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Page 1: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

W.^sf^j 'f^ ?H

'"fC-^'K.i.y^'tt^ PATL^

Thermo Electron

CORPORATION

/ i

DISTRIBUTION JF THIb 0( LJ ' / t f . ' ! iS UHV. ,*

Page 2: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

DISCLAIMER

This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency Thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or any agency thereof. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof.

Page 3: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

DISCLAIMER Portions of this document may be illegible in electronic image products. Images are produced from the best available original document.

Page 4: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

Thermo

[ ' U i P n R A M O KJ

K Electron

Report No. TE4233/4237-60-78

NASA/DOE

ADVANCED THERMIONIC

TECHNOLOGY PROGRAM

PROGRESS REPORT NO. 28

October 1977

NASA Contract NAS3-20959 ERDA Contract EY-76-G-02-3056

P r e p a r e d By

The rmo Elec t ron Corporat ion 101 F i r s t Avenue

Waltham, Massachuse t t s 02154

t^ UiSTPiBJTiON : T,-SS i v ^^ .

Page 5: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

W/M^ Thermo f/c. Electron f ( ) n I •( i n AT I CIN

I . SURFACE STUDIES

A, SURFACE CHARACTERIZATION CHAMBER

Samples from surface charac te r i za t ion and conver ter exper iments

were analyzed by Auger spec t roscopy . A p o s t - m o r t e m Auger analysis

of Converter No. 166 indicated that lanthantim had t r ans fe r r ed from

the lanthanum hexaboride col lector to the tungsten e m i t t e r . In addi ­

t ion, carbon, oxygen, sodiusxi, cesium^ tungsten, and rhenium were

detected on the e m i t t e r . The e33aitter surface had become a dull g ray

that could be peeled eas i ly with a r a z o r blade. The exposed a r e a s con­

tained no rhenitim but did contain a g r e a t e r amount of lanthan\im. The

source of rheniura mus t be the molybdenum-rhenium braze that bonds

the era i t ter to the emi t t e r s l eeve . No molybdentxm peaks were readi ly

apparent ; however , if any weak peaks were p resen t , they could have

been dominated by the tungsten spec t rum. Rhenium and molybdenum

oxides a r e both known to be vola t i le , rhenitim being considerably

m o r e s o .

Suprisingly, no rhenium was evident on the col lector although

carbon, oxygen, ni t rogen, sodium, nickel , ces ium, lanthanum, and

tungsten were detected. The lanthanxim and tungsten signals were of

comparable s t r eng ths . Except for one out of the seven spots analyzed,

carbon concentrat ions were s m a l l . Most l ikely, nickel and sodium

w e r e introduced during handling subsequent to the opening of the

c o n v e r t e r .

The Se len ium-Reservo i r Conver te r , No, 173, was dissected and

i t s contents were analyzed. The coEector had a dark deposit along the

edge of the opening to the se lenium r e s e r v o i r . Auger analysis indicated

1

Page 6: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

ZJZ Thermo f/c Electron t I ) t KM I n A n ci N

this deposit to be e lementa l seleniijxn.. The emi t te r surface was shiny

(like e lectropol ished tungsten) except for a number of smal l da rk

specks about 1/2 inm in d i a m e t e r . The highest concentration of these

specks appeared in the "shadow" of the selenium r e s e r v o i r opening.

Auger analys is showed the specks to have a high concentration of

selenixira. A few of the selenium Auger spec t ra obtained from var ious

spots on the emi t t e r surface were d is tor ted - indicative of a selenium

compound.

The emi t t e r of Converter No. 173 was subjected subsequently to

an e lec t ron mic roprobe ana lys i s . An analysis taken over an a r ea

about 1 m m at the center of the emi t t e r surface showed the presence

of se lenium, tungsten, ces ium, and a slight amount of nickel . F igure

I - l shows a port ion of this analyzed a r e a magnified 1000 t i m e s . The

l ighter rec tangular portion of the is land-l ike s t ruc tu re was found to

be ces ium, a s were the nximerous globules; the smoother , open a r e a s

were tungsten. The c rus ty region contained cesitim, xnost likely

ces ium hydroxide , which dr ied and cracked under the vacuum environ­

ment of the e lec t ron m i c r o p r o b e . Thus , the emi t te r surface is s e g r e ­

gated into regions of tungsten, selenitim, and ces ium (hydroxide). The

observed d is tor ted selenitoin Auger spec t ra a r e mos t l ikely caused by

the complicated surface topography of the sample . These ana lyses ,

coupled with the independence of the conver te r cha rac te r i s t i c s as a

function of se lenium r e s e r v o i r t e m p e r a t u r e , suggest that a selenium

cold spot existed in the diode. A second conver ter is being constructed

in o rder to continue these invest igat ions .

