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Title:
ラムエアに基づく航空機用冷却及び換気システム
Document Type and Number:
Japanese Patent JP2010513119
Kind Code:
A
Abstract:
A cooling system for an aircraft includes an air inlet through which air from the environment of the aircraft enters a ram air channel, and an air outlet through which air emerges from the ram air channel. A heat exchanger is arranged in the ram air channel. A ventilation device is in fluid communication with the ram air channel. Also connected to the ram air channel is a distribution line to cool at least one heat-loaded component of the aircraft, in particular a cabin air conditioning system, and/or to ventilate an installation space of the at least one heat-loaded component.

Inventors:
Thomas Scheler
Rudiger Schmidt
Alexander Soruntsev
Application Number:
JP2009541849A
Publication Date:
April 30, 2010
Filing Date:
December 12, 2007
Export Citation:
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Assignee:
Airbus Operations Game Beher
International Classes:
B64D13/08
Domestic Patent References:
JP2006232269A2006-09-07
JP2008509842A2008-04-03
Attorney, Agent or Firm:
Yasuhiko Murayama
Masatake Shiga
Takashi Watanabe
Shinya Mitsuhiro