F100/F110发动机与F-15/F-16战斗机使用故障的统计与分析

梁春华; 王占学; 曹茂国

F100/F110发动机与F-15/F-16战斗机使用故障的统计与分析

1.
西北工业大学动力与能源学院, 西安 71007
2.
中国航空工业集团公司沈阳发动机设计研究所, 沈阳 110015

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- 文章访问数: 2423
- HTML浏览量: 253
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- 被引次数: 0
出版历程
- 收稿日期: 2010-07-06
- 修回日期: 2011-03-09
- 刊出日期: 2011-07-28

Statistics and analysis of critical failures of F100 / F110 engine and F-15 / F-16 fighter during operation

1.
School of Power and Energy, Northwestern Polytechnical University,Xi'an 71007
2.
Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China,Shenyang 110015,China

摘要

摘要: 为借鉴国外航空发动机在设计、研制和使用中积累的经验与教训,通过大量的数据统计与分析,描述美国F-15与F-16战斗机及其装配的F100与F110发动机在使用中发生的重大故障,归纳并总结这些故障在不同阶段、不同部件、不同影响因素的分布情况与规律.分析表明:发动机在前10年或工作35000h左右,故障率高,在之后的较成熟期,故障明显减少;无论是否考虑结构完整性,发动机各种故障会出现在整个使用过程中,但按结构完整性大纲研制的发动机的故障率明显低;在部件故障分布方面,发动机叶轮机是最主要的故障源;在影响因子分布方面,设计、维护、保障和使用不当是发动机出现故障的最主要原因.
- 故障统计 /
- 故障分析 /
- F100发动机 /
- F110发动机 /
- F-15战斗机 /
- F-16战斗机
Abstract: With reference to foreign experience on fighter engine design and development, the critical failures of F-15 and F-16 fighter powered by F100/F110 engine during operation were described based on a great deal of data statistics and analysis. The distribution and respective rules of the failures during operation phases, various components and influential factors were analyzed and concluded. The analysis shows that the failure rate of the engine is high within initial 10 years or 35000 flight hours, then significantly decreases; various engine failures can be exposed during operation, but the failure rate considering the structure integrity is obviously lower than that without considering the structure integrity; the compressor and turbine are main sources of failures; the design, maintenance, support and operation are main influential factors.
- failure statistics /
- failure analysis /
- F100 engine /
- F110 engine /
- F-15 fighter /
- F-16 fighter

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参考文献(36)

[1]	田忠贤,陈光.从国外几起全面停飞事件看发动机研制的艰巨性[J].航空发动机,1995(3):58-62.
[2]	梁春华,李勇.美国军用涡扇发动机故障缘何这么多[J].国际航空,2002(2):29-31.
[3]	U.S. Air Force Safety Center.FY98 mishap statistics[J].Flying Safety,1999,55(1-2):13-34.
[4]	U.S. Air Force Safety Center.FY01 mishap status[J].Flying Safety,2002,58(1-2):20-50.
[5]	Greenwood R.The Pratt & Whiteney F100:a primer on inspecting for 3rd stage LPT blade 6 tip curling[J].Flying Safety,2000,56(8):22-26.
[6]	Greenwood R.Augmentor no-light troubleshooting on the F100-PW-220/220 engine[J].Flying Safety,2000,57(8):10-11.
[7]	Rodwell A.Engine bearing failure:detection improved with new technology[J].Flying Safety,2002,59(8):24-25.
[8]	Holritz R T,Engle R B.F110 compressor failures[J].Flying Safety,1992(3):26-27.
[9]	Bradford W D.Engine mishap investigation[J].Flying Safety,1986(11):10-12.
[10]	Benninger R,Wagner B.F-16 mishap summary[J].Flying Safety,1993(1):14-15.
[11]	Engle R B,Wagner B.F-16 logistics mishap summary[J].Flying Safety,1994(1):16-18.
[12]	Burke C K.F-15 eagle mishap review’94[J].Flying Safety,1995(1):14-15.
[13]	Wagner W N.F-16 year in review[J].Flying Safety,1995(1):16-17.
[14]	Wagner B,Wood D.F-16 engine-related mishap summary[J].Flying Safety,1995(1):18-19.
[15]	Wood D.FY95 engine-related mishap summaries[J].Flying Safety,1996,51(2-3):40-44.
[16]	Wood D, Bradford B.FY96 engine-related mishap summaries[J].Flying Safety,1996,52(12)/1997,53(1):38-42.
[17]	Bradford B,Greenwood R,Bloomfield B.FY97 engine-related mishap summaries[J].Flying Safety,1998,54(2):24-26.
[18]	Bradford B,Greenwood R,Bloomfield B,et al.FY98 engine-related mishap summary[J].Flying Safety,1999,55(4):22-27.
[19]	Bradford B,Rose S,Bloomfield B,Greenwood R.Engine review:FY99 engine-related mishaps[J].Flying Safety,2000,56(1-2):35-43.
[20]	Bradford B,Greenwood R,Maynard J,et al.FY00 engine-related mishap summary[J].Flying Safety,2001,57(1-2):24-27.
[21]	Bradford B,Fehringer T,Greenwood R,et al.FY01 engine-related mishap summary[J].Flying Safety,2002,58(1-2):42-47.
[22]	Bradford B, Fehringer T,Greenwood R,et al.FY02 engine-related mishap summary[J].Flying Safety,2003,59(1-2):46-53.
[23]	Bradford B,Greenwood R,Maynard J.FY03 engine-related mishap summary[J].Flying Safety,2004,60(1-2):22-26.
[24]	Mcdonald B,Bradford B,Greenwood R,et al.FY04 year in review:engines[J].Flying Safety,2005,61(1-2):48-54.
[25]	Mcdonald B,Bradford B,Greenwood R,et al.FY05 year in review:engines[J].Flying Safety,2006,62(1-2):44-51.
[26]	Mcdonald B,Greenwood R,Wolf B.FY06 year in review:engines[J].Flying Safety,2007,63(1-2):44-49.
[27]	Bradford B,Greenwood R,Wolf B.FY07 year in review:engines[J].Flying Safety,2008,64(1-2):42-48.
[28]	Hembree C.FY08 year in review:engines[J].Flying Safety,2009,65(1-2):40-44.
[29]	Hoffart T.FY05 year in review:F-15[J].Flying Safety,2006,62(1-2):18-19.
[30]	Resnik B.FY05 year in review:F-16[J].Flying Safety,2006,62(1-2):20-21.
[31]	Rodent M B.FY06 year in review:F-15[J].Flying Safety,2007,63(1-2):16-17.
[32]	Hoffart T.FY06 year in review:F-16[J].Flying Safety,2007,63(1-2):18-21.
[33]	Rodent M B.FY07 year in review:F-15[J].Flying Safety,2008,64(1-2):14-15.
[34]	Hoffart T.FY07 year in review:F-16[J].Flying Safety,2008,64(1-2):16-21.
[35]	Rodent M B.FY08 year in review:F-15[J].Flying Safety,2009,65(1-2):10-11.
[36]	Ferenczhalmy T.FY08 year in review:F-16[J].Flying Safety,2009,65(1-2):16-18.