Title:
胴体セグメント及び接合手段を含む胴体要素
Document Type and Number:
Japanese Patent JP2012531341
Kind Code:
A
Abstract:
A fuselage element including a fuselage segment including a skin and a junction means for connecting the skin to an adjacent fuselage segment. The fuselage segment extends along a longitudinal axis of the fuselage, and the skin includes a first section at at least one end of the fuselage segment. The fuselage segment includes at least one longitudinal stiffening element for the fuselage. A junction member is arranged so as to contact an outer surface of the first section of the skin, and the stiffening element partially extends to the junction member along the longitudinal axis.
Inventors:
Guillaume Garan
Roman de la Ae
Marc Dugerie
Marc-Antoine Castane
Roman de la Ae
Marc Dugerie
Marc-Antoine Castane
Application Number:
JP2012516817A
Publication Date:
December 10, 2012
Filing Date:
July 02, 2010
Export Citation:
Assignee:
Airbus Opera Societe Pa Axion simplifier
International Classes:
B64C1/06
Domestic Patent References:
| JPH05286493A | 1993-11-02 |
Foreign References:
| US20080067289A1 | 2008-03-20 | |||
| US20090020646A1 | 2009-01-22 | |||
| US20050183260A1 | 2005-08-25 | |||
| WO1998058759A1 | 1998-12-30 |
Attorney, Agent or Firm:
Atsushi Aoki
Tetsuro Shimada
Shinji Mitsuhashi
Koichi Ito
Kentaro Ito
Tatsuki Sone
Tetsuro Shimada
Shinji Mitsuhashi
Koichi Ito
Kentaro Ito
Tatsuki Sone