Title:
航空機キャビンの温度制御装置および方法
Document Type and Number:
Japanese Patent JP4630287
Kind Code:
B2
Abstract:
A device for temperature control in an aircraft cabin includes a first supply control arrangement and a first pressure control arrangement. The first supply control arrangement includes an air duct and a valve arrangement that controls a supply of heated air delivered to a first temperature area of the aircraft cabin such that a first specified temperature for the first temperature zone is achieved. When the valve arrangement fails, the first pressure control arrangement operates to control a pressure of heated air supplied into the first temperature area such that the first specified temperature for the first temperature zone is achieved.
Inventors:
Nico St. Fante
Marx petrack
Thomas Scheller
Uwe Buchholz
Marx petrack
Thomas Scheller
Uwe Buchholz
Application Number:
JP2006546122A
Publication Date:
February 09, 2011
Filing Date:
December 30, 2004
Export Citation:
Assignee:
Airbus Opera Zion Gesellschaft Mitt Beschlenktel Haftung
International Classes:
B64D13/08
Domestic Patent References:
| JP2602654B2 |
Foreign References:
| US2959028 | ||||
| EP0555500A1 | ||||
| GB1604541A | ||||
| GB1385182A | ||||
| FR2485473A1 |
Attorney, Agent or Firm:
Kenji Sugimura
Kosaku Sugimura
Shiro Fujitani
Kiyoshi Kuruma
Tatsuya Sawada
Kosaku Sugimura
Shiro Fujitani
Kiyoshi Kuruma
Tatsuya Sawada