Design of an Innovative Aviation Integrated Electronic Equipment Rack
This design is an open-loop aviation electronic equipment rack based on ARINC600 for a aircraft under only air exhaust condition.Conduct tress and stiffness analysis via ANSYS calculating the maximum stress and the maximum distortion.Calculate the maximum power of electronic equipment suitable for this equipment suitable for this equipment rack through heat transfer theory and provide theory basis for electronic equipment layout on the overall aircraft.
Electronic equipment rack ARINC600 Stress Stiffness Heat transfer
Xueyong Chen Ning Zhao Shuanhui Sun Xiaoliang Wang
The Mechanical and Electrical engineering, Northwestern Polytechnical University,Xian,Shanxi,710068 The Mechanical and Electrical engineering, Northwestern Polytechnical University,Xian,Shanxi,710068 China Aviation Optical-Electrical Technology CO.,LTD, Luoyang,Henan,471003,China
国际会议
重庆
英文
1195-1198
2011-06-23(万方平台首次上网日期,不代表论文的发表时间)