ! atm

Catalyst: 33Ru67Fe

A 0.t5000 g

mm o.24s96 gO/H Rat jo: 0.5

Flow Rate:

• 25 cc/s

II 25 cc/s

H2

COz

CH4

GIBBS ENERGY DIFFERENCE

0.50

0.25

(Kcal/mo]e)

l=

IOw

laJIz=)¢n¢niJJizIz

._J,==[I--I

IZ

tl

Figure 4.12 Rate of Carbon Deposition as a Function of

AG c for an O/H Ratio of 0.5

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+

V2

Ot_IC;INAL PAGE IS

OF POOR QUALITY

¢::

IE

Ii

ZOI-4I--"I,,-I

0O.

r_

Z0ODO:

0

UJ

rr

1.6

1.4

1.2

t.O

0.8

0.6

0.4

0.2

0.0

C0z

900 K. t ale

Catalyst: 33Ru67FeA 0.t4998 g

O/H Ratio: 0.5& 25 cc/s

HZ0

H2

t.00

0.25

0.00

IE

¢D

¢rJt.lJ¢£EL

..,J

i,.,4i,-Iz

EL

-0.21 + .I

-2.0 -t.0 0.0 1.0 2.0

GIBBS ENERGY DIFFERENCE (Kcal/mole)

Pigure 4.13 Rate of Carbon Deposition as a Function of

AGc for an O/R Ratio of 0.5

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73

OF OOR q'OALITY

However, at temperatures below 8OOK,

energy higher than that of 8-g _phite.

that, although the data obtain> :: over

were not as consistent as thos._ in the

carbon deposition boundary at a given

largely independent of gas mixtures.

The second point is

the 33Ru67Fe catalyst

50Ru5OFe system, the

temperature was again

This is evidenced in

Figure 4.17 which illustrates the value of AGc, where carbon

deposition began, plotted as a function of temperatures for

0/H ratios of 0.5 and 1.5. Table 4.1 tabulates the values of

experimental AGc at which carbon deposition began at various

temperatures and O/H gas ratios for both 5ORu5OFe and 33Ru67Fe

brium with _graphite.

the deviation from the graphite equilibrium was very

pronounced. Specifically, carbon deposition stopped at the

AG c values of 4.1 and 5.5 kcal/mole for temperatures of 750

and and 7OOK, respectively. In addition, there existed a

region where no carbon deposition nor removal occurred, a

phenomenon similarly observed for the 5ORu5OFe catalyst

The determination of carbon deposition equilibrium

boundary was also performed using gas mixtures with an O/H

ratio of 1.5. The results are illustrated in Figures 4.14,

4.15 and 4.16 for temperatures of 700, 750 and 80OK. Two

important points can be made regarding these results. First,

they confirmed the results obtained from Bosch equilibrium

studies using an O/H ratio of 0.5. That is, gas equilibrium

with graphite could be expected at high temperatures while

carbon deposited at low tempe_-_ tures appeared to have Gibbs

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I

74

OF POOR QUALITY

dl===_

E;

S

EV

M

I--

030O.b.IC3

ZC)mrr

U

IJ.C;)

IJJI--

rr

0.07

O. 06

0.05

0.04

0.03

0.02

O.Ol

0.00

-O.OJ

I I I I I

700 K, t arm

Catalyst: 33Ru67FeA 0.15002 9

O/H Ratio: 1.5 COzF]ow RaLe:

• 25 cc/s A,

CH4

CO

- J.O0

- 0.75

0.50

0.25

0.00

S

ID

UJO:

O3

UJ13:O.

_J

I.-I

13:

13.

-0.02 - I I t-2.0 0.0 2.0 4.0 6.0

GIBBS ENERGY DIFFERENCE (Kca]/mo]e)

Figure 4.14 Rate of Carbon Deposition as a Function of

AG c for an O/H Ratio of 1.5

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75

OF POOR _;_LiTY

C

S

E

ZC)

I--I-.I

r,n(:3o.14.1

zc)rnIz:

14.o

IJJl--

rr"

0.07

0.06

0.05

0.04

0.03

0.02

0.0:I

0.00

-0.01

750 K. J arm

Catalyst 33Ru67Fe

A 0.]5002 gO/H Ratio: J.5F]o_ Rate:

• 25 cc/s

Hz0

H2

C02A"

CH4

-0.02 1 J z L _.--L---2.0-t.0 0.0 t.0 2.0 3.0 4.0 5.0

GIBBS ENERGY DIFFERENCE [Kca]/mole)

.00

0.75

0.50

0.25

0.00

IE.4J¢D

I.IJrr

¢r3f,r)14.1

,_1,¢[I,-I

I.--n-

¢L

Figure 4.15 Rate of Carbon Deposition as a Function of

AG c for an 0/H Ratio of 1.5

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76

ORIGtN_L r,_;_"_ _

OF POOR QUALITY

¢.-.i-I

IE

Z

I-4I'--I-4¢/30ELLU

Z0mt,r,¢E¢J

M-C_

LIJp-,¢¢

0.10 .

0.09 -

O.OB -

0.07 -

0.06 -

O. 05 -

I 1

800 K. t arm

Catalyst: 33Ru67Fe

• 0.J5002 gO/H Ratio: 1.5Flow Rate:

• 25 cc/s

0.040.03

0.02

0.01

0.00

H2

CO

-0.01 t-0.02 1 1

-2.0 -l.O

A _2

A

CH4

I I

0.0 l.O 2.0

GIBBS ENERGY DIFFERENCE (Kcal/mo]e)

1.0

0.8

0.6

0.4

0.2

0.0

E,,,t,J¢D

LIJ¢1,"

¢/3U3LIJt'I-13.

