development of materials for high energy batteries
TRANSCRIPT
Physical Sciences Inc. 20 New England Business Center Andover, MA 01810
Physical
Sciences Inc. VG11-193
Development of Materials for
High Energy Batteries
Christopher M. Lang (PI), Anna Cheimets and John D. Lennhoff
NASA Battery Workshop 2011
Huntsville, AL
November 15, 2011
SBIR Data Rights
Contract No.: NNX10CA51C
Contractor Name: Physical Sciences Inc.
Contractor Address: 20 New England Business Center, Andover, MA 01810
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Physical Sciences Inc. VG11-193
Outline
Metal Phosphate Coating for Improved
Cathode Material Safety
Funded by NASA Johnson Space Center and NASA
Glenn Research Center under contract #
NNC09CA04C. COTR: Dr. Judith Jeevarajan.
– Motivation and Coating Benefits
– Program Results
Electrochemical Performance of Silicon Whisker
and Carbon Nanofiber Composite Anode
Funded by NASA Glenn Research Center under
contracts NNX09CD30P and NNX10CA51C. COTR:
Dr. Richard Baldwin.
Summary and Next Steps
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Focus\Accomplishments for Year 2 of the Program
Application and scale-up of the coating developed in year 1 to NASA’s specified
mixed metal oxide cathode material (TODA MNC-9100) in order to support
evaluation in cells constructed by NASA’s commercialization partner.
Demonstration of the cycling and safety performance characteristics of the PSI
coated cathode material.
Optimized coating procedures for coating TODA cathode material.
Coating reduces exotherms observed on heating delithiated cathode material.
Coated cathodes demonstrated <1% loss in discharge capacity over 50 cycles at
a C/5 rate.
Demonstrated scale-up with construction of 1Ah pouch cells: – No reduction in discharge capacity or voltage observed.
– On abuse testing pouch cells utilizing coated cathode material demonstrated
improved stability.
Successfully scaled-up cathode coating to produce and deliver 1500grams of
coated cathode material.
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Problem:
Under abuse conditions, exothermic reactions between high voltage
cathode materials and the battery electrolyte can lead to catastrophic
failure.
Remediation Approach:
PSI formed lithium metal phosphate coatings on metal oxide cathodes
by thermal treatment of a mixture of metal phosphate and the cathode.1
Motivation
1PSI patenting pending process.
Cathode
LiMPO4
ThermalTreatment
Mx(PO4)y
J-8384
Cathode
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Coating is a lithium conductor.
Metal phosphates offer greater stability than their metal oxide
counterparts.
Coating technique can be applied to protect any high energy density
cathode material.
Common processing steps allowing for low cost manufacturing.
Benefits of the Lithium Metal Phosphate Coating
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Key Benefit: Cathode Surface Oxidation State
For high voltage cathode materials:
VMox (Oxidized Metal Potential) > VEl-limit (Stability limit of the Electrolyte)
Results in spontaneous oxidation of the electrolyte.
For coated material, the lithium metal phosphate layer remains in the
reduced form upon full charge.
Lithiated
Metal Oxide
Cathode
LiMxPO4
Discharge Charged
Delithiated
Metal Oxide
Cathode
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DSC Testing Technique
DSC (differential scanning calorimetry) tests were performed to demonstrate the effect of the coating on the thermal stability of the cathode material in its delithiated state.
Testing Technique:
Half-cells (with a lithium counter) were built using PSI’s puck cell fixture and charged to 4.8V at 12.5mA/g (a C/20 rate).
Cathodes were harvested and rinsed with DMC. DSC tests were performed after drying.
Small punches were taken from the cathode and sealed in the DSC pans.
All DSC pans were pre-run from 25-350°C at 5°C/min to provide a baseline.
Spring Loaded Puck Cell DSC Sample Pans
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Heat Flow vs. Temperature for Dry, Delithiated Uncoated and
Phosphate Coated TODA Cathode Material
Coatings adjusted to minimize phosphate content.
