| 转子爆破对飞机机体结构危害的风险量化方法研究 |
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| 引用本文： | 杨万里.转子爆破对飞机机体结构危害的风险量化方法研究[J].航空发动机,2012,38(3):29-33. |
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| 作者姓名： | 杨万里 |
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| 作者单位： | 中航工业上海飞机设计研究院,上海200232 |
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| 摘 要： | 结合某型民用飞机转子爆破对机体结构危害的风险量化分析经验，通过对系统的处理方法进行类比，以概率统计为基础，将转子爆破对飞机机体的危害进行分级量化，形成了1套典型分析方法，可为其他型号飞机的相关设计工作提供借鉴。
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| 关 键 词： | 民用飞机 结构设计 风险量化 转子爆破 非包容性 |
Risk Quantification Method for Airframe Damage due to Rotor Burst |
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| Authors: | YANG Wan-li |
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| Institution: | YANG Wan-li (AVIC Shanghai Aircraft Design and Research Institution, Shanghai 200232, China) |
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| Abstract: | Combined with the hazard quantification analysis experience on commercial aircraft damage due to rotor burst , a typical analysis method was provided , which the hazards was classified into several levels based on statistics and compared withflight systems＂ rotor burst analysis. The method can provide references for the related design of other aircrafts. |
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| Keywords: | commercial aircraft structure design risk quantification rotor burst uncontainment |
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