...I,,,¢EI,-I!.,-,.r'r

EL

Figure 4.16 Rate of Carbon Deposition as a Function of

AG c for an O/H Ratio of 1.5

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/

77

6.0

5.0

4.0

3.0

_ 2.0

t.o

_ 0.0

-t .0

T r 1 I----"

='_ Catalyst: 33Ru67FePressure: I ate

O/H Ratio:• 0.5

- • 1.5

m

-,db-----

I l 1 .1_..--

700 750 800 850 900

TENPERATURE (K)

Figure 4.17 Carbon Deposition Boundary for 0/H Ratios of

0.5 and 1.5 over 33Ru67Pe Catalyst

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Table 4. I

78

G as a Function of Temperatures and 0/HRa_ios for the 50Ru5OFe and 33Ru67Fe Systems

Catalyst Temperature (K) O/H Ratio G c (kcal/mole) I

50Ru50Fe 700 O.5 4.O

800 O. 5 2.2

9OO O. 5 O. 6

700 I. 5 3.9

800 I. 5 2.6

90O I. 5 O. 6

800 O. 17 2.4

33Ru67Fe 700 O.5 5.5

75O 0.5 4.1

8OO 0.5 O.0

900 0.5 O.0

7OO I. 5 4.5

750 I .5 4.0

800 1.5 O. 0

Experimental AGc at which carbon deposition began.

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79

OF POOR QUALITY

catalysts.

Previous investigations by Manning (5), Sacco (7), and

Garmirian (9) have shown cobalt to be the most effective Bosch

catalyst among the three Group VIII metals investigated,

namely iron, nickel and cobalt. For the cobalt system, gas

equilibrium with _-graphite can be attained for temperatures

as low as 80OK, below which deviation from the graphite

equilibrium occurs. E_uilibrium studies of the two unsup-

ported ruthenium-iron alloys in this investigation indicate

that while the 50Ru50Fe powder does not perform as well as

cobalt, the 53Ru67Fe catalyst is as effective as cobalt for

temperatures of 800K and above. At temperatures below 80OK,

however, deviation from the graphite equilibrium for the

33Ru67Fe system is more pronounced than that for the cobalt

system.

4.2 Discussion

An attempt is made in this section to elucidate the

behavior of ruthenium and its alloys with iron towards carbon

deposition. Evidence from various sources is cited to support

plausible explanations. However, further experimentation with

appropriate equipment systems would be required to provide a

definite substantiation.

Also presented at the end of this section is a prelimi-

nary investigation concerning the production of low molecular

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9OORIGINAL PAC-E _SOF POOR QUALITY

weight olefins over supported ruthenium-iron alloy catalysts.

This study was carried out with an anticipation that, if high

production of ethylene and propylene could be achieved, an

understanding of the kinetics involved in the synthesis would

be beneficial for the application of a Ru-Fe catalyst in the

Bosch process.

4.2.1 Ruthenium

As presented in Section 4.1.1, no carbon deposition on

unsupported ruthenium was observed by weight measurement in

this study. The result was quite different from what had

originally been anticipated. As previously mentioned, favora-

ble factors of ruthenium as a potential Bosch catalyst include

the fact that the interference of ruthenium oxide formation

would not occur under Bosch operating conditions. In

addition, because of the very limited stability of ruthenium

carbides, i:L they exist, carbon deposition on ruthenium would

not be limi! ] by the carbide formation, as has been the case

for the nic_ 1 and cobalt systems. Furthermore, Eckerdt and

Bell (26) have reported that a carbon reservoir equivalent to

several monolayers was maintained on silica-supported ru-

thenium at 673K. CO dissociation has also been observed on

alumina-supported ruthenium (25).

Results from a number of investigations have pointed to

an important aspect. That is, supported and unsupported

ruthenium catalysts behave differently. The support has been

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OF POOR QUALITY

81

suggested to alter the catalytic behavior of ruthenium through

both electronic and dispersion effects (34). While CO dispro-

portionation and carbon deposition have been shown to occur on

supported ruthenium, this is not necessarily the case for the

unsupported metal. Low and Bell (25), in their studies of CO

desorption and reaction with H 2 on alumina-supported Ru,

alluded to the fact that no evidence for CO dissociation had

been observed on Ru single crystals, even with the high

surface coverage of CO. An investigation by Delgass et al.

(35,36) using x-ray photoelectron spectroscopy for surface

analysis showed that less than 0.25 monolayer of carbon, if at

all, was detected on the surface of unsupported Ru powder

after 24 hours of Fischer-Tropsch synthesis at 573K and with a

H2/C0 (3:1) gas mixture. They postulated that no carbon

accumulated as a result of the rich supply of adsorbed hydro-

gen on the ruthenium surface. Their reasoning is supported by

a study at low temperztures (313-427K), in which ruthenium has

been reported to have high capacity for H 2 adsorption in the

presence of CO (32). Catalytic decomposition

monoxide on single crystalline ruthenium has been

823K (24); although graphite was observed, it was

the rate of carbon deposition was very slow.

of carbon

studied at

noted that

4.2.2 Ruthenium-Iron Allo__

Figures 4.9 and 4.17 presented in Section 4.1.2 summar-

ize the experimental results of equilibrium studies performed

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i

82 CR!G|T_]AL PAGE I_

OF POOR QUALITY

on 5ORu5OFe and 33Ru67Fe catalysts.

the high water concentration expected from the

equilibrium consideration cannot be achieved in

system at temperatures of 90OK and below or in the

system at teuperatures under 80OK. Based upon the

studies on the Bosch process, two possibilities are

The results indicate that

gas-graphite

the 50Ru5OFe

33Ru67Fe

previous

suggested

to account for the low water yield. One is that some type of

carbon, structurally or chemically different from _-graphite,

is in equilibrium with the gas-phase composition. The other

is that oxidation of the catalyst occurs and inhibits further

carbon deposition, as is the case for the pure iron system.