All exotherms are muted with exotherms for optimized sample of -1W/g or less.
Peak heights for initial coated sample exotherms are less than -2W/g.
Ramp at 5°C/min
Uncoated
Optimized Coating (Grey)
Coating A(Blue)
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C/20 Steady State Cycling Voltage Profile: Cycle 2
Discharge capacity of coated cells is 211 and 206mAh
Discharge capacity of uncoated cells is 208 and 204mAh
No observed difference in voltage trace
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2.8
3
3.2
3.4
3.6
3.8
4
4.2
4.4
4.6
0 50 100 150 200
Vo
ltag
e (
V v
s L
i+/L
i)
Capacity (mAh/g-cathode)
Coated
Coated
Uncoated
Uncoated
Cycle Testing: C/20Coated and Uncoated Full Cells vs.
CarbonVoltage Limits 4.6V and 2.8V
Celgard 2500 Separator1M LiPF6 in DEC/DMC/EC
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Variable C-rate Cycling of Coated TODA
Variation in capacities results from slight variation in anode to cathode ratios
Cells cycled on initial 26 cycle procedure and then for an additional 50 cycles at C/5
For each cell, capacity on cycle 76 is equal or higher than capacity on cycle 6
150
160
170
180
190
200
210
0 10 20 30 40 50 60 70 80
Cycle #
Dis
ch
arg
e c
ap
acit
y (
mA
h/g
-cath
od
e)
S-3
S-2
S-1
Cycle Testing
Coated Full Cells vs. Carbon
Voltage Limits 4.6V and 2.8V
Celgard 2500 Separator
1M LiPF6 in DEC/DMC/EC
Testing Restarted
C/20
C/10
C/5
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First Cycles for
Coated and Uncoated Pouch Cells
Pouch cells were conditioned at C/20 between 4.6 and 2.8V
First cycle efficiency is ~69% for each cell
Initial discharge capacity is consistent with coin cell experiments
2.8
3.2
3.6
4.0
4.4
4.8
0 200 400 600 800 1000 1200 1400 1600
Capacity (mAh)
Cell
Vo
lta
ge
(V
)
Pouch Cell First C/20 Cycle
Voltage Limits 4.6V and 2.8V
Celgard 2500 Separator
1M LiPF6 in DEC/DMC/EC
Coated: Black and Grey
Uncoated: Blue and Red
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Third Cycle for
Coated and Uncoated Pouch Cells
Final C/20 cycles before overcharge.
No polarization observed for coated or uncoated cells.
Cell capacity is similar for coated and uncoated pouches.
2.8
3.2
3.6
4.0
4.4
4.8
0 200 400 600 800 1000 1200
Capacity (mAh)
Cell
Vo
ltag
e (
V)
Pouch Cell Third C/20 Cycle
Voltage Limits 4.6V and 2.8V
Celgard 2500 Separator
1M LiPF6 in DEC/DMC/EC
Coated: Black and Grey
Uncoated: Blue and Red
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Uncoated Cell Discharge Capacity after Abuse Testing
All tests performed by charging to 4.5V at C/10.
After overcharge testing to 5.5V, the cell capacity was 0.9Ah vs. 1Ah after 4.8V charge.
After short-circuit test, the cell capacity was 0.88Ah.
No observable cell damage noted due to testing.
2.8
3.0
3.2
3.4
3.6
3.8
4.0
4.2
4.4
4.6
0 2 4 6 8 10 12 14
Time (hours)
Cell
Vo
lta
ge
(V
)
Initial Discharge
Discharge After Overcharge Testing
Discharge After Discharge to 1V
Discharge of Uncoated Pouch Cell after
Abuse Testing and Charge to 4.5V
Current 70mA; Voltage Limit 2.8V
Celgard 2500 Separator
1M LiPF6 in DEC/DMC/EC
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Coated Cell Discharge Capacity after Abuse Testing
All tests performed by charging to 4.5V at C/10.