The r e su l t s of other Auger ana lyses a r e given in subsequent

sect ions of this r e p o r t .

2

Page 7: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

w 7711-15

F igure I - l , Scanning Elec t ron Photomicrograph of Central Region of the E |n i t t e r (Converter No. 173) (Magnified lOOOx)

Page 8: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

m/gm Thermo f/c, Electron f ( ) t I P ( ) R A I if TM

I I . PLASMA STUDIES

A. CONVERTER THEORY

Schottky and Goiilorab sca t te r ing effects were added to the analyt ical

raodel of the ignited in te re lec t rode p l a s m a . The computer p rog ram was

improved to accommodate these two effects, with prel inainary resu l t s

plotted in F igure I I - 1 . These calculations indicate that Schottky effects

can produce output cu r r en t s significantly l a rge r than the corresponding

sa tura t ion c u r r e n t s . Coulomb sca t te r ing was found to have liie poten­

t ia l of substant ial ly increas ing the a r c d rop .

The requ i red emi t t e r sheath height for the formation of the double

sheath can be calculated f rom a s imple sheath model by matching solu­

tions der ived f rom independent analyses of the p lasma and eini t ter

sheath^ as shown in F igure I I -2 . The double sheath is seen to be

formed at a cu r r en t r a t io of approximately 0 . 5 5 . This value is con­

s is tent with exper imenta l observations^ assuming such formation is

assoc ia ted with the knee of the I-V cha rac t e r i s t i c s of diodes, and

appears at the c u r r e n t ra t ios between 0 .4 and 0 . 6 ,

B , EXPERIMENTAL PLASMA ANALYSES

Spectroscopic analyses of conver te r p lasmas under operating

conditions were ini t ia ted. Spectra a r e being taken throughout the

4000 to 9000 A region. Line width, and re la t ive line and continuum

intensi ty m e a s u r e m e n t s allow determinat ion of e lec t ron densi t ies and

t e m p e r a t u r e s , as well a s excited state population densi t ies through­

out the in te re lec t rode reg ion . Sensitive detection may enable t r ace

consti tuents ( e . g . , oxides) to be moni tored . Changes in p lasma con­

ditions due to var ia t ions in T , T j T , e lect rode spacing, and L C R

4

Page 9: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

7710^4

1.1

1.0

0.9

(0 - 3

0.8

0.7

0.6

0.5

0.4

1 ! 1 1 ! 1 ! 1 r WITH COULOMB SCATTERING ^

WITH SCHOTTKY EFFECT

/

/

/

/

WITHOUT SCHOTTKY' EFFECT

// ' '^^wiTH couLoye / / / SCATTERING

J I I L J i™__„_L

0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 OB 0.9

V^ (VOLTS)

Figure 11-1. Schottky Effect on Converter Per formance

Page 10: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

7710-13

>

5.0

4.0

3.0

2.0

LO

0

1 r I 1 1 —

/ -—PLASMA / SOLUTION

/

/

/ SHEATH'S. / SOLUTION >y y^

- ^/L^""""^ 1 ^ 1 1 1 1

-

-

-

0.5 0.6 0.7

J /J ,

0.8 0.9 1.0

Figure I I -2 . Format ion of Double Valve Sheath

Page 11: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

migm Thermo i c : Electron f ( ) M n ( i n A r I O N

current were observed. Temporal decay of interelectrode conditions

in piilsed converters are also being investigated. Preliminary mea­

surements of a converter with a tungsten oxide collector (T = 1425 K, E

T = 751 K, 0,25 tor r cesium, and l-3xim electrode spacing) have ^ 14 -3

shown maximtim electron densities of 2,8 x 10 cm and electron

temperatures below 3000 K. Relative line intensity measurements

indicate progressively less equilibrated excited state poptxlation den­

sities with decreasing energy levels. C. ENHANCED MODE CONVERSION EXPERIMENTS

Refined measurements were performed to determine surface

thermal deformation of a molybdenum lase r -mi r ror electrode during

heating. The apparatus (see Figure 11-3) allowed the splitting of a

l - m m beam from a He-Ne laser into two components and reflecting

one from the center of the electrode and the other from its edge.

