| 可靠性设计中材料屈服极限的最佳选择 |
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| 引用本文： | 古远,洪其麟,张跃春,李树良.可靠性设计中材料屈服极限的最佳选择[J].航空动力学报,1994,9(3):301-303,336. |
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| 作者姓名： | 古远 洪其麟 张跃春 李树良 |
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| 作者单位： | 北京航空航天大学，株洲航空动力机械研究所，中国南山开发股分有限公司 |
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| 摘 要： | 根据航空发动机结构完整性大纲，对于断裂关键件必须进行损伤容限设计分析。由于材料缺陷，加工缺陷或疲劳引起裂纹的扩展，都会导致构件断裂，为此要求在有缺陷（裂纹）的情况下，构件应能保持足够的损伤容限，这主要靠正确选用材料，控制应力水平，采用抗断裂结构，控制加工精度及采用可靠的检查方法来实现。
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| 关 键 词： | 可靠性设计 损伤 屈服极限 |
| 收稿时间： | 6/1/1993 12:00:00 AM |
| 修稿时间： | 7/1/1993 12:00:00 AM |
OPTIMIZATION OF MATERIALS YIELD LIMIT FOR RELIABILITY DESIGN |
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| Gu Yuan,Hong Qilin,Zang Yuedun and Li Shuliang.OPTIMIZATION OF MATERIALS YIELD LIMIT FOR RELIABILITY DESIGN[J].Journal of Aerospace Power,1994,9(3):301-303,336. |
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| Authors: | Gu Yuan Hong Qilin Zang Yuedun and Li Shuliang |
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| Institution: | 4th Dept.,Beijing University of Aeronautics and Astronautics,Beijing 100083;4th Dept.,Beijing University of Aeronautics and Astronautics,Beijing 100083;Aeroengine Institute 608 412002 |
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| Abstract: | According to aeroengine structure integrity program,fracture critical components must be analysed with damage tolerance concept.Due to crack propagation produced by material defects,working defects or fatigue defects can make structure fracture.Therefore,the sufficient damage tolerance should be maintained.It is realized by selecting material correctly,controlling stress level,using the anti fracture structures and reliable inspection.In this paper,the structural reliability concept is applied to studying optimization of materials for maximum reliability under certain stress levels and crack sizes,to investigating variation influences of material strength and stress level on structure reliability. |
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| Keywords: | Reliability design Damage Yield limit |
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