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等效疲劳寿命及其在疲劳可靠性设计中的应用

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针对结构疲劳性能评估的成本高、样件少问题,分析并确定一种适用于超小样本量样件的P-S-N(疲劳寿命可靠性设计曲线)测定方法——等效疲劳寿命P-S-N方法.针对航空航天领域常用的四种金属材料:18Cr2Ni4WA钢、LY12CZ铝合金、Ti-6Al-4V钛合金、Incoloy 903高温合金,通过将等效疲劳寿命P-S-N方法与GJB/Z 18A 2005、ISO 12107:2012、ASTM推荐的三种方法对比,并分析了不同试验方案下各个方法获得P-S-N的准确性、稳定性、灵活性.结果表明等效疲劳寿命P-S-N方法结果准确,并具有低成本、高效率的特点,可为疲劳寿命可靠性设计曲线的确定提供新方法.
Equivalent Fatigue Life and Its Application in Fatigue Reliability Design
For the high cost and few specimens of the fatigue property evaluation of the key components,a very small sampling P-S-N(fatigue life reliability design curve)measurement method,which is named as the equivalent fatigue life method(EQ method)is analyzed and determined.The EQ method is applied to fitting the P-S-N of the four metals widely used in aeronautics and astronautics:18Cr2Ni4WA steel,LY12CZ aluminum alloy,Ti-6Al-4V titanium alloy and Incoloy 903 high temperature alloy,which also are compared with the standard methods suggested by GJB/Z 18A 2005,ISO 12107:2012 and ASTM.Finally,the accuracy and test time of P-S-N determined by different methods are analyzed.The results indicate that the equivalent fatigue life method can measure the P-S-N curves with low cost and high efficiency,which can be suggested to determine the fatigue life reliability design curve.

equivalent fatigue lifeP-S-Nfatigue reliabilityvery small sample size

白鑫、张鹏、张哲峰、谢里阳

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中国科学院金属研究所 沈阳 110016

东北大学机械工程与自动化学院 沈阳 110819

等效疲劳寿命 P-S-N 疲劳可靠性 超小样本

2024

机械工程学报
中国机械工程学会

机械工程学报

CSTPCD北大核心
影响因子:1.362
ISSN:0577-6686
年,卷(期):2024.60(22)