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Aircraf Bearing Life Reliability Design and Analysis under Multiple Distributed Loads with AFSOM Method
Yang GX(杨广新); Liu GQ(刘广琦); Hu, Yongqiang; Luo HT(骆海涛)
作者部门空间自动化技术研究室
会议名称IEEE/CSAA International Conference on Aircraft Utility Systems (AUS)
会议日期October 10-12, 2016
会议地点Beijing, PEOPLES R CHINA
会议主办者IEEE, Chinese Soc Aeronaut & Astronaut, Org Aviat Util Syst Engn, Natl Key Lab Sci & Technol Aircraft Control, IEEE Control Syst Soc, Nanjing Chapter, Beihang Univ, AVIC Electromechan Syst Co Ltd, State Key Lab Civil Aircraft Flight Simulat, COMAC, Aviat Key Lab Sci & Technol Aero Electromechan Syst Integrat, Fluid Power Transmiss & Control Inst, CMES
会议录名称2016 IEEE/CSAA INTERNATIONAL CONFERENCE ON AIRCRAFT UTILITY SYSTEMS (AUS)
出版者IEEE
出版地New York
2016
页码1079-1082
收录类别EI ; CPCI(ISTP)
EI收录号20165203173040
WOS记录号WOS:000390257400208
产权排序2
ISBN号978-1-5090-1087-5
摘要Accurate design and calculation of the aircraft bearing life reliability have the significant importance for the reliability design of the aviation subsystem components. This paper proposes a new method for solution of the bearing life reliability by AFSOM method under considering load fluctuation. When the bearing life reliability is between 0.4 and 0.9, the bearing reliable life obeys the two parameter Weibull distribution; According to that, the relationship between the bearing life reliability and the reliable life correction coefficient is established. When the bearing life reliability is between 0.9 and 1, the function is established based on the curve fitting. By considering the load fluctuation, reliable life correction coefficient and the limit state equation of bearing life reliability, it can solve the bearing life reliability through the AFSOM method. This method is easy and reasonable, highly reliable and suitable for engineering application.
语种英语
引用统计
文献类型会议论文
条目标识符http://ir.sia.cn/handle/173321/19765
专题空间自动化技术研究室
通讯作者Liu GQ(刘广琦)
作者单位1.Guidaojiaotong Polytechnic Institute, Shenyang, 110016, China
2.State Key Laboratory of Robotics, Shenyang Institute of Automation, CAS, Shenyang, 110016, China
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GB/T 7714
Yang GX,Liu GQ,Hu, Yongqiang,et al. Aircraf Bearing Life Reliability Design and Analysis under Multiple Distributed Loads with AFSOM Method[C]//IEEE, Chinese Soc Aeronaut & Astronaut, Org Aviat Util Syst Engn, Natl Key Lab Sci & Technol Aircraft Control, IEEE Control Syst Soc, Nanjing Chapter, Beihang Univ, AVIC Electromechan Syst Co Ltd, State Key Lab Civil Aircraft Flight Simulat, COMAC, Aviat Key Lab Sci & Technol Aero Electromechan Syst Integrat, Fluid Power Transmiss & Control Inst, CMES. New York:IEEE,2016:1079-1082.
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