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1 NASA Battery Workshop- Huntsville, November 2002 "Safety Performance of Small Lithium-Ion Cells" Safety Performance of Small Lithium-Ion Cells in High Voltage Batteries Philip R. Cowles: COM DEV Space Eric C. Darcy: NASA-JSC Frank J. Davies: HEI/Lockheed Martin Judith A. Jeevarajan: Lockheed Martin, NASA-JSC Robert P. Spurrett: AEA Technology

Safety Performance of Small Lithium-Ion Cells in …...4 NASA Battery Workshop- Huntsville, November 2002 "Safety Performance of Small Lithium-Ion Cells" The nature of a Shorted String

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Page 1: Safety Performance of Small Lithium-Ion Cells in …...4 NASA Battery Workshop- Huntsville, November 2002 "Safety Performance of Small Lithium-Ion Cells" The nature of a Shorted String

1

NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Safety Performance of SmallLithium-Ion Cells in High Voltage Batteries

Philip R. Cowles: COM DEV SpaceEric C. Darcy: NASA-JSCFrank J. Davies: HEI/Lockheed MartinJudith A. Jeevarajan: Lockheed Martin, NASA-JSCRobert P. Spurrett: AEA Technology

https://ntrs.nasa.gov/search.jsp?R=20030112603 2020-03-15T16:41:41+00:00Z

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2

NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Introduction

Small-cell EAPU work done by NASA-JSC & COM DEVLooking at safety features – short circuit protection - PTCsEarly tests showed that long strings do not withstand short circuit• Some PTCs experience large negative voltages• Destructive results

Solution: group cells into shorter substrings, with bypass diodesWork included:• Tests with single cells shorted• Tests with single cells with imposednegative voltages• 6s, 7s and 8s string shorts• Tests with protection scheme in place, on 12s and 41s x 5p

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Specific Requirements

NASA requires a '2-failure tolerance' against catastrophic failure• Fire, explosion, severe venting

One failure is an external short-circuitThe other a is failure in a cell that might propagateNot a usual requirement for unmanned missions• Most spacecraft primes have a fuse-blowing or fault clearance target• e.g. 2000 Amp for 20 mS

Most obvious case is a hard short at or close to the terminalsWe also consider the case of a 'smart short'• defined as a low-resistance short that is

more damaging than a hard short

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

The nature of a Shorted String

Use fully charged cells (4.4V/cell)>60 amp/string inrush currentSony cells have a PTC deviceIn a long string, all PTC's race to tripThe winner gets a high negative voltageMore than ~30V and it breaks downThis implies strings of ~>7swill not be protected by the PTCs

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Long String Test

24s x 2p test battery• Previously used for convergence tests

Charge to 105.6V, 4.4V/cell'Admirals' testShort itLow-rate voltage sampling on each cell + currentConsiderable damage

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

24s x 2p Battery - after

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Condition of Cells after the Test

State No. of Cells

Operating 12

No volts 27

Leaks/vents 25

Wrapper damage 23

Meltdown 4 (cells 39 – 42)

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Cells 39 - 42

Cans ~300°CLost ~10gAluminuminternal tabs melted(>600°C)

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Single-Cell Tests

Aim to understand the PTCFully charged cells, 20°CShorts from 0.5 mΩ to 1.3 ΩCells insulatedMeasured current, voltage, timeEstimated cell Soc, cell Rs, PTC resistance

Cell PTC Test Circuit

Cell partly installed

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

PTC Equivalent CircuitSet Parameters

Cell initial state e.g 4.385V EMF

Load Resistance

Measured parameters are:

V, cell terminal volts (mVolts)

I, cell current (Amps)

T, cell temperature (Temp)

Derived parameters are:

Actual presented load resistance (R eff)

Ah out of cell

Wh dissipated in cell

State of charge

Cell EMF

Cell dissipation, PTC dissipation

Cell dissipation energy (W-h)

Extra parasitic resistance (Rpara)

Cell state estimated using initial state + SoC EMF relationship

S = 0.02081238r = 0.99928065

X Axis (units)

Y A

xis

(uni

ts)