Surface studies of unsupported Ru-Fe alloy powders have

been reported in the literature (37,38). Of interest is the

investigation by 0tt et al. (37), employing a combination of

x-ray photoelectron spectroscopy (XPS) and secondary ion mass

spect_÷scopy (SIMS) for the study of their Ru-Fe alloy

sample_ The powders were reduced in H 2 at 573K and then

passiv_:_ed by exposure to 0.1-O.5 Tort of ultra-high purity of

oxygen. The results of their analyses showed that the pas-

sivated surface of their samples was a Ru-Fe phase partially

covered by islands of pure iron oxide. No ruthenium oxides

were detected.

Their study raises the possibility of the formation

iron oxide patches on the surface of the 50Ru5OFe catalyst

this Bosch investigation. This oxide formation might,

least partially,

of

in

at

contribute to the inhibition of further

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83.... [U

C_ FOOR QUALITy

carbon deposition. This possibility, however, is unlikely in

the light of experimental results on the 53Ru67Fe catalyst at

800 and 900K for which the carbon deposition bom_dary appeared

to coincide with that of gas-graphite equilibria. If the iron

oxidation in the 50Ru5OFe catalyst did occur and were to

account for the discrepancy between the carbon deposition

boundaries experimentally observed and the gas-graphite

equilibria, the difference should have been even more pronoun-

ced with the increase in iron content in the 33Ru67Fe system.

The opposite phenomenon was observed.

Furthermore, in a subsequent study of properties of

Ru-Fe alloys, 0tt et al. (14) reported that the unsupported

Ru-Fe samples were completely reduced under hydrogen treatment

at 673K and I atm for 4 hours, as evidenced from XPg analysis.

in a review paper on structure and catalytic properties of

iron-containing bimetallic catalysts, Guczi (39) has indicated

that the reducti_,n of iron can be facilitated by introducing a

second metal, su h as Pt or Pd, which is highly active on

hydrogenation. This phenomenon has generally been observed in

the ruthenium-iron system as well. Using M_ssbauer

spectroscopy, Vannice et al. (40) showed that Fe/Si02 catal-

ysts with low iron loading (-O.1 wt%) could not be reduced

below the Fe 2+ state even after reduction in hydrogen at 773K.

However, the addition of ruthenium to Fe/SiO 2 samples -- for

example, 0.1 wt% Fe, 5 wt% Ru on silica support -- led to the

reduction of iron from Fe 3+ to Fe 2+ upon exposure to hydrogen

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84 L-_ FC_.-_ :_/.LiPI'

even at room temperature (27). Vannice eta!. (27) further

reported that the supported catalyst was completely reduced at

773K and that Ru-Fe bimetallic clusters were observed by

Mossbauer spectroscopy. Additionally, Good et al- (58)

affirme_ a complete iron reduction of an unsupported Ru-Pe

sample, which was prepared from the chlorides of iron and

ruthenium (FeCI3"xH20 and RuCI3"3H20) and treated with hydro-

gen at 673K; a Mossbauer peak observed was attributed to iron

in the form of a Ru-Fe alloy.

Ruthenium and iron show contrasting behaviors in their

interactions with carbon. Ruthenium carbides have been

reported to be unstable or of very limited stability (I 3). As

reviewed by Shunk (23), although the observation of ruthenium

carbide, RuC, was reported by one investigator, the existence

could not be substantiated in two other studies. Furthermore,

the solubility of carbon _n ruthenium has been shown to be

very small (23). On the [:her hand, as a result of high

binding energy between ca bon an_ iron, carbonaceous deposits

are normally produced on an iron surface during the transfor-

mation of carbon-containing substances. Various iron

carbides, including Fe2C and Fe3C, have been widely reported

in the literature (23,41,42). In addition, while CO dissocia-

tion occurs to a large degree on Fe, adsorption of H 2 takes

place to a much lesser extent on iron than on ruthenium.

Consequently, it would be expected that the tendency towar_

/ de Isition would rise with increasing iron content in

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_5

OF _OGR Q_f-_L|TY

the Ru-Fe alloys.

In their studies of catalytic behaviors

iron and their alloys at 573-673K for

of ruthenium,

Fischer-Tropsch

synthesis, 0tt et al. (14,23) and Fleisch et al. (24) carried

out surface analyses of their catalyst samples using XPS and

SIMS. No carbon deposition was observed on ruthenium nor on

the 97Ru3Fe alloy. This phenomenon was likely a result of the

large hydrogen coverage on ruthenium. Thus, hydrogen atoms

were available for hydrogenation of surface carbon residues

resulting from dissociative adsorption of carbon-containing

species. On the other hand, with an increase in the iron

content, the alloys of 75Ru25Fe and 33Ru67Fe showed a rapid

carbon buildup during Fischer-Tropsch synthesis. For the case

of a pure iron catalyst, a carbide formation was first noted,

followed by the subsequent buildup of a carbon overlayer on

top of the carbide phase. The formation rate of c_rbon

overlayer on the pure iron catalyst was much slower tha_ on

the 75Ru25Fe and 35Ru67Fe samples. The carbon deposition

rates on the two alloys were also shown to be a strong tem-

perature dependence. Additionally, carbon deposition stopped

after a certain amount of carbon had accumulated. From

surface analyses and kinetic studies, Ott et al. and Fleisch

et al. suggested that the buildup of carbon was nonuniform on

the surface and that a fraction of metal sites remained

essentially uncontaminated. High Fe surface enrichment of the

Ru-Fe alloys was also reported.

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86• J

An interesting observation has been made by Ekerdt and

Bell (26) in their study of hydrocarbon synthesis from CO and

H 2 over silica-supported Ru. They reported that although the

catalyst maintained a reservoir of carbon equivalent to

several Ru monolayers in magnitude, the surface coverage by

chemisorbed CO was not affected by the accumulation of carbon.

