Title:
航空機胴体の外板構造
Document Type and Number:
Japanese Patent JP4976421
Kind Code:
B2
Abstract:
A structuring construction for an aircraft fuselage is provided having an outer skin as well as a plurality of formers extending at a spacing side by side crosswise to the longitudinal direction of the fuselage wherein at least a partial number of the formers include a main former portion which is channel-like in cross section and the channel edges of which are adjacent to the outer skin and wherein the channel space of the main former portion serves to accommodate at least one supply air line which may be formed, for example, by a separate pipe line.
Inventors:
Hendrick Fairveyen
Application Number:
JP2008550661A
Publication Date:
July 18, 2012
Filing Date:
January 05, 2007
Export Citation:
Assignee:
Airbus Operations GmbH
International Classes:
B64C1/06; B64C1/14; B64D13/06
Domestic Patent References:
| JP2004217208A | ||||
| JP5062102U | ||||
| JP239920A | ||||
| JP200419598A | ||||
| JP812286A |
Foreign References:
| WO2005110843A1 | ||||
| US5171510 | ||||
| US1966933 | ||||
| GB127943B | ||||
| US4726426 |
Attorney, Agent or Firm:
Kenji Sugimura
Shiro Fujitani
Tatsuya Sawada
Shiro Fujitani
Tatsuya Sawada