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Proactive Strategies for Designing Thermoelectric Materials for Power Generation PNNL / ONAMI Joint Project on Advanced TE Materials & Systems Project ID #PM014 Dr. Terry J. Hendricks, P.E. 1 Professor Mas Subramanian 2 1 Hydrocarbon Processing Group, Energy & Environment Directorate Pacific Northwest National Laboratory Corvallis, OR 2 Department of Chemistry Oregon State University Corvallis, OR Office of Vehicle Technologies 2010 Annual Merit Review 10 June 2010 “This presentation does not contain any proprietary, confidential, or otherwise restricted information”
Transcript

Proactive Strategies for Designing Thermoelectric Materials for Power Generation

PNNL / ONAMI Joint Project on Advanced TE Materials & SystemsProject ID #PM014

Dr. Terry J. Hendricks, P.E.1 Professor Mas Subramanian2

1Hydrocarbon Processing Group, Energy & Environment DirectoratePacific Northwest National Laboratory

Corvallis, OR

2Department of Chemistry Oregon State University

Corvallis, OR

Office of Vehicle Technologies 2010 Annual Merit Review 10 June 2010

“This presentation does not contain any proprietary, confidential, or otherwise restricted information”

Agenda Overview – Timeline, Budget, Technical Barriers, &

Collaborations Objectives Milestones Technical Approach Accomplishments Collaborations & Coordination Future Work Summary Publications/Presentations Critical Issues

2

Proactive Strategies for Designing Thermoelectric Materials for Power Generation - Overview

Project Start Date: 15 December 2008 Project End Date: 15 December 2010 50% Complete

OVT Barriers – Advanced Combusion R&DSolid State Energy Conversion

Budget

Total FY 2009 Project Funding $260K Total FY 2010 Project Funding $260K

Improve heavy truck efficiency to 50 percent by 2015

Achieve stretch thermal efficiencies of 55% in heavy-duty engines by 2018 Fuel Economy Increases of 10% over 2010 Improve Cost-Effectiveness & Performance of Exhaust

Heat Recovery

Achieve at least a 17 percent on-highway efficiency of directly converting engine waste heat to electricity

Improve Light-Duty & Commercial Vehicle Fuel Efficiency up to10%

High-Performance Waste Energy Recovery Materials to Integrate into Advanced Engines

Methods for Maintaining Fuel Economy at Light-Load

Partners Lead: Pacific Northwest National Laboratory Partner: Oregon State University, Corvallis, OR ONAMI

Timeline

RxCo4Sb12

National Waste Energy RecoveryMagnitude of the Opportunity – Why Are We Interested?

4

60-70% Energy Loss in Most of Today’s Processes Transportation Sector

Light-Duty Passenger Vehicles + Light-Duty Vans/Trucks (SUVs)2002: 129.8 billion gallons of gasoline 2004: ~135 billion gallons of gasoline

~ 4.5 quads/yr exhausted down the tail pipe~ 5.5 quads/yr rejected in coolant system

Heavy-Duty Vehicles2002: 29.8 billion gallons of diesel2004: 32 billion gallons of diesel

~1.45 quads/yr exhausted down the tail pipe~1 quad/yr rejected in coolant system (~1 quad)

Hybrid Electric VehiclesMove Toward Electrification – Micro, Mild, and Full

Needs for Power GenerationNeeds for Electric-Driven Cooling

Project Objectives Develop new high-performance n-type and p-type thermoelectric

(TE) material compositions to enable: 10% fuel efficiency improvements from waste energy recovery in advanced light-

duty engines and vehicles. Heavy truck efficiencies to 50% by 2015 Stretch thermal efficiencies of 55% in advanced heavy-duty engines by 2018. Achieve 17% on-highway efficiency of directly converting engine waste heat to

electricity

Improve cost-effectiveness and performance of exhaust heat recovery in light- and heavy-duty vehicles.

Develop TE materials with operational temperatures as high as 800 K to 900 K.

Advanced n-type and p-type bulk TE materials that have peak ZT (Figure of Merit xTemperature) of approximately 1.6 or higher at 600 K

Minimize temperature-dependency in properties to achieve high performance in the 350 K to 820 K range.

Schedule / Milestones

6

Month/Year Milestones:

Dec. 2009–Dec. 2010 P-type and n-type Thermoelectric Development & Testing. Optimize Compositions for TE Performance. Measure TE Properties (Seebeck Coefficient, Electrical Resistivity, & Thermal Conductivity). On-going throughout the year due to third-party validation .

