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1 Thrust 1 Technical Overview Jim Szybist (ORNL), Dan Gaspar (PNNL) September 14, 2016

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Page 1: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

1

Thrust 1 Technical OverviewJim Szybist (ORNL), Dan Gaspar (PNNL)

September 14, 2016

Page 2: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

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Thrust 1 Approach

• From biomass to blendstock

• Blendstock properties• Fuel properties and

engine performance• Advanced spark ignition

engine performance

Page 3: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

3From biomass to blendstocks - spark ignition candidates identified

• Identified 9 molecular classes suitable for further evaluation• Paraffins (especially highly branched paraffins), olefins,

cycloalkanes, aromatics, alcohols, furans, ketones, ethers, and esters

• Developed list of candidates from these classes based on:• Open literature sources• Ongoing National Laboratory research• Proposed plausible pathways from biomass to spark ignition

blendstocks

• Constructed tiered screening process based on fuel merit function, including expected optimal values for properties

Page 4: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

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Fuel selection “funnel”

Page 5: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

5

• Applied tiered screening process >400 potential candidates in Fuel Property Database to generate ~40 candidates*

• Focused on high octane components (>98 RON) to enable downsized, down-speeded, boosted SI engines

• Other criteria included:• Soluble in hydrocarbon• Not OSHA known or suspected human carcinogen or

reproductive toxin• Biodegradation via EPA’s BIOWIN (coupled to water

solubility)• Boiling point <165 oC and freezing point <10 oC• Low expected corrosivity

Page 6: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

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Thrust I candidates meeting Tier 1 criteriaAlcohols Aromatics EthersEthanol (reference only) 1,3,5-trimethylbenzene (mesitylene) Methoxybenzene (anisole)Methanol Vertifuel (60%+ aromatics)n-Propanol Fractional condensation of sugars plus upgrading Furans2-Propanol Methanol-to-gasoline 2-Methylfuran1-Butanol Catalytic fast pyrolysis 2,5-Dimethylfuran2-Butanol Catalytric conversion of sugars 40/60 Mixture of 2-methylfuran/2,5-

dimethylfuran2-Methylpropan-1-ol (isobutanol)2-Methylbutanol Esters Ketones2-Methyl-3-buten-2-ol Acetic acid, methyl ester (methyl acetate) 2-Propane (acetone)2-Pentanol Butanoic acid, methyl ester (methyl butyrate) 2-Butane (methylethylketone; MEK)Guerbet alcohols Pentanoic acid, methyl ester (methyl pentanoate) 2-Pentanone

2-Methylpropanoic acid, methyl ester 3-PentanoneAlkanes 2-Methlybutanoic acid, methyl ester CyclopentanoneIsooctane Acetic acid, ethyl ester (ethyl acetate) 3-HexanoneHigh-octane gasoline blendstock(triptane rich)

Butanoic acid, ethyl ester (ethyl butanoate) 4-Methyl-2-pentanone (Methylisobutylketone; MIBK)

2-Methylpropanoic acid, ethyl ester 2,4-Dimethyl-3-pentanoneAlkenes Acetic acid, 1-methylethyl ester 3-Methyl-2-butanoneIsooctene (2,4,4-trimethyl-1-pentene) Acetic acid, butyl ester (butyl acetate)

Acetic acid, 2-methylpropyl ester Multifunctional MixturesAcetic acid, 3-methylbutyl ester Methylated lignocellulosic bio-oilAnaerobic acid fermentation plus esterification

Page 7: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

7

Selected 20 candidates for analysis from Tier 1 list

Selection based on practical considerations:• Clear production pathway with balance between

production approaches• Cover the chemistry/functional group space• Series of candidates within alcohols and esters

which provide some systematic variation of structure

Page 8: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

820 ASSERT Molecules/Mixtures0 Ethanol (Reference)1 Methanol2 1-butanol3 2-methyl-butanol4 2-butanol5 Isobutanol (2-methylpropan-1-

ol)6 Guerbet alcohol mixture 7 2,5-dimethylfuran/2-

methylfuran mixture8 Acetic acid, methyl ester

(methyl acetate)9 Acetic acid, ethyl ester (ethyl

acetate)10 Acetic acid, butyl ester (butyl

acetate)

11 Anaerobic acid fermentation and esterification mixture

12 2-pentanone

13 Methylethylketone (2-butanone)

14 2,2,3-trimethyl-butane

15 Isooctene

16 Vertifuel (60%+ aromatics)

17 Fractional condensation of sugars + upgrading

18 Methanol-to-gasoline

19 Catalytic fast pyrolysis

20 Catalytic conversion of sugars

Page 9: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

Thank You

Page 10: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

The Central Fuel Hypothesis

If we identify target values for the critical fuel properties needed to maximize efficiency and emissions performance for a given engine architecture, then fuels with those properties and values will provide comparable performance.

