电子电气工程与控制

容错航空蓄电池电源及其均衡管理

  • 王友仁 ,
  • 黄薛 ,
  • 耿星 ,
  • 徐智童 ,
  • 陈则王
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  • 南京航空航天大学 自动化学院, 南京 211106

收稿日期: 2017-09-05

  修回日期: 2018-02-10

  网络出版日期: 2018-02-10

基金资助

国家自然科学基金(61371041);航空科学基金(2013ZD52055);国家商用飞机制造工程技术研究中心创新基金(SAMC14-JS-15-051);江苏省普通高校专业学位研究生科研创新计划(SJLX16_0101)

Fault-tolerant battery power supply for aircraft and its active equalization management

  • WANG Youren ,
  • HUANG Xue ,
  • GENG Xing ,
  • XU Zhitong ,
  • CHEN Zewang
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  • College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China

Received date: 2017-09-05

  Revised date: 2018-02-10

  Online published: 2018-02-10

Supported by

National Natural Science Foundation of China (61371041); Aeronautical Science Foundation of China (2013ZD52055); Fund of National Engineering and Research Center for Commercial Aircraft Manufacturing (SAMC14-JS-15-051); Research Innovation Program for Graduate Students in Jiangsu Province (SJLX16_0101)

摘要

航空蓄电池在实际使用中会出现电池性能衰退与退化速率不一致,电池组容量与使用寿命降低,甚至可能出现严重的安全事故。针对电池单体不一致性和故障隔离问题,提出一种蓄电池电源系统容错体系结构和分级容错控制策略,提出基于电池单体动态重构的主动均衡管理新方法,设计基于"冒泡沉底(BS)择优上岗"的电池单体实时动态重构策略。开发容错航空镍镉电池电源原理样机,给出系统实验性能分析,实验结果表明所提出的系统技术方案可行有效,能够快速隔离故障失效电池单体,明显改善电池不一致性,提高了电池组容量利用率和剩余使用寿命。

本文引用格式

王友仁 , 黄薛 , 耿星 , 徐智童 , 陈则王 . 容错航空蓄电池电源及其均衡管理[J]. 航空学报, 2018 , 39(5) : 321722 -321722 . DOI: 10.7527/S1000-6893.2018.21722

Abstract

In practical use, battery cells will have different problems including performance degradation, different degradation rate of cells, capacity and service life degradation, and even occurrence of serious accidents. To solve the problems of inconsistency of battery and fault isolation requirement, a fault tolerant architecture and hierarchical fault tolerant control strategy for battery power supply are proposed, a method of active equalization management based on dynamic reconfiguration of cells is presented, and a real-time dynamic reconfiguration strategy based on Bubble Sort (BS) for battery cells is given. A prototype of the fault tolerant Ni Cd battery power system for aircraft is developed. The experimental results show that the proposed system scheme is feasible and effective, and fault cells can be isolated quickly to greatly reduce the inconsistency of battery cells and improve the capacity and remaining useful life of the battery power system.

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