The phenomenon suggested that only a small fraction of the

total carbon was present on the ruthenium surface. Ekerdt and

Bell pointed to the possibility that the carbon might be

present on the catalyst support or in filaments extending from

the Ru surface. This speculation w_s not too dissimilar to

the one made by 0tt et al. (55) and Fleisch et al. (36). As

mentioned previously, they pointed out that even though carbon

equivalent to 20-30 layers had been deposited on the unsup-

ported Ru-Fe alloys, the deposited carbon did not cover

uniformly the entire surface of the catalyst. Some of the

alloy surfaces were still accessible to catalyze further

reactions.

The phenomena observed in this Bosch investigation can

perhaps be explained in the light of the studies mentioned

above. No detectable carbon deposition on the pure ruthenium

catalyst reflects the characteristics of unsupported

ruthenium. However, with the addition of _ron to form Ru-Fe

alloys, carbon deposition occurs, as has been the case for

50Ru5OFe and 33Ru67Fe. There are two hypotheses as to why

carbon deposition is enhanced. One is that the introduction

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I

87

of iron to ruthenium changes the electronic properties of the

surface such that carbon deposition is promoted. The other is

that the iron provides favored

deposit; some of the carbon might

bulk alloy.

sites for the

be incorporated

carbon to

into the

brium boundary in the 33Ru67Fe system

gas-graphite equilibria at 800 and 90OK.

atures below 80OK, the gas-graphite

approaches that of

However, for temper-

equilibria cannot be

attained over the 33Ru67Fe catalyst, and this deviation from

the desired equilibria is even more pronounced than in the

50Ru5OFe system. Left unanswered in this study is an under-

standing of reaction mechanisms and Ru/Fe surface interactions

involved in the carbon deposition process. What ].i,_its the

alloy system from approaching the gas-graphite eq_ ,librium?

Is experimental carbon formed structurally or chemically

different from 8-graphite?

The enhancement of carbon deposition increases with the

rise in iron content. This can be observed from the fact that

while carbon deposition on the 50Ru5OFe system ceases upon

reaching certain values of AGc, the carbon deposition equili-

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88_c_ ,_ _._ _

OF. POOR QUALITY

4.2.5 Preliminary Study on the Synthesis of Lower

Olefins I

An unusually high selectivity of unsupported

ruthenium-iron catalysts toward ethylene and propylene has

been reported in an investigation of Fischer-Tropsch synthesis

by Ott et al. (14), as presented previously in Section 2.3.2.

Their experimental data were obtained in a fixed bed reactor

system operated at conversions below 3%- Of interest in this

study is an understanding of kinetic effects on the production

of low molecular weight olefins over alloy catalysts at

various degrees of conversion. If high yields of olefinic

species could actually be obtained at high conversions, such a

knowledge of the kinetics involved would certainly be

valuable, as it could lead to an overall improvement in the

Bosch process. Specifically if ethylene and propylene could

be produced at high levels, the benefits would be derived as

result of both the enhanced carbon deposition from a gas phase

containing high olefi_ content and the low reaction temperatu.

res used in the hydrocarbon synthesis. Highlights of this

preliminary study (43,44) are presented below.

A representation of the experimental apparatus is shown

in Figure 4.18. Originally used in the kinetic study of

I • Credit should be given to D. M. Borowski, B. R. Moroney,E. D. Morris, B.A. Sackett and J.C. Willard for

experimental results presented in this section.

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..... /

s9

OF POOR Qu_-_L,I'Y

2E

I

_n

J

0

r.

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9o

ethylene oxidation by Mahan (45), the equipment w_s modified

and composed of three basic section: the gas feed system, the

reactor, and the gas analytical system. The gas feed system

included four tube rotameters equipped with mass flow regula-

tors for the control of gas flow rates. An eight-position

switching valve allowed the flow of desired gas to pass to the

reactor system. Housed in a heated metal block equipped with

a temperature controlling system, the reactor w_s made of a

I/4-inch glass-lined stainless steel tube 8 cm long. The

catalyst was held in place between plugs of Pyrex wool inside

the reactor. A recycle pump allowed the reactor to be opera-

ted as a CSTR. The pump could be removed from the loop and

valves adjusted to form a single plug flow reactor. Through

the switching of micro-volume sample valves V#5 and V#1, inlet

and outlet gas samples, respectively, were introduced into the

gas analytical system, which consisted of two columns of

Porapak Q$ and a thermal conductivity detector. The gas

components were separated in the following sequence: H 2, CO,

CH4, C02, C2H4 ' C2H6 ' C3H6, C3H8, and higher hydrocarbons. A

pneumatic switching valve allowed the 2-m Porapak QS column to

be bypassed after C02 had evolved so as to shorten the analy-

sis time for the remaining components. A gas mixture of 91.5%

He and 8.5% H 2 was used as a gas carrier, and the signals from

the thermal conductivity detector were integrated by a Spectra

Physics Minigrator. Because of the broad peak and its inter-

ference with other gas peaks, the water component was not

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I

!

91

OF POOR QU;,LIFY

integrated.

Two types of catalysts were prepared

wetness technique. One type of the catalyst

by an incipient

was a 50Ru5OFe

(atomic Ru:Fe = 1:1) alloy supported on _-alumina (20-40

mesh), having a metal loading of -10 wt_; the other was a

97Ru3Fe (atomic Ru:Fe = 97:3) catalyst supported on 40-60 mesh

Y-alumina with a 5 wt_ metal loading.

chloride (RuC13/FeC12) solution of desired

and of known volume was added dropwise to

constant mixing so as to ensure that the solution would all be

uniformly absorbed on V-alumina.

air dried before being reduced

sodium borohydride. The reduced

An aqueous metal

Ru/Fe composition

the support with

several times with distilled water, air dried, and subsequen-

tly treated overnight at 773K under a hydrogen atmosphere, to

remove traces of the chlorides and to presinter the catalyst

before _se. Determined by the BET/N 2 method using a Quanta-

sorb so ption system, surface areas of the activated samples

were 49 0 and 96.9 m2/g for the supported 50RuSOFe and

97Ru3Fe, respectively.