Thrust I Engine Research

• Focused in next-generation SI engines

• Taking a fuel-property approach to new fuel candidates

*SI engines accounted for 72% of on-highway energy consumption in the U.S. in 2013. (Energy Transportation Data Book, 2015).

Assumptions Being Evaluated

1. Fuel properties correctly describe the fuel’s performance in modern SI engines.

2. Fuel property measurements are valid across a wide range of unconventional fuel chemistries

Page 11: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

11Merit Function Allows Individual Fuel Properties to be Valued

Thrust I Research Aims to Refine the Merit Function Terms

Merit = ∑ RON

(𝑹𝑶𝑵𝒎𝒊𝒙 − 𝟗𝟐)

𝟏. 𝟔

OctaneSensitivity

−𝑲(𝑺𝒎𝒊𝒙 − 𝟏𝟎)

𝟏. 𝟔

Heat of Vaporization

𝟎. 𝟎𝟏[𝑶𝑵/ 𝒌𝑱 𝒌𝒈] 𝑯𝒐𝑽𝒎𝒊𝒙 − 𝟒𝟏𝟓 [ 𝒌𝑱 𝒌𝒈]

𝟏. 𝟔

+𝑯𝒐𝑽𝒎𝒊𝒙 − 𝟒𝟏𝟓 [ 𝒌𝑱 𝒌𝒈]

𝟏𝟑𝟎

Flame Speed

(𝑺𝑳𝒎𝒊𝒙 − 𝟒𝟔𝒄𝒎𝒔

)

𝟑

Distillation

−𝑳𝑭𝑽𝟏𝟓𝟎

Particulate Emissions

−𝑯(𝑷𝑴𝑰 − 𝟐. 𝟎)[𝟎. 𝟔𝟕 + 𝟎. 𝟓(𝑷𝑴𝑰 − 𝟐. 𝟎)]

350 400 450

42 44 46 48 50HoV [ kJ/kg ]

Flame Speed [ cm/s ]

0 10 20 30

1.5 2 2.5 3LFV

150 [ % ]

PMI

-4-3-2-101234

88 90 92 94 96

4 6 8 10 12 14 16

Mer

it Fu

nctio

n

RON

Octane Sensitivity

For K = -0.5

350 400 450

42 44 46 48 50HoV [ kJ/kg ]

Flame Speed [ cm/s ]0 10 20 30

1.5 2 2.5 3LFV

150 [ % ]

PMI

-4-3-2-101234

88 90 92 94 96

4 6 8 10 12 14 16

Mer

it Fu

nctio

n

RON

Octane Sensitivity

For K = -0.5

-4-3-2-101234

88 90 92 94 96

4 6 8 10 12 14 16

Mer

it Fu

nctio

n

RON

Octane Sensitivity

For K = -0.5

350 400 450

42 44 46 48 50HoV [ kJ/kg ]

Flame Speed [ cm/s ]

0 10 20 30

1.5 2 2.5 3LFV

150 [ % ]

PMI

-4-3-2-101234

88 90 92 94 96

4 6 8 10 12 14 16

Mer

it Fu

nctio

n

RON

Octane Sensitivity

For K = -0.5

-4-3-2-101234

88 90 92 94 96

4 6 8 10 12 14 16

Mer

it Fu

nctio

n

RON

Octane Sensitivity

For K = -0.5

Page 12: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

Example 1: Clarifying the Effects of HoV on Knock Mitigation 12

• Inconsistencies in literature of HoVimpact on knock propensity

• HoV effect only been observed when covariant with octane sensitivity

• Expanded with new experimental results from ORNL and NREL

• Main conclusion: HoV is a thermal contributor to octane sensitivity

• Aligns the findings of seemingly contrary literature findings

• Consistent with the vaporization effects in the RON and MON tests

0

5

10

15

20

0 10 20 40 60 80 100

Oct

ane

Se

nsi

tivi

ty (

-)

Volumetric Ethanol Content (%)

Thermal Sensitivity ComponentChemical Sensitivity Component

0

5

10

15

20

25

30

0 500 1000 1500 2000

CA

50

[ a

TDC

f]

Brake Mean Effective Pressure [ kPa ]

RON 96.5 (24% Isobutanol)RON 96.6 (E20)RON 97.6 (30% Toluene)

