期刊文献+

航空发动机限寿件高效失效概率算法研究综述

Review on efficient algorithm of failure probability for aero-engine life limited parts
原文传递
导出
摘要 综述了为提高失效概率计算效率的研究成果,包括基于抽样的高效失效概率算法和基于积分的高效失效概率算法。其中,基于抽样的高效失效概率算法在传统蒙特卡洛模拟方法的基础上,通过重要性抽样方法在失效域抽样、最优抽样技术优化分区样本量、分区细化技术减少分区数量,从而减少蒙特卡洛模拟样本量。另外,基于积分的高效失效概率算法通过建立N次飞行循环与初始循环(N=0)随机变量空间的映射关系,解决了时变失效区域中概率密度函数难以求解的困难。在与蒙特卡洛相对误差小于5%条件下,积分算法时间成本降低了数十倍。 The research results for improving the efficiency of failure probability calculation,including the efficient sampling-based algorithms and the efficient integration-based algorithms, were summarized. Among them, based on the traditional Monte Carlo simulation method, the importance sampling algorithm generated samples in the failure domain. The optimal sampling technology optimized the zone sample size. The zone refinement technology reduced the number of zones,thus reducing the Monte Carlo simulation sample size. In addition,the direct integration was realized by establishing the mapping relationship of failure domain at N flight cycles and the initial(N = 0) flight cycles based on the probability density theory. When the relative error with Monte Carlo was less than 5%,the calculation time cost was reduced by at least tens of times.
作者 李果 刘俊博 周惠敏 丁水汀 LI Guo;LIU Junbo;ZHOU Huimin;DING Shuiting(School of Energy and Power Engineering,Beihang University,Beijing 100191,China;Civil Aviation University of China,Tianjin 300300,China)
出处 《航空动力学报》 EI CAS CSCD 北大核心 2022年第11期2398-2407,共10页 Journal of Aerospace Power
关键词 航空发动机 寿命限制件 高能转子轮盘 概率失效风险评估 高效失效概率算法 数值积分算法 蒙特卡洛方法 aero-engine life limited parts high energy rotor disk probabilistic failure risk assessment efficient algorithm of failure probability numerical integration algorithm Monte Carlo method
  • 相关文献

参考文献2

二级参考文献26

  • 1Federal Aviation Administration.Advisory circular 33.75-1A:guidance material for 14 CFR §33.75,safety analysis[R].Washington D C:Federal Aviation Administration,2007.
  • 2Federal Aviation Administration.e-CFR 14 part 33,airworthiness standards:aircraft engines[S].Washington D C:Federal Aviation Administration,2009.
  • 3Federal Aviation Administration.Advisory circular 33.70-1:guidance material for aircraft engine-life-limited parts requirements[R].Washington D C:Federal Aviation Administration,2009.
  • 4Federal Aviation Administration.Advisory circular 33.14-1:damage tolerance for high energy turbine engine rotors[R].Washington D C:Federal Aviation Administration,2001.
  • 5National Transportation Safety Board.Aircraft accident report:United Airlines Flight 232 McDonnell Douglas DC-10-10 Sioux Gateway Airport,Sioux City,Iowa,July 19,1989[R].Washington D C:National Transportation Safety Board NTSB/AAR-90/06,1990.
  • 6National Transportation Safety Board.Aircraft accident report:Uncontained engine failure,Delta Airlines Flight 1288,McDonnell Douglas MD-88,N927DA,Pensacola,Florida,July 6,1996[R].Washington D C:National Transportation Safety Board NTSB/AAR-98/01,1998.
  • 7Leverant G R,Littlefield D L,McClung R C,et al.A probabilistic approach to aircraft turbine rotor material design[R].ASME Paper 97-GT-22,1997.
  • 8Millwater H R,Enright M P,Fitch S H K.A convergent probabilistic technique for risk assessment of gas turbine disks subject to metallurgical defects[R].AIAA 2002-1382,2002.
  • 9Wu Y T,Enright M P,Millwater H R.Probabilistic methods for design assessment of reliability with inspection[J].AIAA Journal,2002,40(5):936-946.
  • 10McClung R C.Fracture mechanics analysis in DARWIN[C]//Application of Probabilistic Methods to Gas Turbine Engines.Jacksonville,Florida,US:FAA/USAF Workshop,1999:1-22.

共引文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部