After overcharge testing to 5.5V, the cell capacity was 1Ah vs. 1.05Ah after 4.8V charge.
After short-circuit test, the cell capacity was 1.01Ah.
No observable cell damage noted due to testing.
2.8
3.0
3.2
3.4
3.6
3.8
4.0
4.2
4.4
4.6
0 2 4 6 8 10 12 14
Time (hours)
Cell
Vo
lta
ge
(V
)
Initial Discharge
Discharge After Overcharge Testing
Discharge After Discharge to 1V
Discharge of Coated Pouch Cell after
Abuse Testing and Charge to 4.5V
Current 82mA; Voltage Limit 2.8V
Celgard 2500 Separator
1M LiPF6 in DEC/DMC/EC
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Impedance Testing Before and After Abuse Testing
Initially the ionic conductivity of the two cells is nearly equivalent with slightly higher
electrical resistance for the coated cell.
After overcharge and short-circuit testing ionic conductivities remain similar though
electrical resistance for the uncoated cell increases more than for the coated cell.
-0.6
-0.5
-0.4
-0.3
-0.2
-0.1
0.0
0.0 0.5 1.0 1.5 2.0
Z' (W)
Z" (W
)
Coated Cell After Conditioning
Uncoated Cell After Conditioning
Coated Cell After Abuse
Uncoated Cell After Abuse
Impedance of Pouch Cells
Test at OCV
Resistance to Ion Flow
Electrical Resistance
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Impedance Testing after Storage at 90°C
Uncharged pouches placed in oven at 90°C for 5.5 hours.
Neither cell catastrophically failed, but the uncoated cell appeared to lose some vacuum.
Coated cell demonstrated increase in electrical resistance, but not ionic resistance.
Both the electrical and ionic resistance for the uncoated cell increased by >3X.
-4.0
-3.5
-3.0
-2.5
-2.0
-1.5
-1.0
-0.5
0.0
0 2 4 6 8 10 12 14 16
Z' (W)
Z" (W
)
Coated Cell After Abuse
Uncoated Cell After Abuse
Coated Cell After 90C Test
Uncoated Cell After 90C Test
Impedance of Pouch Cells
Test at OCV
Resistance to Ion Flow
Electrical Resistance
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Summary of Cathode Coating Results
Optimized coating procedures for coating TODA cathode material.
Coating reduces exotherms observed on heating delithiated cathode
material from greater than -5W/g to less than -1W/g.
Coated cathodes demonstrated <1% loss in discharge capacity over
50 cycles at a C/5 rate.
Demonstrated scale-up with construction of 1Ah pouch cells:
– No reduction in discharge capacity or voltage observed.
– On abuse testing pouch cells utilizing coated cathode material demonstrated
improved stability with reduced impedance growth on abuse testing.
Successfully scaled-up cathode coating to produce and deliver
1500grams of coated cathode material.
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Physical Sciences Inc. VG11-193
Outline
Metal Phosphate Coating for Improved
Cathode Material Safety
Electrochemical Performance of Silicon
Whisker and Carbon Nanofiber Composite
Anode
– Background, overview and previous results
– Scale-up efforts
– Full cell performance
Summary and Next Steps
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Current Silicon Anodes
Illustration of destructive stress
incurred by volume change
during electrochemical cycling.
Silicon anodes reported in the literature*: 1. Pure Si micro- and nano-scale powder anodes,
2. Si dispersed in an inactive matrix,
3. Si dispersed in an active matrix,
4. Si anodes with different binders,
5. Si thin films.
* U. Kasavajjula, C. Wang and A. J. Appleby, Journal of Power Sources, 163, 1003–1039, (2007).
** C. K. Chan, H. Peng, G. Liu, K. McIlwrath, X.F. Zhang, R. A. Huggins and Y. Cui, Nature Nanotechnology, 3, 31 – 35. (2008).
