Device for fastening elongate elements to a structure

A technology for structural parts and fixed supports, applied to electrical components, pipes/pipe joints/pipes, pipe supports, etc., can solve problems such as damage, difficulty in fixing, rough contact surface, etc., and achieve the effect of simplifying inventory management

Inactive Publication Date: 2006-07-26
EUROCOPTER
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, this type of collar presents particular disadvantages
For example, it should be observed that the extension comes at least partly in contact with the hook-shaped fixing means, thereby roughening the contact surface of the collar engaging said extension, which can cause damage, especially when When coaxial cables with particularly thin and fragile center conductors are in the bundle
Furthermore, it is difficult to secure the collar to a structural member without the use of proper tools

Method used

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  • Device for fastening elongate elements to a structure
  • Device for fastening elongate elements to a structure
  • Device for fastening elongate elements to a structure

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0059] figure 1 The shown device 1 for securing extensions is a first embodiment of the invention and it comprises a flexible self-clamping strip 3 with an annular closure system on a first face 30 and on a first face 40 A flexible self-clamping strip 4 with a hook closure system, each of these first and second flexible strips has a second face 35 or 45, respectively, which is self-adhesive, and which Both flex strips are of equal width. For example, each of them can be Velcro TM Profiles, either with a hook closure system ("male" system) or a loop closure system ("female" system).

[0060] The first and second flexible strips 3 and 4 are at least partially bonded to each other by their self-adhesive second faces 35 and 45, so that by attaching the first and second flexible strips 3 and 4 The opposing first and second free end regions 51 and 52 are joined together to form the first flexible band 5 .

[0061] The length of the flexible strip 5 is longer than the outer circu...

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PUM

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Abstract

The present invention provides a device ( 1 ) for fastening elongate elements ( 2 ) such as cables or bundles of cables or the like to a structure (S), includes at least a first flexible self-gripping strip ( 3 ) having a loop-closure system on a first face ( 30 ) and a second flexible self-gripping strip ( 4 ) with a hook-closure system on a first face ( 40 ). The first and second flexible strips ( 3 and 4 ) adhere at least in part one against the other via their second faces ( 35 and 45 ) that are self-adhesive, so as to form a flexible collar (C) by uniting at least their facing free end zones ( 51 and 52 ). The device further includes a rigid plate ( 10 ) for constituting a support for fastening the device ( 1 ) to the structure (S).

Description

technical field [0001] The present invention relates to a device for securing an extension, such as a cable or bundles of cables, optical or other cables, fluid conduits or pipes or the like, which enables said extension to be secured relative to a supporting structure. Support and guide. [0002] More generally, the present invention relates in particular to the manufacture of vehicles in the automotive industry, shipbuilding, and more particularly in the aviation industry. An aircraft includes a number of devices and devices of various types for control purposes, which very much require many circuits of various types (electrical, optical, fluid conversion...) essential information. Therefore, it is important to ensure the safety of these multiple circuits and to orient them correctly with respect to the structure of the aircraft. Background technique [0003] Naturally, the device is not limited to this particular application. It can therefore be used whenever the exte...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16L3/227H02G3/30
CPCF16L3/1025F16L3/137H02G3/32
Inventor G·吉罗
Owner EUROCOPTER
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