Preventing Thermal Runaway Propagation of 3.2 Ah Lithium-Ion Cell Battery Packs with Phase Change Composite Material: Investigating a Cell-Air-PCC (Air-Gap) Design

Author(s):  
Samuel Plunkett ◽  
Chris Coble ◽  
Greg Albright ◽  
Said Al-Hallaj
2021 ◽  
Vol 40 ◽  
pp. 102737
Author(s):  
Malcolm P. Macdonald ◽  
Sriram Chandrasekaran ◽  
Srinivas Garimella ◽  
Thomas F. Fuller

2021 ◽  

Thermal propagation test of lithium-ion battery is an important method to verify the safety of battery system, and how to effectively trigger the thermal runaway of a cell and minimize the energy introduced into the system become the key of test method design. In this work, the influence of different heating area and different heating power on thermal runaway of prismatic cells and pouch cells is studied. The results show that when the heating area is fixed, the heating power increases, the heating time required to trigger the thermal runaway of the cells becomes shorter. The energy needed to be introduced becomes smaller, but there will be a minimum value of the introduced energy. On the other hand, the thermal runaway results of prismatic cells are more sensitive to the change of heating area, and the thermal runaway results of pouch cells are more sensitive to heating power.


2018 ◽  
Vol 54 (1) ◽  
pp. 426-436 ◽  
Author(s):  
Mohamad Salameh ◽  
Stephen Wilke ◽  
Ben Schweitzer ◽  
Peter Sveum ◽  
Said Al-Hallaj ◽  
...  

2021 ◽  
Vol 9 ◽  
Author(s):  
Weisi Li ◽  
Vanessa León Quiroga ◽  
K. R. Crompton ◽  
Jason K. Ostanek

High temperature gases released through the safety vent of a lithium-ion cell during a thermal runaway event contain flammable components that, if ignited, can increase the risk of thermal runaway propagation to other cells in a multi-cell pack configuration. Computational fluid dynamics (CFD) simulations of flow through detailed geometric models of four vent-activated commercial 18650 lithium-ion cell caps were conducted using two turbulence modeling approaches: Reynolds-averaged Navier-Stokes (RANS) and scale-resolving simulations (SRS). The RANS method was compared with independent experiments of discharge coefficient through the cap across a range of pressure ratios and then used to investigate the ensemble-averaged flow field for the four caps. At high pressure ratios, choked flow occurs either at the current collector plate when flow through the current collector plate is more restrictive or the positive terminal vent holes when flow through the current collector plate is less restrictive. Turbulent mixing occurred within the vent cap assembly, in the jets emerging from the vent holes, and in recirculating zones directly above the vent cap assembly. The global maximum turbulent viscosity ratio (μT/μ) of the MTI, LG MJ1, K2, and LG M36 caps at pressure ratio of P1/P2 = 7 were 4,575, 3,360, 3,855, and 2,993, respectively. SRS and RANS simulations showed that both velocity magnitude and fluctuating velocity magnitude were lower for vent holes which are obstructed by the burst disk. SRS showed high levels of fluctuating velocity in the jets, up to 48.5% of the global maximum velocity. The present CFD models and the resulting insights provide the groundwork for future studies to investigate how jet structure and turbulence levels influence combustion and heat transfer in propagating thermal runaway scenarios.


2016 ◽  
Author(s):  
Christopher J. Orendorff ◽  
Joshua Lamb ◽  
Leigh Anna Marie Steele ◽  
Scott Wilmer Spangler ◽  
Jill Louise Langendorf

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