Invention Application
- Patent Title: AIRCRAFT FUSELAGE MADE FROM LONGITUDINAL PANELS AND METHOD OF PRODUCING SUCH A FUSELAGE
- Patent Title (中): 远程面板制造的飞机熔接及其制造方法
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Application No.: PCT/FR2007052081Application Date: 2007-10-04
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Publication No.: WO2008043940A3Publication Date: 2008-06-12
- Inventor: GALLANT GUILLAUME , BERNADET PHILIPPE
- Applicant: AIRBUS FRANCE , GALLANT GUILLAUME , BERNADET PHILIPPE
- Assignee: AIRBUS FRANCE,GALLANT GUILLAUME,BERNADET PHILIPPE
- Current Assignee: AIRBUS FRANCE,GALLANT GUILLAUME,BERNADET PHILIPPE
- Priority: FR0654185 2006-10-10
- Main IPC: B64C1/00
- IPC: B64C1/00
Abstract:
The invention relates to an aircraft fuselage comprising a nose cone (2), a tail section (2) and a central section (3), the central section comprising longitudinal panels (31 - 39) assembled directly with one another, at least one of these longitudinal panels having a length corresponding to the distance between the nose cone and the tail section in order to connect said nose cone with said tail section.
Information query
