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Fatigue Analysis of Composite Materials Using the Fail-Safe Concept

机译：基于故障安全概念的复合材料疲劳分析

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If R1 is the probability of having a crack on a flight component and R2 is the probability of seeing this crack propagate between two scheduled inspections, the global failure regulation states that this product must not exceed 0.0000001.

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作者
Stievenard, G.;
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年度 1982
页码 p.1-11
总页数 11
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aircraft structures; Component reliability; Composite structures; Fail-safe systems; Failure analysis; Fatigue life; Helicopter design; Helicopters; Costs; Crack propagation; Cracks; Probability theory; Risk; Rotors; Rupturing; Vibrational stress;

机译：飞机结构;部件可靠性;复合结构;故障安全系统;故障分析;疲劳寿命;直升机设计;直升机;成本;裂纹扩展;裂缝;概率论;风险;转子;破裂;振动应力;

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Fatigue Analysis of Composite Materials Using the Fail-Safe Concept

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