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1. EP2024228 - FUSELAGE STRUCTURE

Office European Patent Office
Application Number 07729698
Application Date 31.05.2007
Publication Number 2024228
Publication Date 18.02.2009
Publication Kind B1
IPC
B64C 1/14
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like
14Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens
CPC
B64C 1/068
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
06Frames; Stringers; Longerons ; ; Fuselage sections
068Fuselage sections
B64C 1/12
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
06Frames; Stringers; Longerons ; ; Fuselage sections
12Construction or attachment of skin panels
B64C 1/1492
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
14Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens ; accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
1476Canopies; Windscreens or similar transparent elements
1492Structure and mounting of the transparent elements in the window or windscreen
Applicants AIRBUS OPERATIONS GMBH
Inventors PAHL GUENTER
Designated States
Priority Data 102006025930 02.06.2006 DE
81024706 02.06.2006 US
Title
(DE) RUMPFSTRUKTUR
(EN) FUSELAGE STRUCTURE
(FR) STRUCTURE DE FUSELAGE
Abstract
(EN)
The present invention provides a method for the production of a fuselage structure, and a fuselage structure, in particular of an aircraft or spacecraft, with an inner shell arrangement (20) which has an upper inner shell (21) and a lower inner shell (22), the upper inner shell (21) being spaced apart at least in some sections from the lower inner shell (22) by a first gap (23) in order to form a window region; and a window band (41) which is arranged at least in the window region and has a pane device which comprises a grid structure (10) which absorbs fuselage forces.

(FR)
La présente invention concerne un procédé de fabrication d'une structure de fuselage et une structure de fuselage, en particulier d'un aéronef ou d'un astronef, comportant un ensemble coque interne (20) composé d'une coque interne supérieure (21) et d'une coque interne inférieure (22), la coque interne supérieure (21) étant espacée, au moins dans certaines sections, de la coque interne inférieure (22) par un premier espace (23) de façon à former une région de hublot; et une bande de hublot (41) qui est située au moins dans la région de hublot et comporte un dispositif vitre qui comprend une structure en grille (10) absorbant les forces de fuselage.