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1. DE102006025930 - Fuselage structure for aircraft or spacecraft has an inner shell system with upper and lower inner shells and a window hinge plate with a window pane device and a grid structure

Office Germany
Application Number 102006025930
Application Date 02.06.2006
Publication Number 102006025930
Publication Date 13.12.2007
Publication Kind B4
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 GMBH
Inventors PAHL GUENTER
Title
(DE) Rumpfstruktur und Verfahren zur Herstellung einer Rumpfstruktur
(EN) Fuselage structure for aircraft or spacecraft has an inner shell system with upper and lower inner shells and a window hinge plate with a window pane device and a grid structure
Abstract
(DE)

Die vorliegende Erfindung schafft ein Verfahren zur Herstellung einer Rumpfstruktur und eine Rumpfstruktur, insbesondere eines Luft- oder Raumfahrzeuges, mit einer Innenschalenanordnung (20), welche eine obere Innenschale (21) und eine untere Innenschale (22) aufweist, wobei die obere Innenschale (21) zumindest abschnittsweise um einen ersten Spalt (23) zum Bilden eines Fensterbereiches von der unteren Innenschale (22) beabstandet ist; und einem Fensterband (41), welches zumindest im Fensterbereich angeordnet ist und eine Scheibeneinrichtung aufweist, welche eine Rumpfkräfte aufnehmende Gitterstruktur (10) umfasst.

(EN)

An upper inner shell in a fuselage inner shell system (20) fits with a clearance in sections from a lower inner shell with a first gap to form a window area. A window hinge plate fits in a window area and has a window pane device, which has a grid structure (10) to retain fuselage forces. An independent claim is also included for a method for a fuselage structure on aircraft or spacecraft.