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CESSNA172R飞机飞行操纵钢索故障原因分析 被引量:8

Analysis on failure cause of flight control cable in CESSNA172R aircrafts
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摘要 CESSNA172R飞机飞行操纵(副翼、升降舵、方向舵、襟翼)系统钢索多次发生磨损、断裂故障,严重威胁了飞行安全。根据该机型结构设计特点,通过相似机型系统类比、数据可靠性分析等方法分析了各飞行操纵系统钢索失效的主要原因,提出了预防飞行操纵钢索失效的措施。通过调整飞机的操纵钢索系统的维护周期,改进钢索的检查和维护技术,提高飞机在全寿命周期中的安全可靠性。 Cable wear or broken have happened repeatedly in flight control system including aileron, elevator, rudder, flap, causing serious threat to the flight safety. According to the characters of aircraft frame design, by means of similar aircraft comparison and reliability data analysis, the main causes of cable failure in each flight control system were found out, and the prevention measures were proposed. Through the adjustment on maintenance schedule of the aircraft control cable, and improving the cable inspection and maintenance technology, the safety and relia- bility of aircraft in the whole life cycle can be improved.
出处 《中国安全生产科学技术》 CAS CSCD 2014年第2期155-159,共5页 Journal of Safety Science and Technology
基金 中国民用航空飞行学院科研基金项目(J2012-17)
关键词 CESSNA172R 飞机 故障 钢索 CESSNA172R aircraft failure cable
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参考文献10

  • 1张清平.飞机钢索及相关主要部件的维护[J].科技传播,2010,2(14):87-87. 被引量:7
  • 2Piper Aircraft, Inc. PA-44-180 Airplane Maintenance Manual [ M ]. Revision PR091231. Florida 32960 U. S. A. :Piper Aircraft Inc. , 2009. Page 3C17 to Page 3D5.
  • 3Piper Aircraft, Inc. PA-44-180 Airplane Parts Catalog [ M]. Revision PR 091210. Florida 32960 U. S. A. :Piper Aircraft, Inc. ,2009. Page li18 to Page li20.
  • 4Cessna Aircraft Company. Model 172R/172S Maintenance Manual[ M]. Rev 20. Wichita Ks67226 United States: Cessna Aircraft Company,2012. 27-10-00.
  • 5Cessna Aircraft Company. Model 172R/172S Illustrated Parts Catalog [ M ], Rev 20. Wichita Ks67226 United States : Cessna Aircraft Company ,2012. 27-10-00.
  • 6Cirrus Aircraft Company. Model SR20 Cirrus Airplane Maintenance Manual [ M ]. Cirrus Aircraft Company, 2013. 27-10.
  • 7Cirrus Aircraft Company. Model SR20 Cirrus Airplane Il- lustrated Parts Catalog [ M ]. Cirrus Aircraft Company, 2013. 27-10.
  • 8FAA43. 13-1b, Acceptable Methods, Techniques, and PracticesAircraft Inspection And Repair[ M ]. Change 1. U. S. A. FAA. 1998. Chanter7. Pae 7-28.
  • 9刘庭耀,赵晓辉.飞机操纵系统钢索断裂原因分析[J].失效分析与预防,2009,4(4):247-250. 被引量:24
  • 10罗裕富.Cessna172R飞机操作系统钢索分析[J].科技风,2012(20):55-55. 被引量:6

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