Experiments to determine the merits of

alumina-supported 50Ru5OFe and 97Ru3Fe alloys as catalysts for

the synthesis of lower olefins were performed by Borowski et

al. (43) in a recycle reactor modeled as a CSTR. Tests were

done at 473, 523 and 573K with feed mixtures having the H2/C0

ratio of 3:1, 2:1 and 1:1. Heat and mass transfer limitations

The impregnated support was

in an aqueous solution of

catalyst was then washed

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OF pOOR Q_3__i!i'i¢ 92

..... .t

were shown to be negligible. Used catalysts were regenerated

in hydrogen at 723K for 3 hours, and reproducible results were

obtained. This is in agreement with the observation made by

0tt et al. (35), who reported the restoration of the synthesis

activity upon the treatment of unsupported 75Ru25Fe in hydro-

gen at 683K.

trace of ethane

unobserved at

deactivation.

4.2.3.1 50Ru5OFe Supported Catalyst

In their initial investigation of the supported

50Ru5OFe catalyst with CO conversions ranging from 13% to

0.4%, Borowski and coworkers reported no proguction of olefins

and substantial deactivation of the catalyst over time.

Methane was the major, and in many cases the only, hydrocarbon

product. A trace of ethane was observed in some experimental

runs. C02 and H20 were also formed. An example of the

product distribution obtained for the 50Ru5OFe catalyst is

presented in Fig_?re 4.19. Figure 4.20 illustrates the charac-

teristic deactivations of the catalyst, which was observed for

CH 4 and C02 in all of the runs. The drop in catalytic ac-

tivity was sharp initially and leveled off over a period of

time. Borowski et al. noted that similar trends probably

existed for any undetectable hydrocarbons, as, for instance, a

was detected initially in some

a later stage with increasing

runs but

catalyst

The results obtained by Borowski et alL. (43) are not

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95

66.6

21.6

Run Conditions:

H_CO Feed Ratio = 3:1

Temperature = 573K

A%_. _icn = ]3.6 %

3.7

1.4 0.23

Pigure 4.19 Product Distribution for 5ORu5OFe Catalyst (45)

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r.... .r_ _-

94

OF POOR _L_Y'f

1.3

1.2

I.i

1.0

0.9

0.8

0.7

Conditions :

H2/CO Feed Patio = 3 :i

Temperature = 573K

Ave. Conversion = 3.72 %

• I m w w I ! J ! ! I

0 8 16 24 32 40 48

Time (Minutes)

Figure 4.20 Catalyst Deactivation for 50Ru50Fe Catalyst (43)

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95 OF POOR QUALITY

too dissimilar from those reported by 0tt et al. (!4,35). In

their study of Fischer-Tropsch synthesis over unsupported

Ru-Fe alloys using a gas mixture of 3.3 H2/C0, 0tt et al.

indicated a rapid carbon buildup on both the 33Ru67Fe and 75

Ru25Fe catalysts, resulting in a significant drop of the

catalytic activity as active sites on the surface decreased.

More importantly, the selectivity of the catalyst shifted

sharply towards methane and carbon dioxide as the carbon

buildup proceeded. A decrease in ethylene selectivity was

also observed; as pointed out by Ott et al. (_5), this change

is significant in that a low conversion usually leads to an

increase in olefinic to paraffinic ratios. The shift in

selectivity is indicative of large metal ensembles required

for the production of higher hydrocarbons.

While catalyst deactivation was observed by both

Borowski et al. (43) and Ottet al. (14,35), a major dif-

ference was that the deactivation occurred at a much faster

rate in the case of B,,-owski and coworkers than in the other

study. A combination of factors might contribute to this

difference. It might be accounted for by the influence of

metal-support interaction and metal particle size of the

alumina-supported catalyst. In addition, in contrast with the

differential conversion performed by Ott et al., Borowski et

al. carried out their investigation normally _t a relatively

high conversion, which would result in a rapid carbon buildup

on the catalyst. The rapid coverage of catalyst surface with

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96 OF POOR qt_ALtTY

carbon would lead to a sharp decline in large metal

necessary for the

Consequently, only

initial stage of

production of

traces of ethane

the experiments.

including hydrogenation, hydrogenolysis

ensembles

higher hydrocarbons.

were observed at an

Secondary reactions,

and cracking, could

also be enhanced, as hydrocarbon

formed, were recycled back in

reactor. The last hypothesis on secondary reactions has

tested on another alumina-supported catalyst, 97Ru3Fe,

pulse reactor, and the results are presented in a

intermediate species, if

a CSTR-simulated recycle

been

in a

later

section.

4.2.3.2 97Ru3_e Sup_ported Catal___

Ott et al. (14,35) have shown that an

97Ru3Fe alloy, contrary to 33Ru67Fe and 75Ru25Fe

unsupported

catalysts,

exhibited constant selectivity towards hydrocarbon formation

over time, as a result of essentially no carbon buildup on the

alloy. When corrected for an _ncrease in particle size during

the course of reactions, the overall catalytic activity also

remained unchanged. Consequently, as the 50RuSOFe catalyst

experienced heavy carbon deposition, an alumina-supported

et al. (43) as an97Ru3Fe catalyst was chosen by Borowski

alternative choice for further investigation of the merits of

Ru-Fe alloys in the synthesis of lower olefins. CO conver-

sions were in the range of 10-25% in most cases,

conversions above 30% were occasionally experienced

instance, at 573K with H2/CO feed ratios of 2:1 and 3:1.

although

-- for

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97

2.2_10 -4

3.oxio-5

1.6xlO

1o-4 J

0 1 2 3

B2/CD Ratio

Figure 4.21 Overall Reaction Rates of 97Ru3Fe Catalyst at

Various Temperatures and H2/C0 Feed Ratios (43)

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O_;3!N_L F'_CE IS'

