The invention relates to a shielded or double-shielded electric harness with two sealing barriers for zones in which the environment is severe in terms of temperature, vibration, and electromagnetic disturbances, such as, for example, inside a turbojet or a turboprop engine.
A harness of this type comprises a set of electric cables and wires that serve, for example, to provide connections between various pieces of electrical equipment such as a system for electronically regulating the engine, or sensors.
At present, two different technologies are used for assembling electric harnesses, depending on the temperatures that exist in their zones of use. When the maximum temperature in said zones does not exceed 150° C., the electrical connection wires and cables are generally protected by means of a structure comprising a textile braid forming a first layer protecting the electric wires and cables, a tubular braid surrounding the textile braid and providing electromagnetic shielding, and an outer sheath of heat-shrink polymer and having, at its end, an endpiece made of a heat-shrink polymer and serving both to protect the end of the shielding braid on the tubular metal or composite connection part and also to connect with the outer sheath of that connection part. That structure has the advantage of accommodating relatively short radii of curvature, but its ability to withstand temperature is limited to 150° C.
In zones where the temperature is higher and might reach a peak value of 260° C., the electric wires and cables are protected by a tubular structure that comprises an inner sheath of polytetrafluoroethylene (PTFE), a metal braid for electromagnetic shielding surrounding said sheath, and a textile braid surrounding the shielding braid and made of a material that withstands high temperatures, e.g. aramid fibers, the end of said structure being held by a mechanical collar against a metal or composite connection part.
The drawback of that structure is that it is heavier than the preceding structure and does not accept short radii of curvature.
An object of the present invention is to provide a single structure for protecting and connecting electric wires and cables of the above-mentioned type, that does not present the drawbacks of known structures, that can be used equally well in zones having a maximum temperature of about 150° C. and in zones where the peak temperature can reach 260° C., and that accepts relatively short radii of curvature.
To this end, the invention provides a shielded and sealed electric harness, in particular for an airplane engine, comprising a set of conductor elements fitted at their ends with connectors or branch joints, each conductor element comprising at least one electrically conductive wire or cable mounted in a tubular protective and shielding structure that comprises a tubular inner textile braid and an intermediate metal braid for electromagnetic shielding, wherein the tubular structure also comprises a corrugated outer sheath made of polymer, surrounding the intermediate metal braid and having at least one end secured to a tubular endpiece of heat-shrink material, said tubular endpiece enabling the outer sheath to be fastened onto a connector or a branch joint, and serving to clamp and secure one end of the intermediate metal braid, by means of a metal collar or ferrule onto a tubular metal part of the connector or of the branch joint.
The outer sheath is made of a material that withstands high temperatures, e.g. PTFE, and its corrugated structure enables it to accept short radii of curvature.
The endpiece of heat-shrink material that is fastened to the end of said outer sheath serves to fasten the sheath onto a connector or a branch coupling. The end of the shielding metal braid is clamped against said connector or coupling, advantageously by means of a metal ferrule or of an optionally electrically conductive collar so as to provide continuity of the electromagnetic shielding.
In a preferred embodiment of the invention, the end of the outer sheath, when made of PTFE, is treated chemically so as to be capable of being adhesively bonded to the endpiece made of heat-shrink material, e.g. by means of an epoxy adhesive.
The heat-shrink endpiece is made of a plastics material that withstands high temperatures, in particular such as a fluorinated elastomer sold under the Viton trademark, or a silicone elastomer. The ferrule or the collar for clamping the end of the shielding metal braid on the connector or the coupling is made of stainless steel or of copper-nickel alloy, the shielding metal braid advantageously being made of copper-nickel alloy.
The metal part of the connector or the coupling against which the end of the shielding metal braid is clamped is itself preferably made of titanium, which material is selected because of its light weight and its mechanical characteristics.
In order to ensure continuity of the electromagnetic shielding, the titanium part may be given surface treatment, e.g. receiving a layer of nickel that is deposited by a chemical technique.
The textile tubular protection braid is preferably made of aramid fibers, such as those sold under the Nomex trademark.
In general, the harness of the invention presents the advantage of a weight saving of about 20% relative to previously-used technologies. Furthermore it is intended for use equally well in medium temperature zones and in high temperature zones. This results in a simplification to the fabrication of such harnesses in terms of supply and assembly of their components.
The invention can be better understood and other details, characteristics, and advantages thereof appear more clearly on reading the following description made by way of example with reference to the accompanying drawing, in which:
The harness 10 shown in
More precisely, the harness of
As can be seen more clearly in
According to the invention, the structure 22 comprises a tubular inner textile braid 24 surrounding the conductor(s) 20, a metal tubular braid 26 providing electromagnetic shielding, which braid surrounds the inner textile braid 24, and an outer sheath 28 of corrugated shape, surrounding the shielding metal braid 26.
The inner textile braid 24 is made of aramid fibers of the type sold under the Nomex trademark.
The shielding braid is made of nickel-plated copper, and the outer sheath 28 is made of PTFE.
The end of the sheath 28 is fastened, advantageously by bonding by means of an epoxy adhesive, onto the end of a cylindrical endpiece 30 of heat-shrink plastics material, such as a fluorinated elastomer of the type sold under the Viton trademark, or in a variant a silicone elastomer.
In order to enable it to be adhesively bonded to the endpiece 30, the end of the sheath 28 is subjected to chemical treatment of the sodium ammonia type for eliminating structure fluorine atoms from the sheath.
The heat-shrink endpiece 30 surrounds the end of a cylindrical part 32 that is preferably made of titanium, that is secured to a connector 16 or 18, and that includes a cylindrical tail 34 onto which the end of the metal braid 26 is clamped by means of a metal collar or ferrule 36 of stainless steel, in turn covered by the heat-shrink endpiece 30.
In order to enable the titanium part 32 to provide continuity of electromagnetic shielding, its surface is coated in a layer of chemically-deposited nickel, with the end of the metal braid 26 being clamped thereagainst by the metal collar or ferrule 36.
The end of the endpiece 30 remote from the outer sheath 28 includes an inner annular rim for catching an outer annular rim 40 on the cylindrical tail 34 of the part 32.
Number | Date | Country | Kind |
---|---|---|---|
06 04487 | May 2006 | FR | national |
Number | Name | Date | Kind |
---|---|---|---|
4693323 | Owensby | Sep 1987 | A |
4766267 | Gray et al. | Aug 1988 | A |
4786757 | Owensby et al. | Nov 1988 | A |
4896000 | Procter et al. | Jan 1990 | A |
5399808 | Carter et al. | Mar 1995 | A |
5571992 | Maleski et al. | Nov 1996 | A |
5619015 | Kirma | Apr 1997 | A |
6066800 | Renaud | May 2000 | A |
6143986 | Anderson et al. | Nov 2000 | A |
6423952 | Meisiek | Jul 2002 | B1 |
20010011601 | Renaud | Aug 2001 | A1 |
Number | Date | Country |
---|---|---|
0 238 203 | Sep 1987 | EP |
0 693 811 | Jan 1996 | EP |
1 091 623 | Apr 2001 | EP |
Number | Date | Country | |
---|---|---|---|
20070270037 A1 | Nov 2007 | US |