Title:
航空機の内部空間内で互いに取り付けられた、エンジンを支持するための二つの準構造体を備えた航空機の後方部分
Document Type and Number:
Japanese Patent JP2012502845
Kind Code:
A
Abstract:
A rear part of an aircraft, including a support structure for supporting engines, extending through the fuselage, through two openings distributed on either side of a vertical median plane of the aircraft. The support structure includes a first half-structure and a second half-structure respectively extending through the first and second fuselage openings, the first and second half-structures being joined to each other so that they can be disassembled in an inside space defined by the fuselage.
Inventors:
Laurent Lafon
Application Number:
JP2011527376A
Publication Date:
February 02, 2012
Filing Date:
September 16, 2009
Export Citation:
Assignee:
Airbus Operations
International Classes:
B64C1/16; B64D27/14
Domestic Patent References:
| JPS6490897A | 1989-04-07 | |||
| JPH03169799A | 1991-07-23 |
Foreign References:
| FR966757A | 1950-10-18 | |||
| DE961151C | 1957-04-04 | |||
| WO1998025821A1 | 1998-06-18 |
Attorney, Agent or Firm:
Yasuhiko Murayama
Masatake Shiga
Takashi Watanabe
Shinya Mitsuhiro
Masatake Shiga
Takashi Watanabe
Shinya Mitsuhiro