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美军V/STOL飞机机载设备可靠性试验剖面研究
引用本文:王光芦,李维宝.美军V/STOL飞机机载设备可靠性试验剖面研究[J].装备环境工程,2011,8(5):56-61,76.
作者姓名:王光芦  李维宝
作者单位:1. 中国航空综合技术研究所,北京,100028
2. 总参谋部陆航部装备发展办公室,北京,100012
摘    要:简述了美军垂直/短距起落飞机(V/STOL)飞机的特征和环境,提供了垂直/短距起落飞机的10个典型作战任务剖面及其飞行参数,分析了垂直/短距起落飞机和常规起落飞机的环境差异,给出了垂直/短距起落飞机每个作战任务剖面对应的可靠性试验剖面.

关 键 词:垂直/短距起落  任务剖面  振动  试验剖面
收稿时间:2011/3/10 0:00:00
修稿时间:2011/10/15 0:00:00

Development Reliability Test Profile for Equipments in US V/STOL Aircraft
WANG Guang-lu and LI Wei-bao.Development Reliability Test Profile for Equipments in US V/STOL Aircraft[J].Equipment Environmental Engineering,2011,8(5):56-61,76.
Authors:WANG Guang-lu and LI Wei-bao
Affiliation:WANG Guang-lu1,LI Wei-bao2(1.China Aviation Poly-technology Establishment,Beijing 100028,China,2.Equipment Development Office of Marine Aviation Department of General Staff,Beijing 100012,China)
Abstract:Character and service environment of V/STOL aircraft of United States was briefly introduced.Ten typical battle mission profiles and flight parameters of V/STOL aircraft were provided.The environmental difference between V/STOL and traditional aircraft was analyzed.The reliability test profile according to each battle mission profile was given.
Keywords:V/STOL  mission profile  vibration  test profile  
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