某型飞机机翼Ⅱ梁框检修周期的计算
The overhaul periods’calculation of the second crossbeam of certain aircraft’s aerofoil
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摘要: 本文建立某型飞机Ⅱ梁框结构裂纹形成寿命Np与裂纹扩展寿命NP*之间的可靠度模型,将安全寿命设计与损伤容限设计原理有机结合,计算了在给定结构可靠度下该型飞机机翼Ⅱ梁框的检修周期.Abstract: The reliability model between crack formation life and crack growth life is set up.The overhaul periods of the Second Crossbeam of Certain Aircraft's Aerofoil are calculated from the reliability model.