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空气轮启动器的三切式轮轮爆发的外部外结构设计
Jin Tang1, Yong Zhang1, Ge Wang1
1AECC Hunan Aviation Powerplant Research Institute, Zhuzhou, China.
PloS one
|September 27, 2024
概括
航空安全法规要求对高能旋转器部件进行强大的封闭. 这项研究验证了有限元法 (FEM) 方法,用于设计成功制风力轮启动轮轮失效的外.
科学领域:
- 航空航天工程 航空航天工程
- 机械工程 机械工程
- 材料科学 材料科学 材料科学
背景情况:
- 航空法规要求对高能旋转器部件进行封闭能力.
- 确保空气轮启动轮轮轮的封装对于飞机安全至关重要.
研究的目的:
- 提出和验证一种外结构设计方法,以控制风力轮启动轮轮失效.
- 确保符合航空安全法规的关于旋转器部件封闭的规定.
主要方法:
- 确定了封装环的设计厚度和变形.
- 使用有限元法 (FEM) 开发了一种外结构设计方法.
- 进行了两次隔离测试,隔离环和外之间的距离有所变化,以验证FEM方法.
主要成果:
- 基于FEM的外设计方法得到了验证,封闭环变形误差小于7.5%.
- 实验结果与模拟一致,证实了该方法的正确性.
- 在设计厚度为10毫米的情况下,观察到115%的封闭环变形率.
- 考虑到变形均性和组装错误,纳入了1.05的安全差距.
结论:
- 拟议的外设计方法有效地确保了空气轮发动机轮轮失效的封闭.
- 一个特定的设计参数 (外部外的内部直径是封闭环的外径的1.2倍) 可以防止被变形的封闭环损坏.
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