Silicon nanowire based anode by Chan et al. **:
Silicon nanowire on Stainless steel After cycling
- Demonstrated high capacity and rate capability
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PSI Concept: Formation of a
Silicon Whisker and Carbon Nanofiber Composite
Silicon Whiskers/Nanowires on Carbon Nanofiber
Silicon Whiskers
100 nm
J-8382
Nanocarbon Fiber
Material Advantages: High in free volume;
Free of polycrystalline domains (not achievable for silicon anode by CVD);
Tailorable silicon loadings;
Supporting matrix forms an electronically conductive framework;
Processable using established procedure and equipment.
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Cycle Life Performance of the
Silicon Whisker/Carbon Fiber Composite
Discharge: anode lithiation; Charge: anode de-lithiation
All capacity values were calculated based on composite weight
Silicon-on-fiber
architecture
demonstrated with
growth proportional
to reaction time.
Good cycle life
achieved for > 200
cycles;
C/10 cycles seems to
be necessary to
stabilize the cell;
Single crystalline
silicon whiskers are
capable of cycling at
high rate of 1C
0
500
1000
1500
2000
0 50 100 150 200
Cycles
An
od
e C
om
po
sit
e C
ap
acit
y (
mA
h/g
)
Delithiation capacity
Lithiation capacity
Composite Anode Cycled vs. Li
Three cycles at C/10 then 1C
100% DOD
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Successful Material Production Scale-up
Following initial property demonstration, research efforts focused
on moving from producing ~0.5g to 50grams of material per batch.
– Progressively larger batches were run demonstrating linearity and
scalability of the composite formation process.
– Agitation of the sample provides for uniform deposition\material formation.
– PSI has larger reactors that will be utilized for further material production
scale-up efforts.
Electrode optimization has focused on improving the electrode
uniformity to allow for continuous anode material production.
– PSI is producing sufficient electrode for Ah-sized cells and in follow-on
efforts will work to demonstrate electrode production at a pilot casting
facility.
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Rate Performance of Initial High Loading Electrodes
Research has been focused on increasing the material loading from
~0.5mAh/cm2 to ~3-4mAh/cm2.
At low rates, capacities >1000mAh/g-composite were still achievable.
Upon increased rate testing significant polarization was observed
resulting in reduced performance.
0.0
0.2
0.4
0.6
0.8
1.0
1.2
0.0 0.2 0.4 0.6 0.8 1.0
Silicon composite capacity (mAh/g)
Vo
lta
ge
(V
)
100 mA/g
500 mA/g
Anode half cell vs. Li metal
Single layer anodes
Si-composite mass: 4.1 mg/cm2
Separator: Celgard 2500
Electrolyte: 1M LiPF6 in DEC/DMC/EC
(1/1:1:1)
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Improved Performance on Process Optimization
Testing of electrodes in half-cells at C/10 and C/2 was performed to determine the
impact of different processing procedures on performance.
Processing of the composite and slurry was adjusted to improve the cast
uniformity and performance resulting in reduced performance fade on half-cell
cycling at C/2 rates.
0
200
400
600
800
1000
1200
0 2 4 6 8 10
Cycle number
Cap
acit
y (
mA
h/g
)
Gen. 1 Electrode
Gen. 2 Electrode
Anode half cell vs. Li metal
Single layer anodes
Si-composite mass: 3.8-3.9 mg/cm2
Separator: Celgard 2500
Electrolyte: 1M LiPF6 in DEC/DMC/EC (1:1:1)
100mA/g500mA/g
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Successful Transition from Coin to Pouch Cell
Pouch cells of ~75 and ~150mAh have been constructed to demonstrate the
bulk properties of the electrodes and materials.
Initial cycle at 50mA/g-composite was performed to compare coin and pouch cell
performance.
First cycle reversibility is 80-85% using this type of initial cycling procedure.
0.0
0.5
1.0
1.5
2.0
2.5
3.0
3.5
4.0
0 250 500 750 1000 1250
Specific capacity (mAh/g)
Ce
ll V
olt
ag
e (
V v
s.
