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航空发动机晶体管式点火系统火花频率稳定性研究

赵军 张涛

现代电子技术Issue(11):116-118,3.
现代电子技术Issue(11):116-118,3.

航空发动机晶体管式点火系统火花频率稳定性研究

Study on spark frequency stability of aeroengine transistor ignition system

赵军 1张涛2

作者信息

  • 1. 天津航空机电有限公司,天津 300308
  • 2. 中国人民解放军空军驻天津地区军事代表室,天津 300308
  • 折叠

摘要

Abstract

  In order to improve the spark frequency stability of aeroengine transistor ignition system,working principle of the transistor ignition system is analyzed. The factors that affect spark frequency stability were found out. The voltage compensa⁃tion and temperature compensation were adopted for the influence factors. The spark frequency comparison experiment was per⁃formed. In the case of high temperature and voltage fluctuation,the spark frequency stability of the compensated ignition system is increased by a factor of about 50%.

关键词

晶体管式点火系统/火花频率/电压补偿/温度补偿

Key words

transistor ignition system/spark frequency/voltage compensation/temperature compensation

分类

信息技术与安全科学

引用本文复制引用

赵军,张涛..航空发动机晶体管式点火系统火花频率稳定性研究[J].现代电子技术,2013,(11):116-118,3.

现代电子技术

OACSTPCD

1004-373X

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