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转子爆破对飞机机体结构危害的风险量化方法研究 被引量:4

Risk Quantification Method for Airframe Damage due to Rotor Burst
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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。 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.
作者 杨万里
出处 《航空发动机》 2012年第3期29-33,41,共6页 Aeroengine
关键词 民用飞机 结构设计 风险量化 转子爆破 非包容性 commercial aircraft structure design risk quantification rotor burst uncontainment
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参考文献8

二级参考文献14

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共引文献24

同被引文献23

  • 1陈志达.民航客机发动机转子非包容性损坏分析[J].航空制造技术,2011,0(13):75-79. 被引量:12
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  • 8TSO C77b Technology standard order. GAS Turbine Auxiliary Power Units [ S ]. Boston : Federal Aviation Administration, 2000.
  • 9白杰,付仁合,王伟.非包容性失效条件下飞机蒙皮厚度的算法[J].工程设计学报,2010,17(6):444-448. 被引量:2
  • 10李雪姣,付仁合.航空发动机非包容性碎片的危害评估方法研究[J].装备制造技术,2011(2):21-23. 被引量:7

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