Li+
/Li)
Discharge of Coin cellCharge of Coin cellCharge of Pouch cellDischarge of Pouch cell
50mA/g Initial Cycling of Coin and Pouch Cells
Silicon Composite~3.1mg/cm2
Separator: Celgard 2500
Electrolyte: 1M LiPF6 in DEC/DMC/EC (1:1:1)
with Additives
Charge Extended to Address
Initial Irreversibility
Discharge Capacity Improved
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Full Cell Performance Demonstration
Coin and pouch cells were tested at various rates with similar performance
measured for each type of cell.
Utilizing the silicon anode 2.5Ah pouch cells have been designed and are being
built. These cells will offer a 7% increase in the cell energy density as compared
to using graphite anode material. The silicon anode reduces the anode material
weight from 15-20% of the total cell mass to 6-8% of the total cell mass.
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0
200
400
600
800
1000
1200
0 5 10 15 20
Sp
ec
ific
Ca
pa
cit
y (
mA
h/g
)
Cycle Number
Pouch Discharge
Coin Discharge
50 mA/g50 mA/g
100 mA/g100 mA/g
200 mA/g200 mA/g
500 mA/g500 mA/g
100 mA/g1000 mA/g
200 mA/g100 mA/g
Full cells cycling versus NCA cathodesElectrolyte: 1 M LiPF6 in 1:1:1 (DC:EC:DMC) + AdditivesSeparator: CelgardCycling rate: Printed above, pouch cell rate in red.Voltage limits: 4.05 volts on charge, 2.5 volts on discharge
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Silicon Anode Program Summary
PSI has developed a silicon whisker and carbon nanofiber composite
material capable of reversibly delivering >1000mAh/g at up to 1C rates.
Composite fiber production has been successfully scaled to 50 gram
scale, with a clear path to production of 250-500 gram batches.
Electrode formulation optimized to produce electrodes delivering
1000mAh/g at the desired loadings.
Equivalent pouch (150+mAh) and coin cell performance demonstrated.
– Production of 2.5Ah pouch cells to be completed as part of research effort.
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Physical Sciences Inc. VG11-193
Outline
Metal Phosphate Coating for Improved
Cathode Material Safety
Electrochemical Performance of Silicon
Whisker and Carbon Nanofiber Composite
Anode
Summary and Next Steps
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Physical Sciences Inc. VG11-193
Summary of NASA Sponsored
Battery Material Development Efforts
PSI has successfully developed a cathode coating process that improves the cycling and safety performance of high energy density cathode materials.
PSI has developed a silicon whisker and carbon nanofiber composite material capable of reversibly delivering >1000mAh/g at up to 1C rates.
PSI has successfully demonstrated scale-up of the anode and cathode technologies and has developed a clear path to further scale-up.
Equivalent performance in the coin and pouch cell formats demonstrates PSI ability to successfully scale-up and transition these novel technologies to a sufficient scale for application based testing.
Future funded research effort will construct cylindrical cells utilizing composite silicon anode and high energy density cathode materials.
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Acknowledgements
Anode Program:
– Special thanks to NASA for supporting this program under contracts NNX09CD30P
and NNX10CA51C.
– Dr. Richard Baldwin, William Bennett and the NASA Glenn Battery Group
Electrochemistry Branch
NASA Glenn Research Center, Cleveland, Ohio
Cathode Program:
– The cathode work was supported by NASA Johnson Space Center, Houston, TX
77058 and NASA Glenn Research Center, Cleveland, OH 44135 under a NASA NRA
(contract # NNC09CA04C).
– Special thanks to:
– Dr. Judith Jeevarajan (COTR), Thomas B. Miller, Jon S. Read, and Pranav Patel for
their assistance during the program.
All past and present PSI staff who have helped in the execution of these
programs including:
• Kara Constantine, Junqing Ma, Ngoc Do, Alex Elliott, Michael McAllister, Peter
Moran, Aron Newman, Nihala Thanikkal, Jose Vega
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