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Title:
外気を航空機内に供給するための空気路
Document Type and Number:
Japanese Patent JP5358682
Kind Code:
B2
Abstract:
An air duct for supplying ambient air in an aircraft includes an air inlet, a flow duct portion and a feed device that is devised to feed ambient air through the air inlet and the flow duct portion. A flow control flap closes the air inlet in a first position, releases a first flow cross-section of the air inlet in a second position and releases a larger second flow cross-section of the air inlet in a third position. The flow control flap is designed to not increase drag significantly in the second position while still enabling flow through the flow duct portion, while increasing drag to increase air fow through the flow duct portion in the third position.

Inventors:
Castel Dirk
Loelin sebastian
Casas Noriga Wilson Willy
Application Number:
JP2011515189A
Publication Date:
December 04, 2013
Filing Date:
June 23, 2009
Export Citation:
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Assignee:
Airbus Operations GmbH
International Classes:
B64D47/00; B64D13/06
Domestic Patent References:
JP55156800A
Foreign References:
US20020152765
US6349899
GB516099A
FR850267A
WO2005016748A2
US3752422
US20060102779
EP1847458A2
US20110151764
Attorney, Agent or Firm:
Mikio Yoshimiya