OF POOR QUALITY

98

Shown in Figure 4.21 are overall reaction rates of the

supported 97Ru3Fe catalyst in a recycle reactor at various

temperatures and H2/C0 feed ratios.

reaction increased with temperature.

in the H2/CO feed ratio led to a

As expected, the rate of

In addition, an increase

rise in reaction rate,

possibly as a result of additional hydrogen available to

hydrogenate adsorbed species and keep the catalyst surface

clean. Product distributious obtained from the recycle

reactor under the same operating conditions and at 573K are

compared in Figure 4.22 for feed gas mixtures with the H2/C0

ratios of 1:1, 2:1 and 3:1. As mentioned earlier, the overall

conversion increased with the H2/C0 feed ratio. Small amounts

of ethane and propane were observed for the 1:1 H2/CO feed,

which also corresponded to a low conversion. However, as the

H 2 content in the feed stream increased, the product distribu-

methane.

w_ter-gas

water and

tion shifted strongly toward the formation of

Borowski et al. pointed to the importance of he

shift reaction in shifting the distribution

carbon dioxide as the feed ratio of H2/CO varlet

Borowski and coworkers also noted that an increase in

the flow rate of the fresh gas feed to the recycle loop

resulted in a decline in conversion and generally led to a

rise in selectivity towards higher hydrocarbons. Figure 4.23

compares the selectivity towards C 2 and C3 hydrocarbons for

H2/CO feed ratios of 1:1 and 1:2 and at temperatures of 523

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Or,:Cr,' ...... _-'..L _ _,,

OF pOOR QUALITY

50 -

25 -

I:I Feed 2:1

- - .

-- - -

_- C-"

3:1 Feed

_]0t 4

_H20

C2H6

Tsmperature - 573K

Flow Rate - I0 cc/_m

* H 2 and (3D _ up for the ba/ance.

Figure 4.22 Product Distributions over g7Ru_Pe Catalyst

at Varying ._eed (}as Ratios (4_)

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1 O0

i!,

iI

..... °

-=--=:.:g_

52:_1(

-- 0.1 --

-- 0.05--

-- --_-- --_ --_.

_--__-- .--_-- _--

-- --_--.-- --.

_--._-- _-- --_-

r.....

573K

1 :I H2/CO Feed

2:1 H2/CO Feed

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101 ,....._.,_

and 573K. As can be seen from the diagram, the selectivity

towards higher hydrocarbons at 523K w_s much greater than at

573K. A small amount of ethylene, the only olefin ovserved in

this investigation, was observed at 523K with a H2/C0 feed

ratio of 1:1.

Although, for all experiments carried out by

et al. (43), conditions at 523K and H2/C0 feed ratios

and 2:1 showed the most promising result in terms

production of C 2 and C3 hydrocarbons, the selectivity

higher hydrocarbons at these conditions was still

Borowski

of 1:1

of the

towards

at an

unacceptably low level. In addition, no olefins were detected

in most cases. The results of this alumina- supported catal-

yst are in marked contrast with those of unsupported 97Ru3Fe,

for which an unusually high selectivity towards ethylene and

propylene has been noted. One possible factor accounting for

this difference in performance is the high CO conversion level

employed in the Borowski investigation. This notion, however,

attributes only partially to the difference in catalytic

activities, as has been substantiated in a subsequent study by

Sackett and Willard (44). Using the same experimental appara-

tus as Borowski et al. (43) but operated in a plug flow

reactor (PFR) mode with the recycle loop removed, Sackett and

Willard performed experiments over the supported 9TRu3?e

catalyst with a H2/CO feed ratio of 3:1 at varying flow rates

and temperatures. These experiments were intended to simulate

the differential _onversion as carried out by Ott et al. (14)

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102 OF

over their unsupported cata,yst at 573K with a 3.3

mixture. However, no hydrocarbon product except

observed.

The above study by Sackett and

important point: a difference between

H2/CO gas

methane was

Willard _ndicates an

supported and unsup-

ported catalysts as well as a difference even among catalysts

of various supports, as has been reported in a number of

studies (34,39,46). Vannice etal. (27) have also obtained

high olefin yields over silica- supported Ru-Fe alloys, but

the selectivity is lower than that observed by Ott et al.

(14). The metal-support interaction, metal particle size, and

degree of metal dispersion are among possible factors to be

considered. In a_dition, the expected alloy formation on the

alumina support used in the studies by Borowski et al. (43)

and Sackett and Willard (44) might not have occurred as had

been anticipated. Purthermore, the catalyst might not be

completely reduced to its ground state as a result of the

influence of the support, as evidenced in many observations

of well dispersed iron supported catalystsmade in the case

l (39).

Since an unusually high selectivity towards ethylene I

i

i

i and propylene has been observed in a differential reactor

, using an unsupported 97Ru3Fe catalyst, it would be interesting i"

| l

i to see whether the same highly selective result could be I

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103

4.2.3-3 Secondary Reactions

A number of investigations (47,48) have provided

evidence that, except for methane, the primary products from

synthesis gas are olefins. When operated in a recycle mode or

at a high conversion, reaction products formed could be

subject to secondary reactions, including hydrogenation.

hydrogenolysis and cracking. These secondary reactions could

account for, at least partially, the low production of higher

hydrocarbons, and specifically olefinic compounds, observed in

the Borowski study.

The postulate of secondary reactions taking place in

the CSTR- simulated recycle reactor has been confirmed in a

study by Sackett and Willard (44). The reactor was operated

in a PFR mode. Feed mixtures composed of H 2, CO and C24 at

various compositions (H2:C0 = 3:1; C2H4~25-40%) passed through

supported 97Ru3Fe catalysts at temperatures of 473, 523 and

573K. The following were generally observed in most cases.

