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1. WO2007141176 - FUSELAGE STRUCTURE AND METHOD FOR THE PRODUCTION OF A FUSELAGE STRUCTURE

Publication Number WO/2007/141176
Publication Date 13.12.2007
International Application No. PCT/EP2007/055286
International Filing Date 31.05.2007
IPC
B64C 1/14 2006.01
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 DEUTSCHLAND GMBH [DE]/[DE] (AllExceptUS)
  • PAHL, Guenter [DE]/[DE] (UsOnly)
Inventors
  • PAHL, Guenter
Agents
  • PECKMANN, Ralf
Priority Data
10 2006 025 930.002.06.2006DE
60/810,24702.06.2006US
Publication Language English (EN)
Filing Language English (EN)
Designated States
Title
(EN) FUSELAGE STRUCTURE AND METHOD FOR THE PRODUCTION OF A FUSELAGE STRUCTURE
(FR) STRUCTURE DE FUSELAGE ET PROCÉDÉ DE FABRICATION D'UNE 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.
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