CABLE JUNCTION WITH INTEGRATED SPACE CHARGE DETECTOR
20200150171 ยท 2020-05-14
Inventors
Cpc classification
H02G1/00
ELECTRICITY
G01R31/1272
PHYSICS
International classification
Abstract
This power cable junction (10) has an end part of a power cable which has an electrically insulating material (122). The junction (10) has a predetermined region containing a module for measuring the space charge of the insulating material (122).
Claims
1. Power cable junction comprising: an end part of a power cable, said cable having an electrically insulating material, wherein said power has a predetermined region containing a module for measuring the space charge of said insulating material.
2. Junction according to claim 1, wherein said measurement module comprises at least two electrodes.
3. Junction according to claim 2, wherein said measurement module comprises six electrodes.
4. Junction according to claim 1, wherein said measurement module comprises a piezoelectric sensor.
5. Junction according to claim 4, wherein said measurement module further comprises at least one mechanical vibration damping element.
6. Junction according to claim 1, wherein said measurement module comprises an acoustic delay line.
7. Junction according to claim 1, wherein said measurement module comprises means for connecting a source of high-voltage electrical pulses.
8. Power cable, wherein said power cable is equipped with at least one junction according to claim 1.
9. Cable according to claim 8, wherein said cable is of the high-voltage direct current, or HVDC, type.
10. Cable according to claim 8, wherein said cable is extruded.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0033] Other aspects and advantages of the invention will become apparent on reading the following detailed description of particular embodiments, given as purely nonlimiting examples, with reference to the attached drawings, in which:
[0034]
[0035]
DETAILED DESCRIPTION
[0036] As the particular embodiment of
[0037] The power cable 12 is for example of the high-voltage direct current, or HVDC, type.
[0038] As is known per se, the cable 12 comprises a central conductor 120, covered by a layer of electrically insulating material 122, which is itself covered by a layer of semiconductive material 124. The cable 12 can also comprise an internal semiconductive layer (not represented).
[0039] The insulating material of the layer 122 is for example chemically cross-linked polyethylene or CXLPE. It can also be a thermoplastic insulation material based on polyethylene or polypropylene. All these materials, which are given as nonlimiting examples, can be pure or filled.
[0040] According to the present invention, the junction 10 comprises a predetermined region containing a module for measuring the space charge of the insulating material of the layer 122.
[0041] This predetermined region of the junction 10 is for example one of its two ends.
[0042] The space charge measurement module comprises at least two electrodes 14. It can for example comprise six thereof. It also comprises a point of connection to the screen of the cable 12.
[0043] In the particular embodiment illustrated in
[0044] The space charge measurement module further comprises a piezoelectric sensor 16.
[0045] The piezoelectric sensor 16 can for example be of the type based on polyvinylidene fluoride or PVDF. As a variant, it could also be of the type based on barium titanate (BaTiO.sub.3).
[0046] The electrodes 14 and the connection to a central conductor 22 of a link 32 formed for example by a coaxial cable are used to create a high-voltage equipotential zone in line with the piezoelectric sensor 16.
[0047] The electrodes 14 are advantageously produced by a knit of tinned copper wires. As a variant, they can be produced in the form of copper ribbon, possibly tinned, or any other metallic material.
[0048] The electrodes 14 are for example wound around the cable 12, over its semiconductive layer 124.
[0049] Advantageously, the piezoelectric sensor 16 is separated from the outside from the electrostatic point of view, that is to say that it is in a Faraday cage, within the mechanical protective enclosure of the junction 10.
[0050] Advantageously, in order to eliminate the parasitic mechanical vibrations which disrupt the space charge measurement signal, the measurement module comprises at least one mechanical vibration damping element 18 placed in the vicinity of the piezoelectric sensor 16, for example in contact therewith.
[0051] The damping element 18 is for example made of EPDM (ethylene propylene diene monomer) or of rubber or any other material that absorbs mechanical vibrations.
[0052] To measure the space charge in the electrically insulating material 122 of the cable 12, the measurement module uses the PEA technique mentioned in the introduction.
[0053] To this end, the measurement module comprises a link formed for example by a coaxial cable 32, whose central conductor 22 is linked to the electrodes 14 and whose coaxial conductor is linked to the metal screen of the cable 12 and of the junction 10. This coaxial cable 32 and its central conductor 22 are means for connecting a source of high-voltage electrical pulses. The source of electrical pulses is external to the junction.
[0054] In order to temporally separate the PEA signal from the parasitic vibrations caused by the electrical pulse, the measurement module also comprises an acoustic delay line 20, connected to the piezoelectric sensor 16.
[0055] The electrical field applied to the electrically insulating material of the cable 12 by the source of high-voltage electrical pulses generally lies between 0.2 kV and 2 kV per mm of thickness of insulation of the cable 12 and is preferably approximately equal to 0.5 kV/mm.
[0056] Upon the application of this electrical field, the piezoelectric sensor 16 detects the acoustic pressure waves originating from the charges present in the cable 12. The measurement of these charges can be collected via a link connected to the piezoelectric sensor 16 and formed for example by a coaxial cable 24.
[0057] The diagram of
[0058] The external source 26 of high-voltage electrical pulses is powered by a high-voltage generator 28 (typically 10 kV) and generates high-voltage pulses from a wave form 30. These pulses are supplied as input to the junction 10 via the link 32 formed for example by a coaxial cable and via a decoupling capacitor 34.
[0059] In order to collect the measurement of the space charge, the signal originating from the piezoelectric sensor 16 is routed via the coaxial cable 24 to a display device 36, such as an oscilloscope.
[0060] The display device 36 can moreover be equipped with a means for triggering the high-voltage electrical pulses, connected to the external source 26 of high-voltage electrical pulses via a link 38.
[0061] Thus, a cable 12 according to the invention, equipped with at least one junction 10 as described above, presents, by virtue of the space charge measurement module contained in the junction, an integrated indicator of the trend of the quality of its electrical insulation. The primary application targeted by the invention concerns high-voltage direct current, or HVDC, cables, which are for example extruded cables, but the invention is not limited to this type of cables.
[0062] The invention has been described here in its application to the measurement of the space charge within the electrically insulating material of the power cable that the junction links to another cable. However, the invention applies similarly to the measurement of the space charge within the electrically insulating material of the junction itself.