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Title:
ELECTRICAL ARCHITECTURE FOR AIRCRAFT, AIRCRAFT COMPRISING THE ARCHITECTURE, AND METHOD FOR OPERATING THE ARCHITECTURE
Document Type and Number:
Japanese Patent JP2020001691
Kind Code:
A
Abstract:
To provide electric architecture for an aircraft, an aircraft comprising the architecture, and a method for operating the architecture.SOLUTION: The present invention relates to architecture for an aircraft, an aircraft comprising the architecture, and a method for operating the architecture. According to the invention, the architecture comprises: two air-conditioning systems (12, 14); two converters (62L, 62R), each of the two converters (62L, 62R) being intended to supply one of the air-conditioning systems (12, 14); and at least one first electric machine (24L) for starting up a first main engine (42L) of the aircraft. The electrical architecture (60) is configured such that the two converters (62L, 62R) can together supply the first electric machine (24L).SELECTED DRAWING: Figure 5

Inventors:
FREDERIC LACAUX
STEPHANE GUGUEN
AMIRA MAALOUF
Application Number:
JP2019115212A
Publication Date:
January 09, 2020
Filing Date:
June 21, 2019
Export Citation:
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Assignee:
THALES SA
International Classes:
B64D41/00; B64D27/24; H02P5/74; H02P25/16; H02P27/06
Attorney, Agent or Firm:
Kawaguchi International Patent Office



 
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