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1. CA2649339 - FUSELAGE STRUCTURE AND METHOD FOR THE PRODUCTION OF A FUSELAGE STRUCTURE

Office Canada
Application Number 2649339
Application Date 31.05.2007
Publication Number 2649339
Publication Date 13.12.2007
Publication Kind A1
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 DEUTSCHLAND GMBH
Inventors PAHL, GUENTER
Priority Data 10 2006 025 930.0 02.06.2006 DE
60/810,247 02.06.2006 US
Title
(EN) FUSELAGE STRUCTURE AND METHOD FOR THE PRODUCTION OF A FUSELAGE STRUCTURE
(FR) STRUCTURE DE FUSELAGE ET PROCEDE 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.