旋翼航空器尾桨保护装置适航条款分析研究 |
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引用本文: | 吴世豪,黄文斌,崔甲子.旋翼航空器尾桨保护装置适航条款分析研究[J].直升机技术,2013(3):61-64. |
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作者姓名: | 吴世豪 黄文斌 崔甲子 |
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作者单位: | 中航工业直升机设计研究所,江西景德镇,333001 |
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摘 要: | 基于对旋翼航空器尾桨保护装置适航条款的分析,诠释该条款的技术内涵,列举了相关的型号验证实例,为从事旋翼航空器设计和适航审定的人员提供技术参考。
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关 键 词: | 适航 旋翼航空器 尾桨保护装置 条款分析 |
Analysis of Rotorcraft's Tail Rotor Guard on Airworthiness Clauses |
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Authors: | WU Shihao HUANG Wenbin CUI Jiazi |
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Institution: | (China Helicopter Research and Development Institute, Jingdezhen 333001, China) |
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Abstract: | Based on the airworthiness clause of rotorcrafi' s tail rotor guard, this paper analyzed the connotation of the section and enumerated correlative aircraft cases, provided technical reference for rotoreraft designers and airworthiness censors. |
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Keywords: | airworthiness rotorcraft tail rotor guard airworthiness clause analysis |
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