These reflected light beams were observed as two spots on a screen

placed approximately 20 m away, Deforxnation of the electrode sur­

face is measured by the relative motion between these two spots. To

first order, this relative motion is independent of the thermal distor­

tion of the sample support s tructure. In a set of experiments with

electrode temperatures ranging up to 1675 K, maximum deformations -5 never exceeded 8 x 1 0 cm. This value is sufficiently low to allow

efficient operation of close-spaced diodes.

7

Page 12: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

7710-15

•SCREEN

20 METERS

MIRRORS BEAM SPLITTER

He~Nt LASER

\«8i-METAL BELL JAR

TO VACUUM SYSTEM

Figure I I - 3 . Exper imenta l Ar rangemen t for Surface Therm.al Deform.ation Measurement

8

Page 13: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

wi^ Thermo ^ Electron f I 1M p n f 1A I I f 1 fsj

III. CONVERTER DEVELOPMENT

A . LOW-TEMPERATURE CONVERSION EXPERIMENTS

1. Tungsten E m i t t e r , Sprayed Lanthanum Hexaboride Collector

(Converter No, 180)

This var iab le -spac ing device employs a specially gxiarded col­

lec tor s t ruc tu re (see F igure I I I - l ) in o rder to de termine m o r e a c c u r ­

a te ly the work function of i ts sprayed lanthanum hexaboride surface

a t low cu r r en t l eve l s . Plots of col lector work function v e r s u s T /T^^

const ructed f rom re tard ing inode data show good cor re la t ion with dc

back-emiss ion v a l u e s . Work functions a s low as 1.45 eV were ob­

tained at T ^ / T values between 1.4 and 1.5 from re tarding plots

C R

(see F igure 111-2). At tempts to introduce l ow-p re s su re oxygen past

the cesixrm r e s e r v o i r , in o rde r to reduce the col lector work function,

have been unsuccessful . Work is cur ren t ly under way with higher

p r e s s u r e s of oxygen.

B . HIGH-EFFICIENCY CONVERSION EXPERIMENTS

1, Tungsten E m i t t e r , Sintered Lanthanum Hexaboride Collector

("Showerhead" Conver ter No. 166)

Measuremen t s of the effects of oxygen diffusion through the porous

LaB/ col lec tor were continued. Oxygen penetrat ion was observed to

init ial ly deignite the conve r t e r . Pumping on the back of the porous

co l lec tor would subsequently re igni te i t . The saturat ion cu r r en t of

the conver te r was always a factor of 2 to 3 g rea t e r than p r io r to the

oxygen dose . However, this inc reased performance would not l as t

m o r e than 20 to 30 m i n u t e s . Eventual ly the conver ter could not be

9

Page 14: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

7510-IOA

COLLECTOR FEEDTHROUGH

COLLECTOR

COLLECTOR INSULATION CERAMIC

SEAL

FLEXIBLE BELLOWS

EMITTER FLANGE

EMITTER SLEEVE

OUTGASSING TUBE

/ EMITTER ^WITH PYROMETER AND

THERMOCOUPLE HOLES TO CESIUM RESERVOIR

Figure I I I - l . Schematic of Guarded Conver ter

Page 15: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

2.2

2.0

:0N

(eV

) CD

o 1.6 z

cr il.4 QC O 1 -

i i i . 2 o o

1.0

__

+ \ s +

\

'BACK EMISSION M~800K ® - 7 5 0 K X - 7 0 0 K + - 6 5 0 K • - 600K

X X X

1

i

J^ ^

t r CONVERTER NO. 180 SPRAYED La Be COLLECTOR

1

® ®

7710-2

®

M

'

1.4 L8 2.0 22

T/Tr

Figure 111-2. Work Function of Sprayed Lanthanum Hexaboride Collector Ve r sus T / T R

Page 16: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

r p Thermo f/C Electron ( I 1 w R n R A r I C) N

ignited under any condit ions, and it was assumed that a l l the ces ium

had become oxidized. In fact, when the cesiuin r e s e r v o i r was slowly

heated up to 1000 K, no ignition was possible; the conver te r was taken

off t es t and was Auger analyzed.

