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持续适航阶段民用航空发动机故障风险分析与评估 被引量：3

Risk Analysis and Assessment of Civil Aeroengine Failure during Continued Airworthiness
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摘要 介绍了国外民用航空发动机故障的风险分析及评估办法;以某涡轮风扇发动机第8级压气机盘断裂故障为对象,进行了风险分析与评估。 The method of the risk analysis and assessment of foreign civil aeroengine failure was introduced.The risk analysis and assessment of the eighth stage compressor disc fracture for a turbofan engine was conducted.
作者 高艳蕾 周燕佩
机构地区 中国民用航空总局航空安全技术中心
出处 《航空发动机》 2010年第3期50-53,共4页 Aeroengine
关键词 航空发动机 风险管理 持续适航 aeroengine risk management continued airworthiness
分类号 V235.13 [航空宇航科学与技术—航空宇航推进理论与工程]
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参考文献5

  • 1Tim Bedford,Roger Cooke.Probabilistic Risk Analysis: Foundatiotis and Methods.Cambridge University Press, 2001.
  • 2US Department of Transportation Federal Aviation Administration, Advisory Circular, continued airworthiness assessments of powerplant and auxiliary power unit installations of transport category airplanes, Initiated By AIR-100,sep. 8, 2003.
  • 3a joint effort of the federal aviation administration and the aerospace industries association (AIA), Technical Report on Propulsion System and APU-Related Aircraft Safety Hazards, October 25, 1999.
  • 4a joint effort of the federal aviation administration and the aerospace industries association (AIA), 2nd Technical Report on Propulsion System and APU-Related Aircraft Safety Hazards, January 31, 2005.
  • 5John P. Kindinger and John L. Darby, Risk Factor Analysis-A New Qualitative Risk Management Tool, Proceedings of Project Management Institute Annual Seminars & Symposium, 2000.

同被引文献29

  • 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
  • 2Vittal S, Hajela P, Joshi A. Review of approaches to gas turbine life management[ R]. AIAA-2004-4372, 2004.
  • 3Kappas J. Review of risk and reliability methods for aircraft gas turbine engines [ R ]. DSTO-TR- 1306, 2002.
  • 4Green 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.
  • 5Enright 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.
  • 6Southwest 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.
  • 7Millwater 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.
  • 8Millwater H, Larsen J, John R. Effects of residual stresses on probabilistic lifing of engine disk materials [ J ] Materials Science and Engineering: A, 21307,d68-470:129-136.
  • 9Millwater 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.
  • 10Huyse L, Enright M P. Efficient statistical analysis of failure risk in engine rotor disks using importance sampling techniques[ R]. AIAA-2003-1838, 2003.

引证文献3

二级引证文献7

航空发动机
2010年 第3期

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