航空活塞发动机电子点火系统应用研究  

Application Research on Electronic Ignition System of Aviation Piston Engine

作　　者：赵晨迪 秦逸[1] 陈霄阳 ZHAO Chendi;QIN Yi;CHEN Xiaoyang(Civil Aviation Flight University of China,Guanghan 618307,Sichuan,China)

机构地区：[1]中国民用航空飞行学院,四川广汉618307

出　　处：《民航学报》2023年第5期120-123,共4页Journal of Civil Aviation

基　　金：通用固定翼飞机重大结构修理装备研究(ZJ2020-09)资助。

摘　　要：在通用航空飞机和中大型无人机的动力装置中,航空活塞发动机因其运行可靠、结构简单等优势一直具有很高的占比。但在航空活塞发动机整个发展史中,其构型基本不变,较于现有的汽车活塞发动机发展相对保守。本文就广泛使用的航空活塞发动机点火系统构型和原理进行深度剖析,对新型电子点火系统的原理以及改装应用进行研究和阐述。In the power plant of general aviation aircraft and medium and large UAVs,aviation piston engine has a high proportion because of its advantages such as reliable operation and simple structure.But throughout the history of aviation piston engine,its configuration remained pretty much the same,and its development was relatively conservative compared with current automotive piston engine.In this paper,the configuration and principle of the ignition system of widely used aero-piston engines are deeply analyzed,and the principle and application of new electronic ignition systems are studied and expounded.

关 键 词：活塞发动机 通用飞机 电子点火 磁电机 无人机 

分 类 号：V234[航空宇航科学与技术—航空宇航推进理论与工程]