EP 2076430 A2 20090708 - AIRCRAFT FUSELAGE MADE FROM LONGITUDINAL PANELS AND METHOD OF PRODUCING SUCH A FUSELAGE
Title (en)
AIRCRAFT FUSELAGE MADE FROM LONGITUDINAL PANELS AND METHOD OF PRODUCING SUCH A FUSELAGE
Title (de)
FLUGZEUGRUMPF AUS LÄNGSPLATTEN UND VERFAHREN ZUR HERSTELLUNG EINES DERARTIGEN RUMPFES
Title (fr)
FUSELAGE D'AÉRONEF RÉALISÉ A PARTIR DE PANNEAUX LONGITUDINAUX ET PROCÉDÉ DE RÉALISATION D'UN TEL FUSELAGE
Publication
Application
Priority
- FR 2007052081 W 20071004
- FR 0654185 A 20061010
Abstract (en)
[origin: WO2008043940A2] 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.
IPC 8 full level
B64C 1/00 (2006.01)
CPC (source: EP US)
B64C 1/068 (2013.01 - EP US); B64C 1/0683 (2020.01 - EP US); B64C 1/0685 (2020.01 - EP US); B64C 2211/00 (2013.01 - EP)
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
FR 2906785 A1 20080411; FR 2906785 B1 20091204; BR PI0717735 A2 20131022; CA 2663415 A1 20080417; CN 101516723 A 20090826; CN 101516723 B 20130605; EP 2076430 A2 20090708; JP 2010505700 A 20100225; RU 2009117613 A 20101120; RU 2489312 C2 20130810; US 2010032523 A1 20100211; WO 2008043940 A2 20080417; WO 2008043940 A3 20080612
DOCDB simple family (application)
FR 0654185 A 20061010; BR PI0717735 A 20071004; CA 2663415 A 20071004; CN 200780034706 A 20071004; EP 07858512 A 20071004; FR 2007052081 W 20071004; JP 2009531882 A 20071004; RU 2009117613 A 20071004; US 44497207 A 20071004