July 09 Select p-type TE Materials for Structural Testing. Criteria Will Be Selecting the Best TE Materials Properties (ZT vs. T.). Continue Refining n-type In0.2Ce0.15Co4Sb12 for Reproducibility

Dec. 2009–Dec. 2010 Continue Measuring & Categorizing Room Temperature Structural Properties of p-type & n-type TE Materials. Measure E, ν, CTE.

June 2010 Measure High Temperature Structural Properties of n-type TE Materials.

September 2010 Measure High-Temperature Structural Properties of p-type TE Materials

December 2010 Develop and Measure TE Couple Performance Using Selected p-type / n-type TE Materials. Measure I-V Curves at Various Hot-Side / Cold-Side Temperatures.

Technical Approach Power Generation in Light-Duty & Heavy-Duty Applications

Requires TE Materials in the 350 K to 820 K Range

T

Z*T vs. Temperature forVarious n-type TE Materials

LAST

Z*T vs. Temperature forVarious p-type TE Materials

LAST

Single and Multiple Rattlers

Co4Sb12 (n-type)

Rh4Sb12 (p-type)

RxCo4Sb12

RxR’yCo4Sb12

RxCo4-zRhzSb12

RxR’yCo4-zRhzSb12

Strategies in Designing n-type and p-type Skutterudites: RxRy’Co4-xMxSb12

Multiple Rattler Systems Dramatically Reduce Thermal Conductivity While Maintaining Electrical Conductivity & Seebeck Coefficient Single Rattler Systems

Multiple Rattler Systems

R2+: Ba, Ce, Sr, Ca, Ag, Pd,

R3+: La, Ce, Pr, Nd, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb, Lu, In, Sc

Technical Approach Proactive, Systematic Investigation of Dual- & Tri-Rattler Skutterudites

Refine n-type Materials, Characterize at Higher Temperatures & Transition to TE Couple Systematically Develop p-type Materials with Performance Similar to n-type Levels

TE Property Measurements @ OSU Laboratories Seebeck Coefficient Measurements vs. T Electrical Conductivity Measurements vs. T Thermal Conductivity Measurements vs. T

Engaging Third-Party Validation ORNL

Structural / Thermal Property Measurements @ PNNL Resonant Ultra Sound Techniques (E, ν) Up to 300 °C CTE Up to 400 °C Mechanical Strength @ Room Temperature

Recognition That Structural Properties Just as Important as TE Properties

PNNL to Characterize System-Level Benefits of Material Compositions in Waste Energy Recovery Applications (See Supplemental Slides)

Demonstrate High-Performance TE Couples for Transition to Waste Energy Recovery Applications

Project Accomplishments

Structural Property Measurements Measured Coefficient of Thermal Expansion & Determined Elastic

Material Properties Over Elevated Temperatures Measured Coefficient of Thermal Expansion Modified Existing RUS System for Material Property Measurement at

Elevated Temperatures Currently Measuring E and ν at Multiple Temperatures Spanning Room

Temperature to 300 ºC RUS Systems

Room Temperature Shown Right High-Temperature System in Next Charts

Specimen between

Transceivers

Elastic Moduli Estimate by Resonant Ultrasound Spectroscopy: High Temperature Test Chamber

Argon gas inlet

Gas preheat

High temperature wire for three resistive cartridge heaters

Gas diffuser

High temperature RUS transducers

Primary components and fittings are stainless steel.

Upper fixture with fixed transducer

Lower fixture

Resistance temperature detector (RTD) sensor access

Elastic Moduli Estimate by Resonant Ultrasound Spectroscopy: High Temperature Transducers

Vespel ® cylinder (6.6-mm outer diameter)

High temperature coaxial cable (not shown)

Silver epoxy(EPO-TEK® E2116-5)

Inner cavity filled with high temperature epoxy (Aremco-Bond 526N-ALOX-BL-A & B)

Stainless steel tube

Transducer lead wires

PNNL Fabricated High-Temperature Transducers

30-MHz, lithium niobate crystal (2.0-mm diameter active center)

14

Thermal Chamber

Temperature Controller

Assess to Specimen and Transducers

RUS Transducer

RUS Transducer

Power Switch to Thermal Cartridges

QuasarRI-2000

Computer Control of

RUS System

Reference (Fused Silica RPP) in Thermal Chamber

Argon Gas Feed

RUS High Temperature Measurement System

n-Type InxCeyCo4Sb12 TE Properties InxCeyCo4Sb12 Created Using Sintering & Hot-Pressing Processes

Moderate Hot-Pressing Pressures (50 MPa)

