Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Reliability Analysis of Sensor Module of Helicopter Emergency Flotation System
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Affiliation:

1.Nanjing University of Aeronautics and Astronautics;2.Aviation Key Laboratory of Science and Technology on Life-support Technology;3.Nanjing University of Aeronautics &4.amp;5.Astronautics

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{V240.2}

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    Abstract:

    In order to ensure the safe operation of emergency flotation system for helicopters and trigger reliably in the process of impacting on water, the reliability of sensor module, the key component of the system, is analyzed. Based on the systematic understanding of k/n(G) voting system composed of different types of units, Monte Carlo simulation platforms of sensor module under different logic relations are built by using Matlab/Simulink, and the corresponding simulation & theoretical calculation are carried out. The results show that it is feasible and effective to apply Monte Carlo method to reliability analysis of sensor module. According to the results of functional hazard analysis and reliability analysis, the 3/5 voting system is more suitable for the sensor module of the helicopter emergency flotation system. This provides a technical route for the logical relationship selection and reliability design of similar modules.

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guoxing, Sun Jian-hong, Li Ming-qi, Ma Fang-yun, Sun Zhi. Reliability Analysis of Sensor Module of Helicopter Emergency Flotation System[J]. Advances in Aeronautical Science and Engineering,2020,11(4):532-539

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History
  • Received:June 14,2019
  • Revised:July 22,2019
  • Adopted:July 31,2019
  • Online: August 25,2020
  • Published: