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Patent Searching and Data


Title:
航空機の外皮のための熱伝達装置
Document Type and Number:
Japanese Patent JP2011529418
Kind Code:
A
Abstract:
A heat exchanger for an outer skin of an aircraft comprises at least one feed line for a coolant, at least one discharge line for the coolant and at least one bundle of coolant channels through which coolant flows, wherein in the case of the heat exchanger being attached to the outer skin, the coolant channels are positioned directly on the outer skin of the aircraft, at least in areas, for dissipating heat to the surrounding environment of the aircraft. The heat exchanger may comprise cooling fins around which air flows for increasing the heat dissipation.

Inventors:
Pies car marcus
Application Number:
JP2011520452A
Publication Date:
December 08, 2011
Filing Date:
July 27, 2009
Export Citation:
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Assignee:
Airbus Opera Zion Gesellschaft Mitt Beschlenktel Haftung
International Classes:
B64C1/06; B64D47/00; B64D13/08
Domestic Patent References:
JPH0325096A1991-02-01
JPS6461999A1989-03-08
JPH01256775A1989-10-13
JPH06156392A1994-06-03
JP2003110330A2003-04-11
Foreign References:
US2499736A1950-03-07
US4819720A1989-04-11
US5667168A1997-09-16
US5513500A1996-05-07
Attorney, Agent or Firm:
Masayuki Masabayashi
Hayashi Ichiyoshi