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Pre-installed adaptable supply network for aeroplanes

A wire and network technology, applied in the field of manufacturing the aircraft structure, can solve the problems of expensive adjustment of cable lines, short circuit and system function loss, etc., and achieve the effect of saving time

Active Publication Date: 2014-08-27
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Changes in the settings of system components require costly adjustments of the associated cabling
Furthermore, precautions must be taken in order to isolate the cables from the aircraft structure so that fraying or even cutting of the cables is prevented, which could lead to short circuits and loss of system functionality

Method used

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  • Pre-installed adaptable supply network for aeroplanes
  • Pre-installed adaptable supply network for aeroplanes
  • Pre-installed adaptable supply network for aeroplanes

Examples

Experimental program
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Embodiment Construction

[0019] figure 1 An aircraft is shown in which some main structural elements are shown. The structural element extending in the longitudinal direction of the aircraft and designated with reference numeral 10 is called a longitudinal bulkhead. The curved structural element transverse to the longitudinal frame and extending substantially in such a way as to define the shape of the fuselage cross-section is the transverse frame 12 and extends transversely to the longitudinal direction of the aircraft and in the horizontal direction (relative to the aircraft on the ground) The structural elements are referred to as transverse frames, on which, for example, a cabin floor or a cargo floor can be fitted.

[0020] figure 2 A wire configuration according to an embodiment of the invention is schematically shown. In aircraft construction, several longitudinal bulkhead frames 10 generally extend parallel to one another in the longitudinal direction of the aircraft. The first wire grou...

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PUM

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Abstract

The invention relates to an aircraft structure comprising: a structural element (10, 12, 13); a first conductor set (11) fixedly connected to the structural element (10); a second conductor set (14, 15), It is fixedly connected to the structural elements (12, 13) and its longitudinal direction crosses the longitudinal direction of the first conductor group (11), so that the longitudinal direction of the conductors forms a network spanning the aircraft structure at least in sections; the connecting elements (21, 22, 23), so that in the installed state of the structural element (10, 12, 13) in the aircraft structure, the selected first wire group (11) and the selected second wire group (14, 15) Connecting at selected intersection points of the network in order thus to constitute conductors for the transmission of current and / or data. Furthermore, the invention relates to a method for producing such an aircraft structure.

Description

technical field [0001] The invention relates to an aircraft structure with a conductor network, and to a method for producing said aircraft structure. Background technique [0002] Previous cable runs in aircraft for connecting aircraft system components required high planning and manufacturing outlay. The cable routing must be determined during the design of the aircraft, in which space requirements in particular play an important role. A change in the configuration of the system components requires costly adjustments of the cabling that is associated therewith. Furthermore, precautions must be taken in order to isolate the cables from the aircraft structure, so that fraying or even cutting of the cables is prevented, which could lead to short circuits and loss of system functionality. Contents of the invention [0003] It is an object of the invention to at least partially solve the problems associated with cabling of aircraft. [0004] This object is achieved by mean...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02G3/00B64D47/00H02G3/30H02G3/36
CPCH02G3/30H02G3/00H02G3/36H02G3/105B64D47/00H02G3/24Y10T29/49826
Inventor 尼古拉斯·布朗约翰斯特凡·奥斯特纳克
Owner AIRBUS OPERATIONS GMBH