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全机疲劳试验几个问题的探讨

张立新

航空工程进展2024,Vol.15Issue(4):10-15,26,7.
航空工程进展2024,Vol.15Issue(4):10-15,26,7.DOI:10.16615/j.cnki.1674-8190.2024.04.02

全机疲劳试验几个问题的探讨

Discussions on some problems of full-scale aircraft fatigue test

张立新1

作者信息

  • 1. 航空工业成都飞机设计研究所,成都 610091
  • 折叠

摘要

Abstract

Full-scale aircraft fatigue test is a large,complex and long-lasting ground verification test required by the specification to sustain aircraft structural integrity program and meet airworthiness requirements.Several important issues of full-scale aircraft fatigue test,such as test objective,load spectrum,duration and scatter factor,are the key concern and widely discussed by aircraft designer/engineer.The scatter factor is also a problem studied by scholars.In recent years,aiming at the full-scale fatigue tests of several aircraft programs,the study and under-standing of the above-mentioned issues are introduced in this paper,and the fatigue design and full-scale fatigue tests of five fighter jets in China and abroad are compared.Some practical engineering suggestions for full-scale air-craft fatigue test are put forward.The research in this paper can provide important reference for other aircraft full-scale fatigue tests.

关键词

全机疲劳试验/耐久性/损伤容限/载荷谱/持续时间/分散系数

Key words

full-scale aircraft fatigue test/durability/damage tolerance/load spectrum/duration/scatter factor

分类

航空航天

引用本文复制引用

张立新..全机疲劳试验几个问题的探讨[J].航空工程进展,2024,15(4):10-15,26,7.

航空工程进展

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1674-8190

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