0.0 25.3 50.6 75.9 101.2 126.5 151.82.30

2.70

3.10

3.50

3.90

4.30

4.706th Degree PolynomiaCoefficient Data:a = 2.586134b = 0.037551c = -0.00017d = -2.95E-06e = 2.02E-08f = 1.38E-10g = -9.52E-13

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Single Cell Time-to-trip (linear)

Time to Trip

0

500

1000

1500

2000

2500

3000

0.001 0.0

3

0.144 0.3

1

0.51

0.61

0.86

1.241

R_s

Tim

e (S

ec)

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Single Cell Time-to-trip (log)

Time to trip

1

10

100

1000

10000

0.0010.0

10.0

30.1

20.1

440.21

0.31

0.41

0.51

0.5460.6

10.7

590.86

1.022

1.241

R_s Ohms

Tim

e (S

ec)

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Typical Data – hard shortPTC Test 33 Current

012345678

0 20 40 60 80 100 120 140

Time Sec

Amp

PTC Test 33 (hard short) Temp.

0

20

40

60

80

100

120

0 1000 2000 3000 4000 5000 6000 7000

Elapsed (sec)

Cell

Tem

p °C

PTC Test 33 Rptc

0

1

2

3

4

5

0 20 40 60 80 100

Elapsed (s)

Ohm

PTC test No 33, PTC Dissipation

05

101520253035

0 20 40 60 80 100

Elapsed (s)

Wat

t

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Typical Data – 0.41 OhmPTC test No 43 Current

0

2

4

6

8

10

0 20 40 60 80 100

Elapsed Sec

Amp

PTC test No 43 - temperature

0

20

40

60

80

100

120

0 1000 2000 3000 4000

Elapsed (s)

DegC

PTC Test No 43, Rptc

-5

0

5

10

15

20

25

0 1000 2000 3000 4000

Elapsed (s)

Ohm

PTC Test No 43, PTC dissipation

0

2

4

6

8

10

12

0 1000 2000 3000 4000

Elapsed (s)

Wat

t

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Short-String Tests

6, 7 and 8s strings shorted (hard shorts)6s and 7s strings shut down gracefullyWith 8s, 2 out of 3 'sparked'

7S cell bundle ready for test

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

8s Test No 1

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Single-cell tests with reverse voltage

Tests conducted by NASA-JSCAim to simulate the sacrificial cell by applying a negative voltageUse high current power supply

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Single-cell results - 1Cell No. Temp at

start Current during trip

Time to trip (Sec)

Voltage after trip

Current after trip

Notes DPA Notes

61 amb 18A 2.5 0.0V 1.0 cells

1.27A No fail

49 amb 15 A 6.056 -25.4 V 6.8 cells

0.25 A No fail.

60 amb 15 A 5.18 -32.36 V 8.4 cells

3.6 A Failed after less than 1 second of -32 V then seal failure after 8 seconds

Damage to PTC and shorted seal

66 amb 15 A 4.905 -30.6 V 8.0 cells

0.23 A Failure 43 sec after trip PTC end stayed at 70C after external supply removed

Minor damage to PTC and shorted seal

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Single-cell results - 2

Cell No. Temp at start

Current during trip

Time to trip (Sec)

Voltage after trip

Current after trip

Notes DPA Notes

57 amb 15 A 4.383 -22.5 V 6.2 cells

0.26 A No failure

55 65C 13.1 A 0.9 -o 1.2 -27.3 V 7.3 cells

0.19 A Failure after 90 sec of -27.3 V PTC end stayed at 84C after external supply removed and during purge.

No damage to PTC but seal shorted under curled over crimp edge. Thermal evidence that cell discharged itself slowly through PTC and this short.

51 65C 8.5 A 0.788 -26.8 V 7.2 cells

0.06 A No Failure

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Single-cell tests - observations

Temperature at PTC shoots up very quickly when PTC trips. Maximum temperatures on the outside of the case at the crimp go up above 200°F (95°C)Collateral damage caused to crimp sealTests confirmed that ~7s was 'marginally safe'9 Amp diodes appear to handle the ~60A inrush current

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Component Parts

1. Battery cell with built-in short circuit protection.

2. Internal short circuit protection device (PTC). May be similar to Raychem Polyswitch.

3. Electrochemical part of cell (provides electromotive force)

4. Substring

5. Diode

6. Load.

21

3 5

64

Notes:

A. More than two battery cells per substring may be used.

B. More than 3 substrings may be used.

C. The example battery system presented here is of limited size and complexity for clarity.

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

High voltage on PTC during Short Circuit

Battery Cell with built-in short circuit protection device (PTC).

