Title:
航空機外部の空気機構を用いて航空機内域を冷却するためのシステム及び方法
Document Type and Number:
Japanese Patent JP2012518567
Kind Code:
A
Abstract:
A system for cooling an aircraft zone includes a mixing chamber which is connected to an air-conditioning assembly for making cool air available and/or to a recirculated-air conveying device for supplying recirculated air into the mixing chamber. The system further includes an aircraft-side air-distribution system which includes at least one line connecting the mixing chamber to the aircraft zone to be cooled and also at least one line that is connectable to an aircraft-external air-generating assembly in order to route air made available by the aircraft-external air-generating assembly into the aircraft-side air-distribution system.
Inventors:
Krakowski Darius
Gum-stephan
Cologne Hofer Yoga
Gum-stephan
Cologne Hofer Yoga
Application Number:
JP2011550478A
Publication Date:
August 16, 2012
Filing Date:
February 18, 2010
Export Citation:
Assignee:
Airbus Operations GmbH
International Classes:
B64D13/06; B64F3/00
Attorney, Agent or Firm:
Mikio Yoshimiya