Matched RON and S

Varying HoV

Page 13: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

13

Fuels show fixed RON and S with varying HoV

Data represents maximum load at constant combustion phasing

Further Research Shows that at Elevated Intake Temperatures, Impact of HoV is Different from that of S

10

12

14

16

18

20

30 40 50 60 70 80 90 100

Isooctane, DITSF 99.8, DIE40-TRF6x, DIE20+2%p-Cresol-TRF88, DI

IMEP

net

[ b

ar ]

Intake Temperature [ C ]

RON = 99.2-101.6S = 10.7-12.2

HoV

595 kJ/kg

472 kJ/kg

390 kJ/kg

RON = 100S = 0

Page 14: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

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PRFs Aren’t Representative Real-World Fuels

PRF’s are Paraffin

Exhibit 2-stage ignition that is unique when compared to most other fuels

The 2-stage ignition defines the octane number scale

Are RON and MON Still Applicable

Understanding of the beneficial nature of octane sensitivity is becoming accepted

With new bio-derived fuels, do RON, MON and octane sensitivity still have the same meaning?

CFR Engine Doesn’t Match Modern Engines

Fueling System

Carbureted vs. Direct injection

Air Handling

Naturally Aspirated vs. Boosted

Fixed Cam Position vs. Phasing

Combustion Phasing

Advanced vs. Late Phasing

Additional Mismatches

Example 2. Conditions of RON and MON Tests Raise Applicability Questions

Intake Temperature Engine Speed

Equivalence Ratio Knock Detection

Page 15: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

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Experiments show some fuels exhibit pre-spark heat release in stoich SI engines

• Boosted operating conditions

• Elevated intake temperatures

Combination of Experimental Investigations and Kinetic Modeling is Providing Insight into Meaning of RON and MON

600 650 700 750 800 850 900 950100005

10152025303540

Pres

sure

[ ba

r ]

Temperature [ K ]

2.0

3.0

4.0

5.0

6.0

7.0

RON MON

Condition C

Condition B

Condition A

Iso-Octane

Kinetic modeling is being used to understand the operating conditions in the temperature/pressure space

Page 16: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

16

Efficiency benefits of RON and MON

Improving HoV measurements for mixtures

Investigating the impact of HoV on engine performance

Lean and EGR dilution tolerance

Fuel impacts on particulate emissions

Fuel impacts on catalyst light-off temperatures

Fuel impacts on low speed pre-ignition

Findings from Thrust I investigations will feedback to test the central fuels hypothesis and to calibrate the merit function

-20 0 20 40 60 80 1000

25

50

75

100

125

150

175

200

Crank Angle (CA aTDCf)

Cyl

inde

r Pre

ssur

e (b

ar)

Average LSPI (cycle #116)

Spark timing

0.0

2.5

5.0

7.5

10.0

12.5

Spar

k Pr

imar

y C

oil S

igna

l (vo

lt)

Spark timing

Iso-octane N-heptane

Toluene

Ethanol

Methanol

0

10

20

30

40

50

60

40 45 50 55 60

Hea

t of V

apor

izat

ion

[kJ/

MJ]

LFS at 1atm, 358K [cm/s]

6 8 10 12 14 16 18 20 22

2

4

6

8

10

12

14

16

18

20

22

24

EGR

[%

]

CA50 [ CA aTDCf ]

1.0002.0003.0004.0005.0006.0007.0008.0009.000

COV of IMEP [ % ]

Additional Thrust I Research Areas Include

Page 17: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

Backup slides

17

Page 18: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

18

1 alcohol mixture

1 furan mixture

5 hydrocarbon mixtures

1 ester mixture

2 complex mixtures

The 20 includes a range of compositions and functional groups:

Single compounds

Simple mixtures

Complex mixtures

5 alcohols

3 esters

2 ketones

1 paraffin

1 olefin

Page 19: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

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Structural series within alcohols…

…and esters

Page 20: Thrust 1 Technical Overview - Department of Energy · PDF file · 2016-09-27Thrust 1 Technical Overview Jim Szybist(ORNL), ... Selected 20 candidates for analysis from Tier 1 list

20

Next steps

• Fill in process gaps as needed for ASSERT analysis• Examine blending behavior of subset of 20

• Distillation Properties via ASTM D86 in an RBOB; RVP from other methods

• Oxidation Stability via ASTM D525 in an RBOB • Blending RON and MON in a 4 component surrogate

w/ AKI about 88 or 89

Base fuel

Blended fuels@ multiple blending

ratios (10, 20, 30 vol%)

RON and MON in a 4 component surrogate RON and MON in a 4 component surrogate RON and MON in a 4 component surrogate Bio-

blendstocks: mixtures,

single compounds