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Construction group for aircraft for feeding line to cabin module

An aircraft and cabin technology, applied in the field of aircraft structure group, can solve the problems of high cost and high adaptation workload, etc.

Pending Publication Date: 2018-06-05
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] Those structural groups known from the prior art for feeding lines to the cabin modules involve a high adaptation effort for different cabin layouts in the flexible area of ​​the cabin and thus lead to correspondingly high costs

Method used

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  • Construction group for aircraft for feeding line to cabin module
  • Construction group for aircraft for feeding line to cabin module
  • Construction group for aircraft for feeding line to cabin module

Examples

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Embodiment Construction

[0031] figure 1 and figure 2 A structural group 1 for feeding a line 2 of an aircraft to a connector section 4 of a cabin module 3 according to an embodiment of the invention is shown. According to this embodiment, the aircraft is preferably a civil aircraft, and the embodiment is not limited thereto.

[0032] The structural group 1 comprises guide elements 5 which are arranged such that, during reception of the structural group 1 in the aircraft, the lines 2 lead to the fuselage of the aircraft. Preferably, the guide element 5 guides the line 2 along the top part of the fuselage. In particular, the structural group 1 is configured to arrange the guide element 5 in the roof of the cabin of the aircraft. Preferably, the guide element is mechanically connected to the primary and / or secondary structure of the aircraft. In this embodiment, the guide element 5 may preferably be an elongated support extending through the entire cabin along the cabin ceiling. A plurality of ele...

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PUM

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Abstract

A construction group of an aircraft for feeding a line to a connector section of a cabin module, especially used for a cabin of a civil aircraft, includes a flexible zone for providing at least one cabin module having a connector section for physical connection to a line of the aircraft. The flexible zone is configured to receive different cabin modules and / or a cabin module at different positions. The construction group further includes a guide element for guiding the line to be connected to the connector section along the fuselage of the aircraft, and a support element extending along the flexible zone for feeding the line from the guide element to the connector section, wherein during the receiving of the construction group in the aircraft, the longitudinal axis of the support element includes a component in direction of the attitudinal axis of the aircraft. In addition, the invention relates to an aircraft comprising the construction group and a method fo connecting the connector section of the cabin module to the line of the aircraft.

Description

technical field [0001] The invention relates to a structural group for an aircraft. In particular, the invention relates to a structural set of cabins of a civil aircraft. This structural group is suitable for feeding lines to the connector sections of the cabin modules. A cabin module can be a galley, a cabinet and / or another cabin module. The structure includes a flexible area for arranging at least one cabin module, wherein the cabin module includes connector sections for physical connection to wiring of the aircraft. The flexible area is adapted to receive different cabin modules and / or to receive cabin modules in different positions. Furthermore, the structural group comprises guide elements for guiding the lines to be connected to the connector sections of the cabin modules along the fuselage of the aircraft and support elements for feeding the lines from the guide elements to the connector sections. Background technique [0002] Civilian aircraft cabins today incl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D11/00B64D11/02B64D11/04
CPCB64D11/00B64D11/02B64D11/04H02G3/263B64D2011/0046F16L3/221H02G3/22
Inventor 塞巴斯蒂安·舍夫勒安贾·韦塞尔斯马尔特·菲尔斯滕贝格本杰明·克洛茨奥拉夫·格莱斯克尔佐尔坦·楚道尔伊内斯·迪特曼贝恩德·卡茨迈尔
Owner AIRBUS OPERATIONS GMBH
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