| 电子飞控飞机的飞行品质适航验证 |
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| 引用本文： | 张雅妮,李岩,金镭.电子飞控飞机的飞行品质适航验证[J].飞行力学,2012,30(2):117-120. |
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| 作者姓名： | 张雅妮 李岩 金镭 |
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| 作者单位： | 中航工业综合技术研究所适航性与安全性技术研究中心,北京,100028 |
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| 摘 要： | FAA AC25-7A中的飞行品质评定方法 (HQRM)能够对使用电子飞控系统的民用运输机进行飞行品质评估。分析了HQRM评估程序以及相关适航要求,根据某民用飞机飞控系统功能危险分析,针对单侧升降舵卡阻这一典型故障,提出了在该失效状态下的模拟器飞行品质评估试验程序,分别给出了HQRM和相应军用标准评估方法,对军民评估方法的差异性和一致性进行了分析。研究结果对采用电子飞控系统的现代飞机的飞行品质适航验证具有工程参考意义。
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| 关 键 词： | 飞行品质评定方法 电子飞控系统 适航验证 工程模拟器 功能危险分析 |
Handling qualities airworthiness verification for electronic flight control aircraft |
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| ZHANG Ya-ni
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LI yan
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JIN lei.Handling qualities airworthiness verification for electronic flight control aircraft[J].Flight Dynamics,2012,30(2):117-120. |
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| Authors: | ZHANG Ya-ni LI yan JIN lei |
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| Institution: | (Airworthiness and Safety Technology Research Department,China Aviation Polytechnology Establishment,Beijing 100028,China) |
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| Abstract: | Handling quality rating method(HQRM) in FAA AC25-7A provide a means by which one may evaluate flight characteristics for fly-by-wire flight control transport aircraft.This paper explains the HQRM procedure,and analyses airworthiness requirements which are related to HQRM.According to flight control system functional hazard assessment of a commercial airplane,simulator experiment procedure for a elevator jam is proposed,and experiment analysis methods using the FAA method and military standard are offered.The consistency and differences between civil and military standards are analyzed.This study can supply references for flying qualities and airworthiness verification of a modern airplane with electrical flight control system. |
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| Keywords: | handling quality rating method electrical flight control system airworthiness verification engineering simulator functional hazard assessment |
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