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飞机座舱盖疲劳试验玻璃老化问题处理方法
引用本文:梁瑞胜,邸祥发,于金苓,王佳莹.飞机座舱盖疲劳试验玻璃老化问题处理方法[J].飞机设计,2010,30(3):23-26.
作者姓名:梁瑞胜  邸祥发  于金苓  王佳莹
作者单位:1. 海军驻沈阳地区航空军事代表室,辽宁,沈阳,110034
2. 沈阳飞机设计研究所,辽宁,沈阳,110035
摘    要:通过统计海南日照时间和飞机实际暴露时间的方法,确定座舱盖老化试验的曝晒时间;通过测试新、老玻璃的疲劳性能曲线,确定老化玻璃的寿命保持率,继而计算用曝晒后的座舱盖进行疲劳试验的时间。

关 键 词:座舱盖  曝晒  寿命保持率  疲劳试验

The Method of Aging Problem in Canopy Fatigue Test
LIANG Run-sheng,DI Xiang-fa,YU Jin-ling,WANG Jia-ying.The Method of Aging Problem in Canopy Fatigue Test[J].Aircraft Design,2010,30(3):23-26.
Authors:LIANG Run-sheng  DI Xiang-fa  YU Jin-ling  WANG Jia-ying
Institution:1. PLA Military Naval Consumer Representative Office in Shenyang, Shenyang 110034, China) (2. Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
Abstract:We received the insolation time of canopy by investigating the sunny time of hainan and the factual time of the uncovered airplane.Through analyzingthe fatigue curves of the new glass and the old , we received the life maintaining ratio of the aging glass,and then calculated the fatigue test time of the insolated canopy.
Keywords:canopy  insolation  the life maintainable ratio  fatigue test
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