The invention relates to holders and, in particular, to cable holder for holding and guiding bundles of electric cables in aircraft.
Known cable holder used in aircraft are usually difficult to mount, wherein an exchange of such a cable holder during the course of maintenance procedures can only be carried out with a special tool and consequently is quite time-consuming.
According to an exemplary embodiment of the invention, a holder is provided which comprises a base body and a clamp, wherein one end of the clamp is supported on the base body in a pivot point, and wherein the clamp can be brought into a fastening position, in which its other end snaps into the base body, by turning the clamp relative to the base body. The clamp may be inserted into the base body at the pivot point at an angle of 90° and may be closed by turning. In this case, the clamp may be automatically secured, namely geometrically in the pivot point on the bottom and in the interlocking region on the top.
At least one projection may be provided on the end of the clamp that snaps into the base body, wherein this projection snaps into an opening arranged in the base body when the clamp is turned into the fastening position. In the opening, a pin extends in the direction of the snapped-in projection such that the tab is prevented from unintentionally sliding out.
For opening, the pin may be realized in a flexible fashion and may need to be pressed aside, for example, by means of a screwdriver. The pin may then return into its original position.
In its upper region, the holder according to an exemplary embodiment of the invention makes it possible to realize a rapid-action interlock that has a high reliability of operation and can be easily installed and serviced. The holder may be made of plastic and manufactured by means of injection-moulding. This means that the holder represents an inexpensive mass-produced part, so that that the installation times/costs are reduced. During maintenance procedures, the cables that may be clamped or penned in, according to the invention, between the base body and the clamp can be very quickly exchanged “in situ” without requiring special tools. The warehousing/variety of parts can be reduced because the clamp is suitable for use on the left as well as on the right side of an aircraft.
The holder according to the invention may make it possible to hold and guide, in particular moving, electric cables and to simultaneously protect these cables from mechanical damages on structural components.
According to an exemplary embodiment of the invention, a holder is developed for holding and guiding cables (bundles of cables) that can be inexpensively manufactured, has a high reliability of operation and can be easily installed and serviced.
One exemplary embodiment of the invention is described below with reference to the enclosed figures. Identical elements are identified by the same reference symbols.
The figures show:
According to the invention, the base body 2 may have such a shape that it can be easily mounted, in particular, in the region of the aircraft door. It is also possible to realize different shapes of the base body 2 in dependence on the point of installation.
The holder 1 also comprises a clamp 4 that is attached to the base body 2 on both of its end regions.
For example, cables may extend in the space 7 formed between the clamp 4 and the base body 2 and are clamped against the base body 2 by the clamp 4.
The pivoting region A is described below with reference to
When installing the clamp 4, it is initially inserted into the base body 2 at the pivot point 8 at an angle of 90°, as indicated by the horizontal double arrow. The end region of the leg 5 of the clamp 4 is suitably designed, for example, such that it can be clamped into a correspondingly designed clip on the base body 2 by means of a press fit. According to the exemplary embodiment, the clamp 4 is then pivoted upward by 90° as indicated by the other double arrow. This automatically causes the clamp 4 to be geometrically secured at the bottom in the pivot point.
According to
As mentioned above, the clamp 4 is initially inserted into the base body 2 at the pivot point 8 at an angle of 90° and then pivoted upward by 90°. During this process, the projections 9 snap into an opening 10 arranged in the base body 2 as shown in
According to the invention, the holder 1 also comprises a pin 11 that is arranged in the interlocking region B and additionally secures the projections 9 snapped into the opening 10 of the base body 2 from sliding out.
Although the preceding description of the invention referred to one exemplary embodiment, it should be understood that this embodiment could be modified and changed in different ways without departing from the scope of the invention. For example, it would be possible to choose another suitable shape for the clamp in order to fix parts other than electric cables on the base body. It should also be understood that the holder according to the invention is not only suitable for use in aircraft, but also in the automotive industry or in other fields, in which electric cables or conduits need to be reliably held and guided such that they can be easily serviced.
The holder according to the invention is not only suitable for holding bundles of cables, but may also be designed for holding pipes or hoses. The holder is particularly suitable for holding movable cables.
It should be noted that the term “comprising” does not exclude other elements or steps and the “a” or “an” does not exclude a plurality. Also elements described in association with different embodiments may be combined.
It should also be noted that reference signs in the claims shall not be construed as limiting the scope of the claims.
Number | Date | Country | Kind |
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10 2004 011 184.7 | Mar 2004 | DE | national |
This application claims the benefit of the filing date of U.S. Provisional Patent Application No. 60/598,567 filed Aug. 3, 2004, the disclosure of which is hereby incorporated herein by reference.
Number | Date | Country | |
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60598567 | Aug 2004 | US |