留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

航空发动机部件故障风险评估方法研究

徐庆宏 孙有朝 李龙彪

徐庆宏, 孙有朝, 李龙彪. 航空发动机部件故障风险评估方法研究[J]. 机械科学与技术, 2016, 35(8): 1291-1296. doi: 10.13433/j.cnki.1003-8728.2016.0823
引用本文: 徐庆宏, 孙有朝, 李龙彪. 航空发动机部件故障风险评估方法研究[J]. 机械科学与技术, 2016, 35(8): 1291-1296. doi: 10.13433/j.cnki.1003-8728.2016.0823
Xu Qinghong, Sun Youchao, Li Longbiao. Study on Risk Assessment Method for Aero-engine Component Failure[J]. Mechanical Science and Technology for Aerospace Engineering, 2016, 35(8): 1291-1296. doi: 10.13433/j.cnki.1003-8728.2016.0823
Citation: Xu Qinghong, Sun Youchao, Li Longbiao. Study on Risk Assessment Method for Aero-engine Component Failure[J]. Mechanical Science and Technology for Aerospace Engineering, 2016, 35(8): 1291-1296. doi: 10.13433/j.cnki.1003-8728.2016.0823

航空发动机部件故障风险评估方法研究

doi: 10.13433/j.cnki.1003-8728.2016.0823
基金项目: 

国家自然科学基金委员会与中国民用航空局联合项目(U1333119)、中国民用航空局科技计划项目(MHRD201123,MHRD200817,MHRD200908)及国防科工局技术基础科研项目(Z052013B003)资助

详细信息
    作者简介:

    徐庆宏(1961-),博士研究生,研究方向为大型飞机可靠性与安全性工程,xuqinghong@comac.cc

    通讯作者:

    孙有朝(联系人),教授,博士生导师,sunyc@nuaa.edu.cn

Study on Risk Assessment Method for Aero-engine Component Failure

  • 摘要: 在已有的航空发动机历史故障数据的基础上,采用蒙特卡洛方法建立了航空发动机部件故障风险仿真模型,给出了发动机故障危险等级划分、危险系数确定和风险因子计算的方法,预测了发动机故障的发生情况,评估了发动机运营阶段的故障风险,确保使用可靠性与安全性。根据故障事件危险等级及相应的风险准则对某型号发动机进行了风险评估,制定了3种合理的可降低风险方案,分别对3种方案重新进行蒙特卡洛仿真与及风险评估,分析了不同维修方式和维修周期对风险因子的影响,制定出最合理的降低风险方案。
  • [1] Vittal S,Hajela P,Joshi A.Review of approaches to gas turbine life management[R].AIAA-2004-4372,2004
    [2] Kappas J.Review of risk and reliability methods for aircraft gas turbine engines[R].DSTO-TR-1306,2002
    [3] Green A J.The future direction and development of engine health monitoring (EHM) within the United States air force[C]//Proceedings of JOAP International Condition Monitoring Conference.Arlington,VA:[s.n.],1998
    [4] Enright M P,Hudak S J,McClung R C,et al.Probabilistic-based system for prognosis of fatigue in aircraft engine components[C]//Proceedings of the 44th AIAA/ASME/ASCE/AHS Structures,Structural Dynamics and Materials Conference,Non-Deterministic Approaches Forum4.Norfolk,VA:AIAA,2003
    [5] Southwest Research Institute,Allied Signal,General Electric,et al.Turbine rotor material design,phase 1 final report[R].FAA Grant 95-G-041,Washington,DC:Federal Aviation Administration,2000
    [6] Millwater 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
    [7] Millwater H,Larsen J,John R.Effects of residual stresses on probabilistic lifing of engine disk materials[J].Materials Science and Engineering:A,2007,468-470:129-136
    [8] Millwater H R,Fitch S H K,Wu J,Enright M P.A probabilistically-based damage tolerance analysis computer program for hard alpha anomalies in Titanium rotors[C]//ASME Turbo Expo 2000:Power for Land,Sea,and Air.San Antonio,TX:ASME,2000
    [9] Huyse L,Enright M P.Efficient statistical analysis of failure risk in engine rotor disks using importance sampling techniques[R].AIAA-2003-1838,2003
    [10] Huyse L,Enright M P.Efficient conditional failure analysis:application to an aircraft engine component[J].Structure and Infrastructure Engineering,2006,2(3-4):221-230
    [11] Leverant G R,McClung R C,Millwater H R,et al.A new tool for design and certification of aircraft turbine rotors[C]//Proceedings of the 47th ASME International Gas Turbine&Aeroengine Technical Congress.Amsterdam,The Netherlands:ASME,2002
    [12] Leverant G R,Millwater H R,McClung R C,et al.A new tool for design and certification of aircraft turbine rotors[J].Journal of Engineering for Gas Turbines and Power,2004,126(1):155-159
    [13] U.S.Department of Transportation,Federal Aviation Administration.Advisory circular 39-8:continued airworthiness assessments of powerplant and auxiliary power unit installations of transport category airplanes[S].Washington,DC:FAA,AC 39-8,2003
    [14] 虞兰.航空发动机故障风险仿真评估方法[J].上海大学学报(自然科学版),1997,3(1):106-110 Yu L.Simulation assessment method of failure risk for aeronautical engines[J].Journal of Shanghai University (Natural Science),1997,3(1):106-110(in Chinese)
    [15] 高艳蕾,周燕佩.持续适航阶段民用航空发动机故障风险分析与评估[J].航空发动机,2010,36(3):50-53 Gao Y L,Zhou Y P.Risk analysis and assessment of civil aeroengine failure during continued airworthiness[J].Aeroengine,2010,36(3):50-53(in Chinese)
    [16] Technical report on propulsion system and APU-related aircraft safety hazards[R].FAA and AIA,1999
  • 加载中
计量
  • 文章访问数:  238
  • HTML全文浏览量:  43
  • PDF下载量:  8
  • 被引次数: 0
出版历程
  • 收稿日期:  2014-09-09
  • 刊出日期:  2016-08-05

目录

    /

    返回文章
    返回