| 航空装备的完整性 |
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| 引用本文： | 王立群.航空装备的完整性[J].航空学报,1988,10(10):433-439. |
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| 作者姓名： | 王立群 |
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| 作者单位： | 空军第一研究所 |
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| 摘 要： | 简述完整性概念在航空装备上的应用情况,提出了航空装备完整性概念,并简介了航空装备的完整性原理,
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| 收稿时间： | 1987-04-12; |
AIRCRAFT EQUIPMENT INTEGRITY |
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| First Instiutte of Air Force Wang Liqun.AIRCRAFT EQUIPMENT INTEGRITY[J].Acta Aeronautica et Astronautica Sinica,1988,10(10):433-439. |
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| Authors: | First Instiutte of Air Force Wang Liqun |
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| Institution: | First Instiutte of Air Force Wang Liqun |
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| Abstract: | The term "integrity" has been used as a quality characteristic of main aircraftequipment in the past two decades. It was applied to aircraft structures first, and then toengine structures and avionics.On the basis of this fact, the author is putting forward the term"aircraft equipment integrity". Both UsAF's aircraft structural integrity program and enginestructural integrity program use durability and damage tolerance design as the integrity technique,while USAF's avionics integrity program (AVIP) uses eight- main integrity techniques in designphase, namely: piece parts selection, parts derating, parts burn-in, environmental stress screen,failure prediction analysis, computer aided design, testability and design reviews.These integritytechniques for aircraft structures, engine structures and avionics are briefly described in thispaper. |
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| Keywords: | structural integrity damage tolerance design engine structure design avionics design |
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