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1. CN101460358 - Fuselage structure and method for the production of a fuselage structure

Office China
Application Number 200780020434.6
Application Date 31.05.2007
Publication Number 101460358
Publication Date 17.06.2009
Grant Number 101460358
Grant Date 06.06.2012
Publication Kind B
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
空中客车德国运营有限责任公司
Inventors Pahl Guenter
京特·帕尔
Agents wang xinhua
中科专利商标代理有限责任公司 11021
Priority Data 102006025930.0 02.06.2006 DE
60/810,247 02.06.2006 US
Title
(EN) Fuselage structure and method for the production of a fuselage structure
(ZH) 机身结构和具有该机身结构的飞机或航天器
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.

(ZH)

本发明提供了机身结构的制造方法,和机身结构,尤其是飞机或航天器的机身结构,具有内壳体装置(20),其具有上部内壳体(21)和下部内壳体(22),上部内壳体(21)至少在一些部分中从下部内壳体(22)间隔开第一间隙(23),以形成窗户区域;和窗户带(41),其至少布置在窗户区域中,并具有包括吸收机身力的栅格结构(10)的窗格板设备。