Title:
ELECTRIC POWER SYSTEM FOR AIRCRAFT
Document Type and Number:
Japanese Patent JP2015047935
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide an electric power system for an aircraft, which can supply high power to a load while suppressing upsizing of an electric motor and the like.SOLUTION: An electric power system 1 for an aircraft includes a high-voltage bus 14 for FCS, which is used to supply electric power to an electric actuator 41. The high-voltage bus 14 for FCS is configured to be capable of being constantly connected to a main generator 21 and a flywheel battery 27, which serve as two or more different types of power supply devices.
Inventors:
NAKAGAWA SHINGO
YAMAMOTO YOICHI
OYORI HITOSHI
YAMAMOTO YOICHI
OYORI HITOSHI
Application Number:
JP2013180120A
Publication Date:
March 16, 2015
Filing Date:
August 30, 2013
Export Citation:
Assignee:
NABTESCO CORP
IHI AEROSPACE CO LTD
IHI AEROSPACE CO LTD
International Classes:
B64D41/00; B64C13/50
Domestic Patent References:
| JP2012525815A | 2012-10-22 |
Foreign References:
| US20090302153A1 | 2009-12-10 | |||
| US20070174177A1 | 2007-07-26 | |||
| US20120232728A1 | 2012-09-13 | |||
| US20080174177A1 | 2008-07-24 |
Attorney, Agent or Firm:
Patent business corporation Wang Dee IP partners
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