摘要
简述了某发动机电子控制器电磁兼容性设计的思想和方法 ,并通过试验进行了验证和完善 。
Design of electromagnetic compatibility of the electronic controller is disc ussed in a typical aircraft engine. The design is demonstrated and imp roved, and the results are s atisfactory.
出处
《航空发动机》
2003年第3期38-40,34,共4页
Aeroengine