Title:
POWER SUPPLY SYSTEM OF AIRCRAFT
Document Type and Number:
Japanese Patent JP2023125210
Kind Code:
A
Abstract:
To provide a technique for a power supply system of an aircraft, capable of supplying electric power to a power generation device while suppressing an increase in the number of components.SOLUTION: In a power supply system 22 of an aircraft, when supplying electric power from a power generation unit 28 to a drive unit 40, the power supply system 22 supplies the electric power from the power generation unit 28 to the drive unit 40 through a first power transmission path 52, and a voltage is applied to a second power transmission path 54 by a failure detection circuit 26 in a state in which the power generation unit 28 and the drive unit 40 are disconnected from the second power transmission path 54. When the power generation unit 28 is started, electric power in the failure detection circuit 26 is supplied to the power generation unit 28 in a state in which the power generation unit 28 is connected to the second power transmission path 54.SELECTED DRAWING: Figure 7
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Inventors:
MITANI MANABU
YOSHIDA MASATAKA
YOSHIDA MASATAKA
Application Number:
JP2022029189A
Publication Date:
September 07, 2023
Filing Date:
February 28, 2022
Export Citation:
Assignee:
HONDA MOTOR CO LTD
International Classes:
B64D47/00; B64D25/00; H02J1/00
Attorney, Agent or Firm:
Takehiro Chiba
Toshiyuki Miyadera
Takayuki Chima
Yasuharu Nakasone
Shiro Sakai
Tosuke Sekiguchi
Toshiyuki Miyadera
Takayuki Chima
Yasuharu Nakasone
Shiro Sakai
Tosuke Sekiguchi