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Title:
航空機の電力網を管理するための方法
Document Type and Number:
Japanese Patent JP6396325
Kind Code:
B2
Abstract:
A method for managing an electrical power supply system (1) of an aircraft, the power supply system (1) comprising at least one distribution bus arranged so as to power the electrical loads, at least one generator (G1, G2) of a propulsion engine of the aircraft, at least one engine-class main power unit (MPS1, MPS2), a plurality of contactors (C1-C18) which are capable of electrically connecting the distribution buses to the propulsion engine generator (G1, G2) and/or the main power unit (MPS1, MPS2); and a management module which is capable of controlling the contactors (C1-C18), a method wherein, during normal operating conditions of the aircraft, the distribution bus is powered by the engine-class main power unit (MPS1, MPS2) and, during the back-up operating mode of the aircraft, the distribution bus is powered by the propulsion engine generator (G1, G2).

Inventors:
Rideau, Jean-Francois
Florentine, Dharma
Application Number:
JP2015551215A
Publication Date:
September 26, 2018
Filing Date:
December 24, 2013
Export Citation:
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Assignee:
Micro Churvo
International Classes:
B64D41/00; H02J3/46
Domestic Patent References:
JP2011504832A
Foreign References:
WO2012025688A1
US20060061213
Attorney, Agent or Firm:
Kawaguchi International Patent Office