Over 50 percent of ethylene wa_ hydrogenated to ethane

initially; the percentage dropped with increasing time on

stream while the fraction of unreacted ethylene increased, the

phenomenon indicative of catalyst deactivation possibly as a

result of surface coverage with carbon and adsorbed species.

Small amounts of methane and propylene were observed, and so

were traces of propane which, interestingly, appeared in a

smaller quantity than propylene. These products also declined

as reaction time increased. The results are consistent with a

i

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1 04

general observation that hydrogenation of olefins occurs more

rapidly than the cracking activity (49). Furthermore, the

presence of ethylene enhanced the incorporation of additional

carbon, resulting in the formation of propane and propylene.

A blank run was also carried out to de_ermine whether

secondary reactions would occur over the support. A gas

mixture of 25% ethylene and 75% H2/CO (3:1) was passed over

V-alumina with no metal loading at 523K. Only traoes of

methane and ethane were observed, thus indicating virtually no

direct influence of the support on secondary reactions. This

conclusion does not, however, exclude the metal-support

interaction which alters catalytic properties of supported

catalysts from unsupported ones.

Sackett and Willard (44) further investigated the

influence of supported 97Ru3Fe on secondary reactions, speci-

fically cracking, using a pulse reactor shown schematically in

Figure 4.24. Helium was used as a carrier gas and was con-

stantly passed over the catalyst. A pulse of a desired gas

component, 0.10 cm 3 in volume, was injected into the reactor

through the switching valve

analyzed by the on-line

earlier.

The catalyst, 0.30

ethylene and propane at 523K.

occurred to a large extent,

methane.

V#1. The effluent stream was

gas analytical system described

gram, was pulsed with ethane,

In the case of ethane, cracking

resulting in the formation of

No ethane was observed initially. After ten pulses,

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,,,_++

105

|

,I+

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106.OF POO_ Q_!_tiTV

however, ethane started appearing and

with an increasing number of pulsing

methane declined. A small amount of

its content increased

while the fraction of

hydrogen was observed

throughout the run. For the pulsing experiment with ethylene,

methane was the only hydrocarbon product observed initially.

A small amount of ethane was observed after seven pulses, and

ethylene appeared at the eighth pulsing. The formation of

methane dropped dramatically in subsequent pulses; meanwhile,

ethane reached its peak, after which it declined rapidly and

ethylene became the dominant species. Again, hydrogen was

detected throughout the experiment.

The saturated hydrocarbons methane, ethane and propane

were observed throughout the pulsing study with propane. At

an early stage, methane was the dominant product. Mowever,

with an increase in the number of pulsing, the fraction of

propane rose while the methane content decreased

substantially. _thane remained at a low level throughout the

run. In all three pulse experiments, the catalyst was pulsed

with hydrogen after the pulsing with hydrocarbons

completed. A substantial amount of methane was detected

all cases, indicative of

catalyst.

The results from the

that the Ru-Fe catalyst

active surface carbon on

W_S

in

the

Furthermore, mass balance and a drop in activity indicate some

of the products were strongly adsorbed on, and thus poisoned,

pulse experiments clearly show

enhances the cracking activity.

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107OF PO0_ QUALITY

the catalyst surface. Both

experiments by Sackett and

activity of hydrogenation

the PFR study and the pulse

Willard (44) substantiate the

and cracking over the 97Ru3Fe

supported catalyst. Consequently, for a successful production

of low molecular weight olefins as primary products, not only

is the development of _ highly selective catalyst

but the suppression of secondary reactions is also

to minimize the desired olefins converted to

products.

required,

necessary

unwanted

:_i

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108

• • _..-._. _

.... -..... QJALI'rV

5. Application of the Results

Ruthenium and its unsupported alloys with iron --

50RuSOFe and 33Ru67Fe -- have been investigated in this study

in a continuing process to develop an efficient catalyst for

the Bosch process. An efficient Bosch catalyst is defined as

the one which can yield the maximum water concentration

therm_dynamically allowable at moderate temperatures

(700-80OK). This yield corresponds to the water concentration

in equilibrium with the 8-graphite phase. The extent of water

conversion is a major consideration in designing a recycle

equilibrium Bosch process as remaining gas components are to

be recycled to the reactor. The higher the water conversion

per pass is, the lower the recycle ratio is required.

Shown in Figure 5.1 are equilibrium water concentra-

tions as a function of temperature for the 8-graphite and

various catalyst systems for an 0._H ratio of 0.5. Inhibited

by the formation of oxides, the iron system exhibits the

maximum water concentration at 915K, the temperature at which

the iron-iron oxide-gas equilibrium and the graphite-gas

equilibrium intersect at an O/H ratio of 0.5 (5,7). For

nickel and cobalt catalysts, the water concentration is

determined by the carbide equilibrium at low temperatures and

the graphite equilibrium at high temperatures. The maximum

water concentration for the cobalt and nickel systems occurs

at 800 and 825K, respectively (9). It should be noted that

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109

ORIGINAL P,_-E IS

OF POC', QUALITY

50

40

3O

o/H= o.5

3"Lq:lu67F'e Fe

_50Fe

N1

e-aphi_ _-" ""E_i]ibria i ,. _ i

0 ;'_ 900700 750 800 : _-

TF.I_ERATLIRE (K)

Figure 5.1 Equilibrium W_ter Concentration of a Bosch Reactor

for Various Catalyst System

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110oR'C:;',;;_.Lr":',3F: I_OE POOR QUAL;JTY

the maximum water yield for the nickel system does not corres-

pond to the temperature where the carbide-gas equilibrium

coincides with the graphite-gas equilibrium, as is the case

for cobalt. Garmirian (9) reported the graphite-gas equili-

brium for the nickel catalyst not attainable even at 90OK.

