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1. WO2007138082 - LINE SYSTEM ARRANGEMENT IN AN AIRCRAFT OR SPACECRAFT HAVING A FUSELAGE

Publication Number WO/2007/138082
Publication Date 06.12.2007
International Application No. PCT/EP2007/055267
International Filing Date 30.05.2007
IPC
B64C 1/00 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like
B64C 1/12 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like
06Frames; Stringers; Longerons
12Construction or attachment of skin panels
H02G 3/00 2006.01
HELECTRICITY
02GENERATION, CONVERSION, OR DISTRIBUTION OF ELECTRIC POWER
GINSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
3Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
CPC
B64C 1/066
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
066Interior liners
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 1/1446
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
1407Doors; surrounding frames
1446Inspection hatches
B64D 11/00
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
11Passenger or crew accommodation; Flight-deck installations not otherwise provided for
B64G 1/22
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
1Cosmonautic vehicles
22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
Applicants
  • AIRBUS DEUTSCHLAND GMBH [DE]/[DE] (AllExceptUS)
  • LAUE, Hans-Georg [DE]/[DE] (UsOnly)
Inventors
  • LAUE, Hans-Georg
Agents
  • PECKMANN, Ralf
Priority Data
10 2006 025 388.431.05.2006DE
60/809,56231.05.2006US
Publication Language English (EN)
Filing Language English (EN)
Designated States
Title
(EN) LINE SYSTEM ARRANGEMENT IN AN AIRCRAFT OR SPACECRAFT HAVING A FUSELAGE
(FR) AGENCEMENT D'UN SYSTÈME DE LIGNE DANS UN AÉRONEF OU UN ENGIN SPATIAL POSSÉDANT UN FUSELAGE
Abstract
(EN)
The present invention provides a line system arrangement (1) in an aircraft or spacecraft having a fuselage (3), with at least one receiving region (4, 41 ) for receiving at least one component of a line system (2), wherein the at least one receiving region (4, 4' ) is accessible, at least in some sections, from outside the fuselage (3) of the aircraft and spacecraft for installation and/or maintenance of the line system (2); and an aircraft or spacecraft with a corresponding arrangement (1).
(FR)
L'invention concerne un agencement d'un système de ligne (1) dans un aéronef ou un engin spatial possédant un fuselage (3), avec au moins une zone de réception (4, 41) afin de recevoir au moins un composant d'un système de ligne (2), cette zone de réception (4, 4') étant accessible, au moins au niveau de certaines sections, de l'extérieur du fuselage (3) de l'aéronef ou de l'engin spatial en vue de l'installation et/ou de l'entretien du système de ligne (2); et un aéronef ou un engin spatial présentant un agencement correspondant (1).
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