Title:
航空機または宇宙船の胴体、およびそのような胴体を有する航空機または宇宙船、並びにそのような胴体を能動的に断熱する方法
Document Type and Number:
Japanese Patent JP2010519119
Kind Code:
A
Abstract:
The present invention relates to a fuselage of an aircraft or spacecraft, with at least one shell element and a structural element. An interspace to which air can be admitted by an air stream is provided between the at least one shell element and the structural element. The fuselage is distinguished by the fact that, to form the air-admitting air stream as an outgoing/incoming air stream of a pressurized interior space of the fuselage, the interspace is connected to a corresponding outgoing/incoming air connection of the interior space. The invention also relates to a corresponding aircraft or spacecraft and to a method of actively insulating such a fuselage.
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Inventors:
Ioan Paul
Application Number:
JP2009550711A
Publication Date:
June 03, 2010
Filing Date:
February 21, 2008
Export Citation:
Assignee:
Airbus Operations Game Beher
International Classes:
B64C1/40; B64D13/06
Domestic Patent References:
| JP2007530367A | 2007-11-01 | |||
| JP2003191897A | 2003-07-09 |
Foreign References:
| WO2008101986A1 | 2008-08-28 | |||
| DE10154063A1 | 2003-05-15 | |||
| US6491254B1 | 2002-12-10 | |||
| US4291851A | 1981-09-29 | |||
| WO2005095206A1 | 2005-10-13 |
Attorney, Agent or Firm:
Masahiko Nishito