Similar results have been observed in this study for the

unsupported 50Ru5OFe system, in which AG c was 0.6 kcal/mole at

90OK. The maximum water concentration for the 50RuSOPe alloy

takes place at 865K. Figure 5.1 also shows the water mole

fraction as a function of temperature for the S3Ru67Fe system,

havin6 the maximum water content at 80OK. The water concen-

trations of the Ru-Ee alloy systems were determined from the

values of _c of the carbon deposition boundaries linearly

interpolated about experimenta_ points, as shown in Figures

4.9 and 4.17. The maximum water concentrations attainable for

different Bosch catalysts are tabulated in Table _.I with

their corresponding temperatures.

A Bosch recycle reactor is shown

Figure 5.2.

schemat3 _ally in

For every two moles of H 2 and one mole of C02 fe4

to the reactor, two moles of water are produced.

plified calculation wlth the assumption that the

water by condensation from the reactor effluent

1OO%, the number of moles of recycled gases (H2, CO,

CO 2) per mole of C02 fed is

In a sim-

removal of

stream is

CH 4 and

I

r = 2 r_I-IL J

XH20,equtlbrium

(5.1)

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111ORIG.,,_,LOf pOOR QUALITY

Table 5. I Maximum Water Concentrations and Minimum Recycle

Ratios for Various Bosch Catalysts

Catalyst Temperature Maximum Water Minimum Recycle

Fe 915 15.8 10.6

Ni 825 24.5 6.2

Cc 800 "52.3 4.2

50Rur-,OFe 865 14.8 11 . 5

_3Ru67Fe 800 _2.3 4.2

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L

L

0

u¢)

IO,J

eftC

"0C0LJ

C;

..0 0

0U "-

ur)

0

C3

L.)

4'

urt

:z: _:

o'_ _oc_ c,uALrrv

LJ >.,

o _

cr_ W

- 0

-r

x

v

04_0o_

Iz:

0

0

,¢:oo3o

L_

Obk

r=,

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113

ORIG|NAL "'""_"

OF POOR QUALITY

where XH20,equi I is the equilibrium mole fraction of water.

Figure 5.3 shows the recycle r_tios as _ function of

temperatures for various catalysts. The minimum recycle

ratios for iron, cobalt, nickel, 50Ru5OFe and 33Ru67Fe are

I0.6, 4.2, 6.2, 11.5 and 4.2, respectively. A substantial

reduction in recycle ratio can be achieved by the additlon of

a reverse water-gas shift reaction before the gas mixture is

sent to the Bosch reactor; details of improved versions of the

Bosch process can be found in Manning (5), Sacco (7) and

G_rmirian (9).

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0.5 i 1 ! i i

O/H = 0.5"" _6raphite

Equil ibria

0.4 - _. _

0.3 -

O.E

O.l

0.0 i l I I700 750 800 B50 900

TEMPERATURE (K]

Figure 5._ G_s Recycle Ratio for a Bosch Recycle Equilibrium

Reactor

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OF POOR QLIALII'Y

II_

No detectable e_rbon depo,_i_!on by wPi_h% _e._suremPnt

hns been observed for unsupported ruthenium powders, thus

rullna out the possibility of this unsupported metql bein_ a

_ood Bosch catalyst. The result Is in m_rked contrast with

that of supported ruthent%l_, t'or which c_rbon deposition has

been observed in a number of studies, lPurther_ore, experimen-

tal results lnaieate that the 5ORu_OPe alloy is not superior

to the two previouslv inv_,_% i_ated cobalt and nlekel

catalysts. On the other hand. results from the _Ru67Pe

syste_ are prosisin_. _,% temperatures of SOOK and beyond.

lu,_xi_u.'u v, tPr eon,-entr_tions in equ_llbrlum wlth F-_raphlte

c_n bo qtt._inPd in th_ _XRu67Fe system, qs ham also bP_n the

cs.q_ for the cob ql% e,talyst. However. th_ _evlatlon from

gr_phite-gns equilibri, in the x_R_|6"FP system at _OO and 7_OK

is more pronounced th.%n that observed with the cobalt catalyst

or even the 50_uSOPe ,lloy. Defln_te explanations for reae-

tlon mechanisms and the influence of ruthenium/iron content on

the carbon deposition process are unavailable from this study.

._ueh an un,_erstanding Of surface behaviors of alloy catalysts

could lead to the development of an t_prove_ Bosch ea'calyst.

In the investig._tion of synthesis of low molecular

weight clef ins, methane was the dominant hydrocarbon product

for both _ORuSOFe and 97Ru3Pe c..talysts supported on

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116 OF POCR Q_JALITY

y-alumina. Most experiments were conducted at CO conversions

of 10-30% in the temperature range of 473-573K using H2/CO gas

mixtures of various compositions. For the 50Ru5OFe supporte_

catalyst, ethane was the only higher hydrocarbon observed and

appeared in a small amount In the initial stage of

experiments. Catalyst deactivation occurred very rapidly. On

the other hand, the 97RuSFe supported catalyst showed higher

catalytic activity, better selectivity

hydrocarbons and longer catalyst life

catalyst. However, the selectivity

towards C 2

than the

towards

and C3

50Ru5OFe

higher

still athydrocarbons, and specifically towards olefins, was

an unacceptably low level. Experiments on the 97Ru3Fe catal-

yst have also shown secondary reactions, namely, hydrogenation

and cracking, to take place under synthesis conditions.

The results from the study of hydrocarbon synthesis

o_r the supported catalysts have proved to be quite different

fr n those originally anticipated. The unusually high selec-

ti ity towards ethylene and propylene, as reported by Ott et

al. (14) using a differential reactor with unsupported Ru-Fe

alloys, has not been observed in this study. The selection of

y-alumina as a support is perhaps an unwise choice as a result

of metal-support interactions. It would be interesting to

determine whether the high selectivity of unsupported Ru-Fe

alloys towards ethylene and propylene would still be main-

tained when the catalysts are operated at high conversions.

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OF pOOR QUALITY

117

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118

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120 : ..... ' "" '

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,'_, •:" i T"¥OF pO0_ _""-"

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