Volume 31 Issue 9
Sep.  2016
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Article Navigation >  Journal of Aerospace Power  > 2016  >  31(9): 2195-2202
SUN Yang-hui, YANG Kun, HOU Nai-xian, CHEN Jian, BAI Guo-juan. Probabilistic risk assessment method for turbine disk[J]. Journal of Aerospace Power, 2016, 31(9): 2195-2202. doi: 10.13224/j.cnki.jasp.2016.09.019
Citation: SUN Yang-hui, YANG Kun, HOU Nai-xian, CHEN Jian, BAI Guo-juan. Probabilistic risk assessment method for turbine disk[J]. Journal of Aerospace Power, 2016, 31(9): 2195-2202. doi: 10.13224/j.cnki.jasp.2016.09.019
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Probabilistic risk assessment method for turbine disk

doi: 10.13224/j.cnki.jasp.2016.09.019

  • Commercial Aircraft Engine Company Limited, Aviation Industry Corporation of China, Shanghai, 201108, China

  • Received Date: 2015-05-07
  • Publish Date: 2016-09-28
    Abstract
  • For the turbine disk probabilistic risk assessment requirement of CCAR 33.70 airworthiness regulation, the applications of response surface method used in definition of failure zone and estimation of crack growth life were studied. A method of variance reduction of sampling and improving sampling efficiency was demonstrated based on the response surface method to allocate the failure sampling zone during Monte Carlo simulation. It was shown that importance sampling method could significantly improve sampling efficiency:samples rate between failure samples and total samples was 94% by importance sampling method, bigger than traditional direct sampling method (only 33%). The importance sampling method can minimize the total number of samples required to achieve a desired analysis accuracy results. In addition, the life approximation function by response surface method was presented to significantly reduce the computation time of crack growth life:computation time for 104 samples was only 2 minutes by using life approximation function, which was much shorter than traditional life model (288 min). The life error analysis showed that the maximum error was only 1.0%, which had good agreement with traditional method of crack growth life. These results can be applied to improve the efficiency of turbine disk probabilistic risk assessment.

     

