基于航空发动机温度分区的线束分布式设计
Analysis of Harness Distributed Design Based on Aero Engine Temperature
赵猛 1姜睿智 1李聪 1袁广银1
作者信息
- 1. 沈阳兴华航空电器有限责任公司,辽宁 沈阳,110144
- 折叠
摘要
本文介绍了航空发动机温度分区情况.阐述了发动机电缆的分布式设计流程和原理.分析了通过不同等级的耐高温器件、材料和结构实现分布式设计的关键技术和解决措施.研究了发动机电缆分布式设计与腐蚀环境防护和电磁兼容设计之间的相互影响情况.最后展望了分布式设计的发展趋势.
Abstract
This paper introduces the temperature zoning of aero engine.The distributed design process and principle of engine harness are described.The key technologies and solutions of distributed design through different grade high temperature resistant devices,materials and structures are analyzed.The interaction between distributed design of engine harness,corrosion protection and electromagnetic compatibility design is studied.Finally the devel-opment trend of distributed design is forecasted.
关键词
航空发动机/温度分区/发动机电缆/分布式设计/耐高温Key words
aero engine/temperature zoning/engine harness/distributed design/high temperature resistance引用本文复制引用
出版年
2024
NETL
NSTL
万方数据