-210

-200

In0.15Ce0.1Co4Sb12 HUP 50MPa

In0 1 Ce0 1Co4Sb12 HUP 50MPa 675oC/4Hr

In0.15Ce0.1Co4Sb12 HUP 50MPa "Light" SampleSeebeck

0 000024

0.000025

0.000026

In0.15Ce0.1Co4Sb12 HUP 50MPa "Light" SampleResistivity

-240

-230

-220

In0.15Ce0.1Co4Sb12 HUP 50MPa 675 C/4Hr

In0.15Ce0.1Co4Sb12 HUP 50MPa (675oC/4Hr)*2

eck,

V/

K

0.000019

0.000020

0.000021

0.000022

0.000023

0.000024

vity

, m

-270

-260

-250Seeb

e

0.000014

0.000015

0.000016

0.000017

0.000018

0.000019

In0.15Ce0.1Co4Sb12 HUP 50MPa

In0.15Ce0.1Co4Sb12 HUP 50MPa 675oC/4Hr

In Ce Co Sb HUP 50MPa (675oC/4Hr)*2R

esis

tiv

300 350 400 450 500 550 600 650

Temperature, K

300 350 400 450 500 550 600 6500.000013

In0.15Ce0.1Co4Sb12 HUP 50MPa (675 C/4Hr) 2

Temperature, K

n-Type InxCeyCo4Sb12 TE Properties InxCeyCo4Sb12 Created Using Sintering & Hot-Pressing Processes

Moderate Hot-Pressing Pressures (50 MPa) High Power Factors Exhibited in In0.15Ce0.1Co4Sb12 Compounds

0 0038

In0.15Ce0.1Co4Sb12 HUP 50MPa "Light" SamplePower Factor

Fairly Insensitive to Temperature From 350 – 550 K

0 0033

0.0034

0.0035

0.0036

0.0037

0.0038

K2 )-1

0.0029

0.0030

0.0031

0.0032

0.0033

wer

Fac

tor W

(mK

300 350 400 450 500 550 600 650

0.0025

0.0026

0.0027

0.0028In0.15Ce0.1Co4Sb12 HUP 50MPa

In0.15Ce0.1Co4Sb12 HUP 50MPa 675oC/4Hr

In0.15Ce0.1Co4Sb12 HUP 50MPa (675oC/4Hr)*2

Pow

Temperature, K

n-Type InxCeyCo4Sb12 TE Properties Ultimately Led to ZT ~ 1.5 – 1.6 at 425 – 525 K for In0 2Ce0 15Co4Sb12y 0.2 0.15 4 12

Compounds Once Again – Bulk Materials Easily Integrated into TE Device

0.007

0.008 In0.15Ce0.1 In0.15Ce0.15 In0.2Ce0.15 2.3

2.4

2.5

In0.15Ce0.1 In0.15Ce0.15 In0.2Ce0.15

0.004

0.005

0.006

(W/m

K2 )

2.0

2.1

2.2

(W/m

K)

0.002

0.003

PF

1.7

1.8

1.9 (

300 350 400 450 500 550 600 650

0.001

T (K)300 350 400 450 500 550 600 650

1.6

T (K)

n-Type InxCeyCo4Sb12 TE Properties Ultimately Led to ZT ~ 1.5 – 1.6 at 425 – 525 K for In0 2Ce0 15Co4Sb12y 0.2 0.15 4 12

Compounds Once Again – Bulk Materials Easily Integrated into TE Device Must Monitoring MicroCracking

1 6

1.8

2.0

In0.15Ce0.1 In0.15Ce0.15In0 2Ce0 15

g g

1.2

1.4

1.6 In0.2Ce0.15

0 6

0.8

1.0 ZT

0.2

0.4

0.6

300 350 400 450 500 550 600 650

T (K)

n-Type Thermoelectric & Structural PropertiesResonant Ultrasound Spectroscopy

Preliminary Data E,Preliminary DataSpecimen Label and Comments

Temperature (ºC)

, density(g/cm3)

,Poisson's

ratio

Modulus of Elasticity(1011 N/m2)

rmserror (%)

In0.15Ce0.1Co4Sb12 - LBL17 3032-5-2010 --- 7.303 0.215 1.348 0.12

In0.15Ce0.1Co4Sb12 - LBL13-9-2010 20.6 7.303 0.204 1.344 0.33

In Ce Co Sb LBL2In0.15Ce0.1Co4Sb12 – LBL22-9-2010 --- 7.264 0.204 1.326 0.49

In0.15Ce0.1Co4Sb12 – LBL23-10-2010 21.5 7.264 0.200 1.319 0.40

In0.15Ce0.1Co4Sb12 – PNNL3-G1B 1-21-2010 --- 7.315 0.181 1.339 ---

In0.15Ce0.1Co4Sb12 – PNNL3-G1B 2 05 2010 Repeat 1 21 2010 --- 7.315 0 185 1 339 ---2-05-2010 Repeat 1-21-2010 --- 0.185 1.339 ---

