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RELIABILITY AND DAMAGE TOLERANCEANALYSIS FOR AIRCRAFT PROPELLER
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作者 Fei Binjun gao zhentong(institute of solid mechanics, beijing university ofaeronautics and astronautics, beijing, china, 100083) 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 1994年第4期269-275,共7页
he stress-strength interferenee model can be used for the structure with-out fatigue cracks. It is not available for the structure that is often damaged slightlysuch as propellers. A two-dimensional interferenee relia... he stress-strength interferenee model can be used for the structure with-out fatigue cracks. It is not available for the structure that is often damaged slightlysuch as propellers. A two-dimensional interferenee reliability model using thetwo-dimensional fatigue load distribution and the distribution of fatigue crack growththreshold for the reliability of the structure with fatigue crack is established. The relia-bility of the propeller of Y7-200B with different crack sizes is listed. A damage toler-ance analysis using an interference integration formula with the two-dimensional loaddistribution is carried out for the propeller and the fatigue crack inspection period withgiven reliability is presented. 展开更多
关键词 PROPELLERS RELIABILITY damage assessment
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