Mounting Device For Aircraft Supply Systems

一种安装装置、供给系统的技术,应用在飞机零件、运输和包装、电路或流体管路等方向,能够解决装置不能特别容易地使用、电线隔离距离未被保持、无法装备间距保持恒定等问题,达到安装操作且经济、精确性不必过高、简化安装的效果

Active Publication Date: 2014-07-16
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0016] Said device has the disadvantage that the fastener support is only weakly fastened to the rail
[0018] It is therefore possible that the spacing between the equipment (supply systems) cannot be kept constant, and this proves to be particularly harmful when said equipment comprises wires: the known separation distance of the wires is not maintained
[0019] It is to be noted here that the isolation distance corresponds, for example, to the distance at which two wires should be separated in order to limit the effects due to electromagnetic interference
[0020] Finally, the device present in said document is not particularly easy to use, since, in order to fasten the fastener support to the rail, it is necessary to lock the elastic grip of the fastener support in the rail by means of a snap ring. position, where part of the snap ring is wedged in the opening made in the wall of the fastener support, this operation is very complicated for the operator

Method used

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  • Mounting Device For Aircraft Supply Systems
  • Mounting Device For Aircraft Supply Systems
  • Mounting Device For Aircraft Supply Systems

Examples

Experimental program
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Embodiment Construction

[0082] figure 1 A mounting device 1 for an aircraft supply system 2 according to a first embodiment of the invention is shown, said device being fastened to both faces 5 of a support bracket 6 of the structure of the aircraft.

[0083] Since these support brackets 6 are known in the prior art and are not an integral part of the present invention, the structure of the support brackets 6 will not be described here.

[0084] The installation device 1 consists of a cross member (ramp) 10 , a first end piece 20 , a second end piece 30 , and a support module 40 .

[0085] Also shown is an intermediate device 50 fixed to the module 40 for holding the supply system. In this case, the intermediate device 50 is a prior art collar. Therefore, these intermediate devices 50 will not be described herein.

[0086] Such as figure 2 visible in the figure 2 Only the cross member 10 is shown, which is a part extending in the longitudinal direction and having a rectangular cross section, t...

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PUM

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Abstract

A mounting device for aircraft supply systems comprises a cross member (10) and at least one support module (40) including a body having a shape complementary to that of a cross member. The body includes an opening and a device for securing an aircraft supply system (2). Furthermore the at least one support module (40) comprises a pin, wherein the opening forms a guide that is able to receive a portion of the pin. The cross member (10) includes grooves (101) that are regularly spaced apart in the direction of elongation of said cross member (10). The pin has a shape complementary to that of the grooves and has a lip transverse to the direction of elongation of the pin. The support module is anchored to the cross member by the pin being inserted into the opening, the pin engaging with one of the grooves, as far as an anchoring position in which the lip is in contact with the support module (40).

Description

technical field [0001] The invention relates to a mounting device for an aircraft supply system. Background technique [0002] In order to supply the various systems present in the aircraft, it is necessary to install the associated (electrical, hydraulic, pneumatic, etc.) supply systems. These supply systems are in the form of wiring, piping, and other pathways. These supply systems are arranged on the fuselage structure, in particular between frames holding the fuselage structure in the plane of the fuselage structure section. These frames are connected to reinforcements provided by spars along the longitudinal axis of the aircraft. Since the space available for installing the supply system is mainly provided in the region of the girders and panels forming the skin of the aircraft, the volume for installing the system in the pressure compartment is critical. [0003] Thus pipes, wires, wire assemblies, electrical wiring or stranded wires are mounted on the frame above t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16L3/00F16L3/16B64D47/00
CPCB64D47/00F16L3/00H02G3/32B64C1/00B60R16/0215
Inventor 劳伦特·雷沃略索米歇尔·达尔-辛
Owner AIRBUS OPERATIONS GMBH
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