In0.15Ce0.1Co4Sb12 – PNNL3-G1B 3-25-2010 20.8 7.315 0.194 1.358 0.78

In0 2Co4Sb12 – NM211_3-5-10

19

0.2 4 12 _3-30-2010 - BNW-60608 – 15 --- 5.694 0.185 0.666 0.34

n-Type Thermoelectric & Structural PropertiesResonant Ultrasound Spectroscopy

Preliminary Data EPreliminary DataSpecimen Label and Comments

, density(g/cm3)

,Poisson's

ratioCTE (/°C)

E,Elastic Modulus

(1011 N/m2)ZT

(@ 600 K)

CoSb3 (literature) 0.222 1.396 0.6

La0.75CoFe3Sb12 (literature) 0.228 1.365

CoSb3 (PNNL) 0.226 12.8x10-6 1.398

CoSb3 (PNNL) 0.225 1.391

In0.1Co4Sb12 (PNNL) 0.227 8.37x10-6 1.396

Y0.1In0.1Co4Sb12 (PNNL) 0.247 9.26x10-6 1.413 0.82In0.15Ce0.1Co4Sb12 – PNNL3

1 21 2010 hi ff~7.314 0.181 1.339

1-21-2010 --- chip off corner

In0.15Ce0.1Co4Sb12 – PNNL3

2-5-2010 --- REPEAT of 1-21-2010

~7.314

0.185

8.61x10-61.339

0.95

In0.15Ce0.1Co4Sb12 - LB1

2-5-20107.304 0.215

8.56x10-61.348

0.95

In0.15Ce0.1Co4Sb12 - LB2

2-9-20107.264

0.204

8.26x10-61.326

0.95

20

In0.2Ce0.15Co4Sb12 - 03161035

4-13-2010 (Preliminary Data) 7.019

0.105

8.11-8.34x10-6 1.0661.4

(1.5-1.6 @ 475K)

Resonant Ultrasound Spectroscopy (E, ν) MeasurementsThermal Cycling Effects

Thermal Fatigue Cycling Showing Good Stability 200 Cycles

40 °C to 400 °C

Good Indicator of Reliability in Future TE Modules

Temperature [°C]

Before Thermal Cycling After Thermal Cycling Young’s

Modulus, E X 109 [N/m2]

Poisson’s Ratio, ν

Young’s Modulus, E X 109 [N/m2]

Poisson’s Ratio, ν

In0.15Ce0.1Co4Sb12 (LBL1)

20-22 134.8 0.215 134.4 0.204

In0.15Ce0.1Co4Sb12 (LBL2)

20-22 132.6 0.204 131.9 0.200

In0.15Ce0.1Co4Sb12 (PNNL3-G1B)

20-22 133.9 0.185 135.8 0.194

p-Type Co1-xRhxSb3 (without Rattlers): High Temperature Power Factor

Power Factor Temperature Dependency for p-type x= 0.6 sample x = 0.6 was optimum composition

Higher Power Factor, But Costs Too High as Pointed Out @ 2009 OVT Merit Review

Reported Last Year, But Work Discontinued Due to Cost & κ

300 350 400 450 500

2

3

4

5

6

7

Pow

er F

acto

r µ W

/K2 -c

m

Temperature(K)

Co0.4Rh0.6Sb3

High Temperature Power Factor Data

S.No Compound ZT Ref1 LaFe4-xCoxSb12 0.9 at 800 K B. C. Sales, D. Mandrus, and R. K.

Williams, Science 272, 1325 (1996)2 CeFe4-xCoxSb12

x < 3 p-typex > 3 n-type

0.7 at 800 K;1.2-1.4 at 900 K

J.-P. Fleurial, T. Caillat, A. Borshchevsky, D. T. Morelli, and G. P. Meisner, in Proceedings of the 15th International Conferenceon Thermoelectrics(1996) 91

3 Ce0.28Fe1.5Co2.5Sb12 1.1 at 750 K Tang, Xinfeng; Zhang, Qingjie; Chen, Lidong; Goto, Takashi; Hirai, Toshio., Journal of Applied Physics (2005), 97(9) 093712/1-093712/10

4 Ba0.27Fe0.98Co3.02Sb12 0.9 at 750 K Tang, X. F.; Chen, L. D.; Goto, T.; Hirai, T.; Yuan, R. Z., Journal of Materials Research (2002), 17(11), 2953-2959

