| 含置信度叶片疲劳寿命可靠性试验技术 |
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| 引用本文： | 庄忠良,高德平,鲁启新.含置信度叶片疲劳寿命可靠性试验技术[J].航空动力学报,1989,4(3):209-212,289. |
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| 作者姓名： | 庄忠良 高德平 鲁启新 |
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| 作者单位： | 南京航空学院
(庄忠良，高德平)，南京航空学院(鲁启新) |
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| 摘 要： | 本文指出在进行叶片可靠性试验时,不仅要考虑可靠度指标要求,还必须综合考虑置信度、可靠度,小样特性和模拟试验技术等等因素。从这一观点出发,本文提出了一种较合理的确定叶片疲劳寿命的可靠性试验。这种技术也适用于其它零件的疲劳寿命试验。
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| 收稿时间： | 1/1/1989 12:00:00 AM |
RELIABILITY TESTING TECHNIQUE OF BLADING FATIGUE WITH CONFIDENCE LEVEL |
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| Zhuang Zhongliang,Gao Deping and Lu Qixin.RELIABILITY TESTING TECHNIQUE OF BLADING FATIGUE WITH CONFIDENCE LEVEL[J].Journal of Aerospace Power,1989,4(3):209-212,289. |
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| Authors: | Zhuang Zhongliang Gao Deping and Lu Qixin |
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| Institution: | Nanjing Aeronautical Institute;Nanjing Aeronautical Institute;Nanjing Aeronautical Institute |
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| Abstract: | During reliability testing of binding fatigue, it is necessary to consider neronly its reliability, bul also its confidence, characteristics of specimens. simulation technique ana so on simultaneously. In this view, a reliability testing technique with confidence level is presented which can estimate blading fatigue life more reasonably. This technique also can be applied to predicting fa-tigue life of other mechanical parts. |
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