摘要
民用飞机的快速发展正在对电子设备结构设计提出新的要求。按照DO254要求对电子设备结构设计的研制生命周期进行了分析,对民机应遵循的封装规范进行了比较,对如何满足民机环境适应性进行了分析并提出了解决方案。
More new requirements were advanced with the fast development of the civil aeroplanes. According to the demand of D0254, this article made some analysis of the research and whole manufactury period for the electronic equipment structure. Also made some research on the compare of the package criterion of civil aeroplane, present a solution about how to fit the civil circumstance adaptability.
出处
《航空计算技术》
2010年第2期108-110,116,共4页
Aeronautical Computing Technique
关键词
民机
电子设备结构
适航
封装
环境适应性
civil aeroplane
electronic equipment structure
airworthiness
package
environmental adaptability