5 Ca0.18Ce0.12Fe1.45Co2.55Sb12 1.2 at 750 K Tang, Xinfeng; Li, Han; Zhang, Qingjie; Niino, Masayuki; Goto, Takashi.Journalof Applied Physics (2006), 100(12), 123702/1-123702/8

p-Type Skutterudites with High ZT p-Type Skutterudites Quite Difficult to Produce Very Few Dopents Act as Electron Acceptor from the Co-Sb Conduction Band Following Compounds are Guiding Our p-Type Investigations Reproducibility of Compounds Below Has Not Been Confirmed

ZT of ~0.2 is obtained for In0 2Co3FeSb12 at 623 K

p-Type Skutterudites To Date0.2 3 12

0.01450.01500.0155

0.20Fe1

0 01150.01200.01250.01300.01350.0140 Fe05

In02Fe05 In02Fe1 Fe1

K) 0.14

0.16

0.18

0 00900.00950.01000.01050.01100.0115

(W

/cm

0.10

0.12Fe0.5

ZT

0 50 100 150 200 250 300 350 400

0.00750.00800.00850.0090

T (C)0.00 0.05 0.10 0.15 0.20

0.06

0.08 Fe1

Fe0.5

IT (C) In conc

ZT of ~0.2 is obtained for In0.2Co3FeSb12 at 623 K

p-Type Skutterudites To Date

p‐Type LAST Materials Could be Combined with n‐Type In‐Ce Based Skutterudites to Demo TE Couple Well‐Developed Thermoelectrically & Structurally  (Tellurex Corp., 2009) Demonstrated in TE Modules  (Tellurex Corp., 2009) ZT = 1.2 @ 750 K 

2Na

0 95Pb

20SbTe

22p-type Ag

0.9Pb

9Sn

9Sb

0.6Te

20 (100g)

1.5

T

BixSb

2–xTe

3

0.95 20 22

Zn4Sb

3

Ag0.5

Pb6Sn

2Sb

0.2Te

10

CeFe4Sb

12

(AgSbTe2)0.15

(GeTe)0.85

Ce Fe Co Sb

nanoBi

xSb

2–xTe

3

0.5

1ZT

x 2 x 3

PbTeYb

14MnSb

11

Ce0.28

Fe1.5

Co2.5

Sb12

Ag Pb Sn Sb Te

0400 600 800 1000 1200

Temperature (K)

Ag0.9

Pb9Sn

9Sb

0.6Te

20

This SERDP Project(shown green bold)

Temperature (K)

Partners Oregon State University, MicroProduct Breakthrough

Institute Oregon Nanoscience & Microtechnology Institute Oak Ridge National Laboratory – Validation Testing

Technology Transfer Tellurex Corporation BSST LLC ZT Plus

Coordination with OVT Waste Heat Recovery & Utilization Project

Collaboration and Coordination with Other Institutions

Future Work & Path Forward

Optimize Synthesis Procedures for n-type (In,R)Co4Sb12 Compositions Good Reproducibility Fabricating Highly Dense Samples

Introduce Single & Multiple “Rattlers” (In, Rare Earth) in FexCo4-xSb12 , (i.e., Iny FexCo4-xSb12 ; Cey FexCo4-xSb12 ) For Better p-Type Materials

Characterize TE Properties & Validate with Third Party Testing (ORNL) Structural Property Measurements

Young’s Modulus, E(T) Poisson’s Ratio, ν(T) CTE(T) Mechanical Strength

Transition to TE Couples & Measure Performance

Summary Results

n-type Skutterudite TE Materials Showing Excellent TE Properties (See Publication) p-type Skutterudite TE Materials Are More Challenging Structural & CTE Testing On-Going; Good Structural Stability Upon Thermal Cycling High Temperature Structural Test Equipment Operational & Calibrated

Challenges Batch to Batch ZT Reproducibility and Consistent Properties Sintering to High Dense Samples

Continue Evaluating Stability Issues During Thermal Cycling Benefits

System-Level Analyses Show OSU/PNNL Skutterudites Superiority (See Supplements) Higher Performance Than TAGS / PbTe Combinations & Other Skutterudite

Combinations TE Conversion Efficiencies Can Be High

9-10% in Automotive Applications in Preferred TE Design Regions 11-12%+ in a Direct-Fired APU System Potential Superiority to Other Materials in Automotive TE Systems

Bulk TE Materials for Easy Integration into TE Module / System Designs

24

Questions & Discussion

We are What We Repeatedly do. Excellence, Then, is not an Act, But a Habit.

Aristotle

AcknowledgementWe sincerely thank Jerry Gibbs, Office of Vehicle Technologies Propulsion Materials, for his support of this project.


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