Title:
航空機用の電気ベースの2次動力システムアーキテクチャ
Document Type and Number:
Japanese Patent JP2006516230
Kind Code:
A
Abstract:
Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet engine. The jet engine can be configured to provide propulsive thrust to the aircraft, and the electric generator can be configured to receive shaft power from the jet engine. The environmental control system can be configured to provide outside air to a passenger cabin of the aircraft in the absence of bleed air from the jet engine.
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Inventors:
Atkey, Warren A.
Alan Thi, Bernier
Bowman, Michael Di
Campbell, Thomas A.
Cruise, Jonathan M
Charles Jay, Fitterman
Charles S. Myth
NJ, Casey, Wai Kay
Nozari, Fahd
Gerinski, edward
Alan Thi, Bernier
Bowman, Michael Di
Campbell, Thomas A.
Cruise, Jonathan M
Charles Jay, Fitterman
Charles S. Myth
NJ, Casey, Wai Kay
Nozari, Fahd
Gerinski, edward
Application Number:
JP2004547053A
Publication Date:
June 29, 2006
Filing Date:
October 22, 2003
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64D41/00; B64D13/06; B64D13/08
Domestic Patent References:
| JPH08507736A | 1996-08-20 |
Foreign References:
| US20020113167A1 | 2002-08-22 |
Attorney, Agent or Firm:
Kuro Fukami
Toshio Morita
Yoshihei Nakamura
Yutaka Horii
Hisato Noda
Masayuki Sakai
Toshio Morita
Yoshihei Nakamura
Yutaka Horii
Hisato Noda
Masayuki Sakai