Example uses Li-Ion cells charged to 4V per cell.

0.0V

4.0V

8.0V

12.0V

16.0V

20.0V

24.0V

Normalload

0.0V

4.0V

8.0V

-12.0V

-8.0V

-4.0V

0.0V

Short

circuit

Tripped current limiting device (PTC) in high impedance state. Note that it has 24V across it. This voltage may exceed the voltage rating of the device.

12.0V

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Trip Sequence – initial stage

Shor

tCirc

uit60

A

Short circuit appears. All PTC short circuit protection devices start heating up.

Notes:

1. No current through diodes yet.

2. Short circuit current is limited by cell impedances and cold PTC impedances.

3. This stage may last several seconds, depending on PTC characteristics.

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Trip Sequence – later stages

First PTC trips, shunting current through diode.

Note:

1. Small current flows through shorted substring, keeping PTC tripped.

2. Current through short is reduced, but not dramatically, since the current is still basically limited by the cell impedances. Other substrings have not tripped yet.

3. Maximum voltage across tripped PTC is two cells worth plus diode drop.

4. Diode takes almost maximum short circuit current until trip sequence is complete.

5. Which substring trips first depends on device tolerances.

6. The other substrings follow.

Shor

t Circ

uit

0.50A

54.5A

54.5A

54.5A

55.0A

Tripped

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

12s Short-Circuit Test- with diodes

12s bundle configuration9 Amp Schottky diodesDead shortMonitor current and diode voltages

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

12s Short-Circuit - current

12s String with diodes

0

10

20

30

40

50

0 0.5 1 1.5 2 2.5 3 3.5

Elapsed (Sec)

Amp

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

12s Test – Diode Voltage -1

12s diodes - diode voltages

-0.4-0.3

-0.2-0.1

0

0.10.20.3

0.40.5

0 50 100 150 200 250 300

Elapsed (s)

Volts

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

12s Test – Diode Voltage -2

12s diodes - diode voltages

-0.3

-0.2

-0.1

0

0.1

0.2

0.3

2 3 4 5 6 7

Elapsed (s)

Volts

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

41s x 5p Short-Circuit

EAPU GTMCharge to 180.4VShortSuccessful- no damage- no venting- still works

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Submodule 01 Short

SubM_01_short

0

50

100

150

200

250

300

350

0 0.5 1 1.5 2 2.5

Elapsed (s)

Amp

Short using EV200 relay, 0.5 mΩKelvin resistor.

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Post-short EAPU Mission Cycle

SubM 01 Mission Post Short

120

130

140

150

160

170

180

0 20 40 60 80 100 120

Elapsed (min)

Volt

560W

4000W

Battery charged to pre-launch state, including losses

Launch and de-orbit run concatenated

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Diode Protection Scheme - summary

Advantages:• Increases robustness• Protects PTCs – allows them to operate normally• Allows operation of cells within voltage environment that they were

designed for (short series strings, not long series strings). • Bypass diodes across substrings help with other high impedance cell

conditions (tripped CID, shutdown separator, discharged cell) by holding down max. voltage.

Disadvantages:• Added components increase size, weight and complexity.• Diodes sized to take maximum current are not small.

Testing will allow us to optimize diode sizing.

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NASA Battery Workshop- Huntsville, November 2002

"Safety Performance of Small Lithium-Ion Cells"

Conclusions

We have gained considerable insight into cell PTC operation• Maximum voltage rating of the PTC at 65°C is 31V• Once tripped, PTCs are more tolerant to higher voltages

Even without diode protection, a short with a small-cell battery is not a violent eventThe diode protection scheme works • Using commercial Schottky diodes

The battery is usable afterwardsThe scheme is being implemented on current modulesFurther short-circuit tests are planned• To validate function in worst-case conditions• To better understand cell failure mechanisms