Simulation of charge-discharge cycling of lithium-ion batteries under low-earth-orbit conditions

被引：45

作者：

Lee, Jong-Won ^{[1
]}

Anguchamy, Yogesh K. ^{[1
]}

Popov, Branko N. ^{[1
]}

机构：

[1] Univ S Carolina, Dept Chem Engn, Ctr Electrochem Engn, Columbia, SC 29208 USA

来源：

JOURNAL OF POWER SOURCES | 2006年 / 162卷 / 02期

关键词：

lithium-ion battery; capacity fade simulation; aerospace application; low-earth-orbit;

D O I：

10.1016/j.jpowsour.2006.07.045

中图分类号：

O64 [物理化学（理论化学）、化学物理学];

学科分类号：

070304 ; 081704 ;

摘要：

Charge-discharge behavior of SONY 18650 lithium-ion batteries for aerospace applications was simulated under low-earth-orbit (LEO) conditions, by using a first-principles based mathematical model. The model determines the capacity fade on the basis of the irreversible loss of active lithium ions due to electrolyte reduction. The capacity fade during LEO cycling was studied for 5 years of continuous operation with 20% depth of discharge as a function of the cycling parameters such as the end of charge voltage and the charging rate. (c) 2006 Elsevier B.V. All rights reserved.

引用

页码：1395 / 1400

页数：6

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