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
Research on the characteristic parameters of fire in the cargo hold of aircraft in the presence of combustible materials and an ignition source state.
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Civil Aviation Flight University of China

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V216.8

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    Abstract:

    At present, the civilian aircraft cargo hold is mainly used photoelectric smoke detector as a fire smoke identification, due to the aircraft cargo hold will be suspended in other interference particles (dust, or water vapor, etc.) will trigger the fire detector alarm, there is a high false alarm rate problem. Based on the dual-wavelength photoelectric smoke detector can effectively reduce the problem of high false alarm rate, the collection of aircraft cargo hold typical combustibles as well as interference sources of infrared light scattering power, blue light scattering power as a fire parameter, through the particulate matter of infrared light scattering power and blue light scattering power analysis, as well as a collection of the Sauter average particle size analysis for the subsequent development of composite smoke detector optimization of the fire parameter, the results show that: the infrared and blue light have a good effect on the fire smoke particles, the results of which are: infrared and blue light have a good effect on the fire smoke particles. blue light have a better response to fire smoke particles, combined with the average particle size of Sauter can effectively distinguish between fire smoke particles and non-fire smoke particles, reduce the false alarm rate, the false alarm rate of the interference source does not exceed 6.7%.

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bu zong hao, Wang Hai Bing, Zhang Zhi Hui, liu quanyi. Research on the characteristic parameters of fire in the cargo hold of aircraft in the presence of combustible materials and an ignition source state.[J]. Advances in Aeronautical Science and Engineering,2024,15(4):179-188

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History
  • Received:January 12,2024
  • Revised:June 05,2024
  • Adopted:June 18,2024
  • Online: July 01,2024
  • Published:
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