A new LaB/ "showerhead" conver te r is being designed with a

window to pe rmi t spec t roscopic ana lyses of the oxygen diffusion

p r o c e s s e s ,

2, Lanthanum Hexaboride E m i t t e r , Guarded Nickel Collector

This conver te r is essen t ia l ly a repea t of No. 168 with a gxiarded

nickel col lector (see F igure i n - 3 ) , The problem with Converter

No, 168 was that the cu r r en t from the tungsten cup could not be

separa ted f rom the cu r r en t frora the LaB , emi t te r s lug. The guarded

col lec tor should al leviate this p rob lem in that the cu r r en t from the

tungsten shoxild flow to the gxiard, whereas the cu r r en t from the LaB . o

slug shoxild flow to the col lec tor button. The construct ion of this

conver t e r is near ly completed.

12

Page 17: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

7711-6

GUARD

COLLECTOR

COLLECTOR INSULATION

KOVAR SLEEVE

SAPPHIRE WINDOW

EMITTER HOHLRAUM

SPACING PAD

COLLECTOR FEEDTHROUGH

0.004 SPACING LaBg EMITTER ELECTRODE

RHENIUM WIRE SUPPORT TUNGSTEN EMITTER BODY

Figure 111-3, LaB, Emitter, Guarded Nickel Collector Converter

Page 18: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

m» Thermo f/c. Electron ( ( ] n p) n n A I I n f^j

IV, COMPONENT HARDWARE PROGRAM

A, CVD COMPONENT DEVELOPMENT

The f i r s t f ree-s tanding si l icon carbide-graphi te- tungs ten com­

posite hot shel l has been fabr ica ted. This shel l , shown in F igure

I V - 1 , m e a s u r e s 9. 53 cm in length by 2. 54 cm in d i ame te r . The

tungsten and graphite l aye r s have uniform th icknesses of 0.02 cm

and 0,1 cm, respec t ive ly . The si l icon carbide outer layer is 0 ,28 cm

thick at the he in i spher ica l end and 0.05 cm throughout the cyl indrical

por t ion . Design studies a r e in p r o g r e s s to determine a method to

grow g r e a t e r th icknesses of s i l icon carbide at the round end, and to

es tab l i sh a hydrogen purge to the inside of the shell during CVD of

the si l icon ca rb ide . The hydrogen purge is n e c e s s a r y to maintain the

in te rna l tungsten deposit free f rom t r a c e amounts of silicon ca rb ide .

The t e m p e r a t u r e and flow r a t e set t ings of the tungsten CVD

appara tus have , for the t ime being, becoine es tabl ished. Tungsten

she l l s , which a r e 0,05 cm thick at the open end and 0 ,04 cm thick

at the round end, a r e now routinely formed after an 85-minute expo­

s u r e to a 150-SCCM flow of tungsten hexafluoride.

A capabili ty for producing composite hot shells has been demon­

s t r a t ed . The CVD hot shel l effort of the component ha rdware p r o ­

g r a m wil l now be directed along the l ines of establishing routinely

reproducib le fabrication p r o c e s s e s .

B . ALLOY HOT SHELL DEVELOPMENT

Simulated furnace test ing continued at a furnace gas t empera tu re -7

of 1573 K. The inside of each shel l is evacuated to 10 t o r r . Table

IV-1 p r e s e n t s the status of these t e s t s as of November 2, 1977, A

14

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w

• ; • • • » • • • ' .

.-. -ilrWtel

7710-17

F igure I V - 1 . Composite CVD Silicon Carbide and Tungsten Emi t t e r Subassembly

15

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TABLE IV-1

SIMULATED FURNACE TESTS (November 2, 1977)

TEST P O R T NO,

1

2

3

4

5

6

HOT S H E L L

REACTION BONDED SILICON CARBIDE

KANTHAL A !

KANTHAL A l

INCONEL 671

CHROMIZED STAINLESS S T E E L 446

KANTHAL A l

T E S T HOURS

14 ,213

12.626

12,492

5 , 6 6 3

5, 172

2, 810

COMMENT

LEAKTIGHT THIS HOT S H E L L WAS BRAZED TO A M O L Y B ­DENUM S L E E V E WITH N I C K E L - C O P P E R

LEAKTIGHT

LEAK OBSERVED REMOVED 3 ! Oct . 77

LEAKTIGHT

LEAK OBSERVED

LEAKTIGHT

DATE OF TEST INITIATION

9 A p r i l 75

25 Aug. 75

9 Sept . 75

17 Nov. 76

17 Nov. 76

7 May 77

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»y^ Thermo • ' . - • • f/^ Electron { ( ) H P D F ^ A T I O N

leak was observed on the Kanthal A-1 sample on October 31 , 1977,

This shell has been removed from the furnace for failure ana lys i s .

Two additional hot shel ls were placed on tes t on October 31, 1977.

Both of these shel ls were del ivered to Thermo Elec t ron on October

6, 1977 in connection with Subcontract 7070-4190-411-Mod #3 , The

samples were mounted a s follows;

Tes t P o r t No, 3: 446 CRES P l a s m a a r c sprayed with n ichrome, 0. 01 to 0. 02 cm thick and difftised for 8 hours at 1367 K in a hydrogen a tmosphe re .

Tes t P o r t No. 5; 446 CRES P l a s m a a r c sprayed with Cr O , 0.01 to 0.02 cm thick.

Both samples had 2. 54 c m inside d i a m e t e r s , 0, 38 cm wall th icknesses

and were 20, 3 cm long. The end caps were TIG welded. The asseanbly

was s t r e s s re l ieved for one hour at 1256 K and a i r cooled.

17

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m» Thermo W^ Electron r I J M p n ^̂ A ! I c) NI

V. COMBUSTION-HEATED THERMIONIC DEVICE

The objective of this t ask is to design, construct , and tes t a

f lame-heated thermionic device for eventual use in combustion-heated

pane l s . The f i r s t step in this development will be the construct ion and

f larae-heated t e s t of a "miniature device" employing the mos t promis ing

m a t e r i a l s in s izes that a r e readi ly avai lable . The next step wil l be the

fabricat ion of a l a r g e r "workhorse device^ " which will be evaluated in

a t e s t furnace that provides coinbustion p a r a m e t e r s s imi la r to tih.ose in

fossi l - fuel powerplants . The data and experience with the minia ture

and workhorse devices wil l then be factored into a l a rge r "prototype

d e v i c e . "

The design of the min ia ture device (see Figxire V-1) in tegra tes

the r e su l t s of the al loy hot shel l development at TRW with the va r i ab le -

spacing diode t e s t s a t T h e r m o E lec t ron . To date , the mos t promising-

m a t e r i a l for alloy hot shel ls is INCONEL 671. This high chromium

nickel aUoy has shown good stabil i ty in s h o r t - t e r m t e s t s a t TRW and

a l so in a l ong - t e rm t e s t in the Simulated Furnace Faci l i ty a t The rmo

E lec t ron .

The hot shel l d imensions a r e determined by readi ly available

INCONEL 671 tubing (nominally 2. 54 c m in d i ame te r ) . The effective a r ea 2

of the conver te r is 2, 0 cm and is de termined by the maximum d iam­e te r of the col lector that can be inse r ted into the emi t te r hot shell without shor t - c i r cu i t ing .

The L605 emi t t e r m a t e r i a l was chosen on the basis of the favor­

able data f rom the var iable spacing Converter No. 143. These data

were repor ted in the P r o g r e s s Repor t for August 1976.

18

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MOUNTING BRACKET

CESIUM RESERVOIR-

7710-4

MOLYBDENUM REINFORCEMENT RING'

NICKEL COLLECTOR

INCONEL WICK / EMITTER

:LLOWS WICK SUPPORT

INCONEL 671 HOT SHELL

Figure V - 1 . Miniature F lame-Hea ted Device

Page 24: Thermo Electron/67531/metadc1053825/...Thermo [ ' U i P n R A M O KJ K Electron Report No. TE4233/4237-60-78 NASA/DOE ADVANCED THERMIONIC TECHNOLOGY PROGRAM PROGRESS REPORT NO. 28

mf^ Thermo ^ Electron

In o rde r for the t empe ra tu r e drop through the collector s t ruc ture

to be min imized , a potassixim filled heat pipe is used in the collector

stejXL. A cooling fin, a n d / o r an axxxiliary hea te r , may be clamped to

the outboard end of the col lec tor for diagnostic tes t ing .

The hea t source for heating the emi t t e r of the device will be a

gas t o r c h . A p r o p a n e / a i r , or propane/oxygen, torch will be used

in the init ial t e s t s .

Construction of the min ia ture device is in p r o g r e s s . Test resxilts

should be available next month .

20