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Research of Commercial Aircraft's Battery Layout Design Method Based on Ditching Situation

Conference paper
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Part of the Lecture Notes in Electrical Engineering book series (LNEE, volume 680)

Abstract

From Airworthiness regulation, the electronic power supply system must meet the requirement of power demanding devices which are used to support emergency evacuation of passengers, during emergency landing, including ditching situation. In this situation, the main power supply is often failure, and battery will supply power instead. However, after ditching, the fuselage structure is often damaged, water will flow over into fuselage, if battery, charge or wires are under water and short circuit, then all the devices which are used to support emergency evacuation will failure to work, and passenger evacuation will be very dangerous. For this problem, this paper researches the ditching floating characteristics of commercial aircraft, especially the leakage time of compartment, time-variation of water level, etc. At the same time, this paper analyzes the time of passenger evacuation. Based on those impact facts, this paper researches the battery layout design method of commercial aircraft.

Keywords

Commercial aircraft Battery layout Ditching 

Reference

  1. 1.
    Snow CC, Carroll JJ, Allgood MA (1970) Survival in emergency escape from passenger aircraft. DOT/FAA/AM/70–16, Department of transport, federal aviation administrationGoogle Scholar
  2. 2.
    Hasbrook AH, Garher JD, Snow CC. (1962) Evacuation pattern analysis of a survivable commercial aircraft crash. AD No.282 893Google Scholar
  3. 3.
    Qian L (2018) Study on the selection of battery for civil aircraft. Sci Technol Vis.  https://doi.org/10.19694/j.cnki.issn2095-2457.2018.19.094

Copyright information

© The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2021

Authors and Affiliations

  1. 1.Shanghai Aircraft Design & Research InstituteShanghaiChina

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