Title:
航空機の電動タキシングシステム
Document Type and Number:
Japanese Patent JP6626328
Kind Code:
B2
Abstract:
An electric taxiing system of an aircraft (1) includes: a wheel (5a, 7a) of an aircraft (1); a taxiing motor (5b, 7b) which is rotated together with the wheel (5a, 7a) in landing of the aircraft (1) to apply breaking force to the wheel (5a, 7a) and to generate regenerative power according to the breaking force, and which rotates the wheel (5a, 7a) in taxiing of the aircraft (1); and a power supply control unit (27) which supplies the regenerative power to an electric element of the aircraft (1), the electric element (9b, 11b, 13b, 15b, 29a, 31a) being driven in order for the aircraft (1) to perform landing or re-takeoff after cancelling landing.
Inventors:
Noriko Morioka
Kakiuchi Daiki
Oi Jin
Hiroyuki Asakura
Kakiuchi Daiki
Oi Jin
Hiroyuki Asakura
Application Number:
JP2015235530A
Publication Date:
December 25, 2019
Filing Date:
December 02, 2015
Export Citation:
Assignee:
Ihi Co., Ltd.
Sumitomo Precision Products Co., Ltd.
IHI Aerospace Co., Ltd.
Sumitomo Precision Products Co., Ltd.
IHI Aerospace Co., Ltd.
International Classes:
B64C25/36; B60T1/16; B64C25/42; B64D27/24; B64D41/00; H02P3/18
Domestic Patent References:
| JP2009023628A | ||||
| JP2001095272A |
Foreign References:
| US20090076668 | ||||
| US20100252691 | ||||
| US20080258014 | ||||
| DE102013209538A1 | ||||
| US20160325826 |
Attorney, Agent or Firm:
Hidekazu Miyoshi
Iwa Saki Kokuni
Shunichi Takahashi
Masakazu Ito
Toshio Takamatsu
Iwa Saki Kokuni
Shunichi Takahashi
Masakazu Ito
Toshio Takamatsu