Revealing the Degradation Mechanism of Lithium‐Ion Batteries for Electric Aircraft

S Shihai Tang (School of Chemical Engineering Sichuan University Chengdu 610065 China) F Fu Sun (Qingdao Industrial Energy Storage Research Institute, Qingdao Institute of Bioenergy and Bioprocess Technology) H Hailong Wang (Beijing Key Laboratory for Science and Application of Functional Molecular and Crystalline Materials, Department of Chemistry and Chemical Engineering, School of Chemistry and Biological Engineering) Q Qinlang Rong N Nuo Sun L Liang Zhang Y Yuan Zhao Q Qianjin Xiong (School of Chemical Engineering Sichuan University Chengdu 610065 China) B Bingxuan Huang (School of Chemical Engineering Sichuan University Chengdu 610065 China) L Linyu Hu J Jan‐Philipp Hoffknecht (Institute for Electrochemical Energy Storage (CE‐IEES) Helmholtz‐Zentrum Berlin für Materialien und Energie Hahn‐Meitner‐Platz 1 14109 Berlin Germany) Z Zhimeng Liu X Xin He

Abstract

Abstract The widespread adoption of electric vehicles has spurred the exploration of airworthy lithium‐ion batteries (LIBs) for electric‐powered aircraft. However, LIBs used for aviation exhibit rapid aging and shortened service life due to the harsh conditions of aviation, posing significant risks to flight safety. In this study, a comprehensive analysis is conducted under simulated flight conditions to reveal the degradation mechanism of aviation batteries. Low‐temperature and low‐pressure lead to a sluggish kinetics and hinder thermodynamic process. As the reversibility of Li‐ions insertion and extraction is deteriorates, residual Li‐ions accumulate and plated‐Li on the anode, accelerating the aging process and arising the issue of internal short circuits. Additionally, the interatomic distance of Ni‐coordination induces significant stress variations, which drives an expanded occupation of porosity in the electrode under flight conditions, with 2.13% void spaces of cathode and 13.39% of anode. The formation and growth of cracks elongate the charge transfer pathway, increasing resistance and reducing rate capability. As a result, this study quantifies the degradation mechanisms of aviation batteries and establishes the relative impact weights of temperature and pressure factors, offering critical insights for optimizing future electric aircraft power battery designs.

Article Details

Volume / Issue Vol. 37, Issue 29
Published July 01, 2025
ISSN 0935-9648
Publisher Unknown Publisher

Journal Info

Advanced Materials

Unknown Publisher

ISSN: 0935-9648 Physical Sciences

Authors (13)

S

Shihai Tang

School of Chemical Engineering Sichuan University Chengdu 610065 China

F

Fu Sun

Qingdao Industrial Energy Storage Research Institute, Qingdao Institute of Bioenergy and Bioprocess Technology

H

Hailong Wang

Beijing Key Laboratory for Science and Application of Functional Molecular and Crystalline Materials, Department of Chemistry and Chemical Engineering, School of Chemistry and Biological Engineering

Q

Qinlang Rong

N

Nuo Sun

L

Liang Zhang

Y

Yuan Zhao

Q

Qianjin Xiong

School of Chemical Engineering Sichuan University Chengdu 610065 China

B

Bingxuan Huang

School of Chemical Engineering Sichuan University Chengdu 610065 China

L

Linyu Hu

J

Jan‐Philipp Hoffknecht

Institute for Electrochemical Energy Storage (CE‐IEES) Helmholtz‐Zentrum Berlin für Materialien und Energie Hahn‐Meitner‐Platz 1 14109 Berlin Germany

Z

Zhimeng Liu

X

Xin He