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    • References(21)
  • [1]
    United State Department of Transportation,Federal Aviation Administration.Advisory circular 33.70-1:guidance material for aircraft engine-life-limited parts requirements[R].Washington DC:FAA,2009.
    [2]
    National 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 DC:National Transportation Safety Board,NTSB/AAR-90/06,1990.
    [3]
    National Transportation Safety Board.Aircraft accident report:uncontained engine failure,Delta Air Lines Flight 1288,McDonnell Douglas MD-88,N927DA,Pensacola,Florida,July 6,1996[R].Washington DC:National Transportation Safety Board,NTSB/AAR-98/01,1996.
    [4]
    廖敏辉,柴光远.蒙特卡洛法在液压系统可靠性设计中的应用[J].机床与液压,2013,41(11):194-196. LIAO Minhui,CHAI Guangyuan.Application of Monte Carlo simulation in the reliability design of hydraulic system[J].Machine Tool and Hydraulics,2013,41(11):194-196.(in Chinese)
    [5]
    胡肖肖,李育隆,吴宏.基于蒙特卡罗法的航空发动机稳态空气系统网络计算[J].航空发动机,2014,40(6):28-32. HU Xiaoxiao,LI Yulong,WU Hong.Aeroengine steady air system calculation based on Monte Carlo method[J].Aeroengine,2014,40(6):28-32.(in Chinese)
    [6]
    朱本仁.蒙特卡洛方法引论[M].济南:山东大学出版社,1987:30-42.
    [7]
    王进玲,曾声奎,马纪明.基于MCMC的模糊自适应重要抽样法[J].系统工程与电子技术,2012,34(2):317-322. WANG Jinling,ZENG Shengkui,MA Jiming.Fuzzy adaptive importance sampling method based on MCMC[J].System Engineering and Electronics,2012,34(2):317-322.(in Chinese)
    [8]
    刘建平,方越峦.分层抽样层界限确定方法研究[J].统计与决策,2012(3):9-11 LIU Jianping,FANG Yueluan.A method of determining the layer boundaries in stratified sampling[J].Statistics and Decision,2012(3):9-11.(in Chinese)
    [9]
    Lavenberg S S,Welch P D.A perspective on the use of control variables to increase the efficiency of Monte Carlo simulations[J].Management Science,1981,27(3):322-335.
    [10]
    张峰,吕震宙.一种基于混合遗传算法优化的截断重要抽样法[J].应用力学学报,2009,26(1):190-193. ZHANG Feng,LÜ Zhenzhou.An importance sampling method based on hybrid genetic algorithm[J].Chinese Journal of Applied Mechanics,2009,26(1):190-193.(in Chinese)
    [11]
    Karamchandani A,Bjerager P,Cornell C A.Adaptive importance sampling[C]//Proceeding of International Conference on Safety and Reliability.San Francisco:American Society of Civil Engineers,1989:855-862.
    [12]
    陈勇,宋迎东,高德平,等.热、机械载荷作用下夹杂对应力强度因子的影响[J].计算力学学报,2005,22(6):776-779. CHEN Yong,SONG Yingdong,GAO Deping,et al.Effects of inclusion on the stress intensity factor under thermo-mechanical loads[J].Chinese Journal of Computational Mechanics,2005,22(6):776-779.(in Chinese)
    [13]
    毋玲,孙秦.含MSD结构应力强度因子半解析数值算法研究[J].西北工业大学学报,2003,21(2):214-217. WU Ling,SUN Qin.A better method for determining SIF of MSD structure[J].Journal of Northwestern Polytechnical University,2003,21(2):214-217.(in Chinese)
    [14]
    Wu Y T,Enrighe M P,Millwater H R.Efficient and accurate methods for probabilistic analysis of titanium rotors[C]//Proceedings of the 8th ASCE Joint Specialty Conference on Probabilistic Mechanics and Structural Reliability.South Bend,Indiana,US:University of Notre Dame,2000:200-221.
    [15]
    Wu Y T,Enright M P,Millwater H R.Probalistic methods for design assessments of reliability with inspection[J].AIAA Journal,2002,40(5):937-946.
    [16]
    吕大刚,贾明明,李刚.结构可靠度分析的均匀设计响应面法[J].工程力学,2011,28(7):109-115. LÜ Dagang,JIA Mingming,LI Gang.Uniform design response surface method for structural reliability analysis[J].Engineering Mechanics,2011,28(7):109-115.(in Chinese)
    [17]
    Kathleen M C,Natalia Y K,Jeff R.Response surface methodology[R].Computational Analysis of Social and Organizational System Technical Report CMU-ISRI-04-136,2004.
    [18]
    魏大盛,杨晓光,王延荣.基于缺陷概率特点的粉末冶金材料寿命预测概率模型[J].航空动力学报,2005,20(6):951-957. WEI Dasheng,YANG Xiaoguang,WANG Yanrong.A probabilistic model for prediction of life based on probabilistic character of defects in PM alloys[J].Journal of Aerospace Power,2005,20(6):951-957.(in Chinese)
    [19]
    李辉,白广忱.基于响应面法的涡轮盘低循环疲劳可靠性分析方法[J].航空发动机,2008,34(1):28-31. LI Hui,BAI Guangchen.Reliability analysis of low cycle fatigue of turbine disc based on response surface method[J].Aeroengine,2008,34(1):28-31.(in Chinese)
    [20]
    赵国藩.工程结构可靠性理论与应用[M].辽宁大连:大连理工大学出版社,1996.
    [21]
    魏大盛,王延荣,王相平,等.基于应力循环特征的裂纹萌生寿命预测方法[J].航空动力学报,2012,27(10):2342-2347. WEI Dasheng,WANG Yanrong,WANG Xiangping,et al.Life prediction method based on characteristic of cyclic stress[J].Journal of Aerospace Power,2012,27(10):2342-2347.(in Chinese)
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