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Method of civil aircraft emergency electrical power requirement analysis based on Systems Engineering
Author(s) -
Zhiqiao Zhao,
Jun Zhang
Publication year - 2022
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/2252/1/012061
Subject(s) - architecture , electricity , electric power system , power (physics) , function (biology) , electric power , work (physics) , engineering , electrical equipment , systems architecture , systems engineering , reliability engineering , automotive engineering , control engineering , computer science , electrical engineering , mechanical engineering , art , physics , quantum mechanics , evolutionary biology , visual arts , biology
In this paper, the minimum function of civil aircraft power supply emergency is defined based on the model- based system engineering method and the principle of ensuring aircraft flight safety. Through functional architecture-logical architecture-physical architecture modeling, realize the mapping from minimum functions to minimum equipment. The system equipment that needs to work under the emergency electrical power supply of each aircraft system is sorted out from the forward direction, and the electricity requirements of the electrical equipment in different scenarios are analyzed statistically, and then the emergency electrical power requirements of the whole aircraft are obtained as the design input of the electrical power system.

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