Title:
個別に温度制御することができる複数の気候ゾーンを有する航空機のための空調装置
Document Type and Number:
Japanese Patent JP4897833
Kind Code:
B2
Abstract:
An air conditioning arrangement for an aircraft with a plurality of climate zones that may be individually temperature-controlled includes a main branching system having an air supply feed path system with a mixing chamber and a plurality of sub-branching systems branching from the mixing chamber and leading to one of the climate zones in each case. Basic temperature control means are used for controlling the temperature of the air supply in the mixing chamber. Individual temperature-control means are used on the other hand for individually controlling the temperature of the air supply in each of the sub-branching systems as a function of a desired temperature value of the respective climate zone. Basic temperature control of the air supply in the mixing chamber preferably takes place independently of a temperature requirement of the climate zone with associated combined heat and power engine.
Inventors:
Nico St. Fante
Application Number:
JP2008552707A
Publication Date:
March 14, 2012
Filing Date:
January 11, 2007
Export Citation:
Assignee:
Airbus Operations GmbH
International Classes:
B64D13/08
Domestic Patent References:
| JP2001163042A | 2001-06-19 | |||
| JPS6475865A | 1989-03-22 | |||
| JPS444195B1 |
Foreign References:
| WO1994020363A1 | 1994-09-15 |
Attorney, Agent or Firm:
Kenji Sugimura
Shiro Fujitani
Tatsuya Sawada
Shiro Fujitani
Tatsuya Sawada