Title:
航空機の胴体
Document Type and Number:
Japanese Patent JP2010514616
Kind Code:
A
Abstract:
The fuselage has a central fuselage (4) comprising zones (10, 12, 14) on a side of a front fuselage (2). The width of the zone (10) measured along a tangent axis increases until a maximal width from the front towards rear of an aircraft. The width of the zone (12) decreases from the front towards rear of the aircraft. The width of the zone (14) is constant. The zone (14) is located at the rear of the zone (14). The zone (12) is directly connected to the zone (10). Engines are connected to a rear fuselage (6).
Inventors:
Saint-Jarm, Bruno
The Neboni, Jason
Belleville, Mathieu
The Neboni, Jason
Belleville, Mathieu
Application Number:
JP2009543498A
Publication Date:
May 06, 2010
Filing Date:
December 21, 2007
Export Citation:
Assignee:
Airbus
AIRBUS FRANCE
AIRBUS FRANCE
International Classes:
B64C1/00; B64C23/00
Domestic Patent References:
| JPH03287494A | 1991-12-18 | |||
| JP2008535734A | 2008-09-04 | |||
| JP2004276900A | 2004-10-07 | |||
| JPH03287494A | 1991-12-18 | |||
| JP2008535734A | 2008-09-04 |
Foreign References:
| WO2002057135A1 | 2002-07-25 | |||
| US4674712A | 1987-06-23 | |||
| GB913005A | 1962-12-12 | |||
| US6612522B1 | 2003-09-02 | |||
| US4976396A | 1990-12-11 | |||
| US20030189135A1 | 2003-10-09 | |||
| RU2096267C1 | 1997-11-20 | |||
| US4828204A | 1989-05-09 | |||
| US20030062449A1 | 2003-04-03 | |||
| WO2002057135A1 | 2002-07-25 | |||
| US4674712A | 1987-06-23 | |||
| GB913005A | 1962-12-12 | |||
| US6612522B1 | 2003-09-02 | |||
| US4976396A | 1990-12-11 | |||
| US20030189135A1 | 2003-10-09 |
Other References:
JPN5010000703; ＦＬＩＧＨＴ ＩＮＴＥＲＮＡＴＩＯＮＡＬ Ｖ１６２ Ｎ４８５０, 20020924, ＲＥＥＤ ＢＵＳＩＮＥＳＳ ＩＮＦＯＲＭＡＴＩＯＮ
JPN6013023583; ロシア国特許発明明細書第２０９６２６７号 , 19971120
JPN6013023583; ロシア国特許発明明細書第２０９６２６７号 , 19971120
Attorney, Agent or Firm:
Atsushi Aoki
Jun Tsuruta
Tetsuro Shimada
Shinozaki Masami
Kazuyoshi Ohira
Yasushi Ohashi
Jun Tsuruta
Tetsuro Shimada
Shinozaki Masami
Kazuyoshi Ohira
Yasushi Ohashi