CN201435246Y - Heat-resistant shielded cable for aviation - Google Patents
Heat-resistant shielded cable for aviation Download PDFInfo
- Publication number
- CN201435246Y CN201435246Y CN2009201719100U CN200920171910U CN201435246Y CN 201435246 Y CN201435246 Y CN 201435246Y CN 2009201719100 U CN2009201719100 U CN 2009201719100U CN 200920171910 U CN200920171910 U CN 200920171910U CN 201435246 Y CN201435246 Y CN 201435246Y
- Authority
- CN
- China
- Prior art keywords
- conductor
- cable
- high temperature
- temperature resistant
- aviation
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 239000004020 conductor Substances 0.000 claims abstract description 39
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 20
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 15
- 229910052802 copper Inorganic materials 0.000 claims abstract description 12
- 239000010949 copper Substances 0.000 claims abstract description 12
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 10
- 238000007747 plating Methods 0.000 claims abstract description 10
- 229910052709 silver Inorganic materials 0.000 claims abstract description 10
- 239000004332 silver Substances 0.000 claims abstract description 10
- 239000000463 material Substances 0.000 claims abstract description 9
- 239000004697 Polyetherimide Substances 0.000 claims abstract description 5
- RTZKZFJDLAIYFH-UHFFFAOYSA-N ether Substances CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 claims abstract description 5
- 229920001601 polyetherimide Polymers 0.000 claims abstract description 5
- 229920002725 thermoplastic elastomer Polymers 0.000 claims abstract description 5
- 230000004888 barrier function Effects 0.000 claims description 8
- 238000000576 coating method Methods 0.000 claims description 4
- 239000011248 coating agent Substances 0.000 claims description 3
- 230000008029 eradication Effects 0.000 claims description 3
- 230000032683 aging Effects 0.000 abstract description 5
- 239000003063 flame retardant Substances 0.000 abstract description 3
- 229910052736 halogen Inorganic materials 0.000 abstract description 3
- 150000002367 halogens Chemical class 0.000 abstract description 3
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 abstract description 2
- 229910052698 phosphorus Inorganic materials 0.000 abstract description 2
- 239000011574 phosphorus Substances 0.000 abstract description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 abstract 2
- RNFJDJUURJAICM-UHFFFAOYSA-N 2,2,4,4,6,6-hexaphenoxy-1,3,5-triaza-2$l^{5},4$l^{5},6$l^{5}-triphosphacyclohexa-1,3,5-triene Chemical compound N=1P(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP=1(OC=1C=CC=CC=1)OC1=CC=CC=C1 RNFJDJUURJAICM-UHFFFAOYSA-N 0.000 abstract 1
- 238000009941 weaving Methods 0.000 abstract 1
- 239000000126 substance Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 230000002045 lasting effect Effects 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- CBENFWSGALASAD-UHFFFAOYSA-N Ozone Chemical compound [O-][O+]=O CBENFWSGALASAD-UHFFFAOYSA-N 0.000 description 1
- CDBYLPFSWZWCQE-UHFFFAOYSA-L Sodium Carbonate Chemical compound [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 238000010616 electrical installation Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000004079 fireproofing Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000002480 mineral oil Substances 0.000 description 1
- 235000010446 mineral oil Nutrition 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 230000001172 regenerating effect Effects 0.000 description 1
- 238000012958 reprocessing Methods 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Images
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- Insulated Conductors (AREA)
- Ropes Or Cables (AREA)
Abstract
A heat-resistant shielded cable for aviation is characterized in that a conductor has a twisting structure of a plurality of nickel plating, silver or tin plated soft copper filaments; a polyester-ether thermoplastic elastomer TPE-E insulating layer is extruded on the conductor so as to form an insulated conductor core; one insulated conductor core or a plurality of insulated conductor cores are twisted to form a cable so as to form a cable conductor; and the cable conductor is externally provided with a nickel plating, silver or tin plated copper weaving shielding layer, and a thin-wall sheath layer taking polyetherimide as materials is extruded on the surface. The heat-resistant shielded cable has combination properties of high/low temperature resistance, humidity resistance, weather resistance, ageing resistance, halogen free, phosphorus free, flame retardant property, electromagnetic interference resistance, softness and the like, can adapt to various working environment, and is suitable for being used as connecting electric wires of aerospace planes.
Description
Technical field
The utility model relates to the aviation cable, relates in particular to a kind of high temperature resistant aviation shielded type cable, belongs to technical field of electric wires and cables.
Background technology
Aerospace equipment has requirements such as volume is little, in light weight along with the raising requirement of equipment performance to special installation.As spacecraft electrical installation, instrument and meter connecting line, want that cube is little, to adapt to all kinds of adverse circumstances, ampacity big and to bear overload capacity strong, and require cable to have favorable mechanical physical property, electric property and lay conveniently, cable should have characteristics such as anti-electromagnetic shielding, fire-retardant, Halogen, oil resistant, heatproof, moisture-proof, and safety guarantee is had relatively high expectations.But existing normal cable can not satisfy this requirement.
The utility model content
The utility model is for avoiding above-mentioned existing in prior technology weak point, provide a kind of and can possess combination properties such as anti-high/low temperature, moisture-proof, weather-proof, ageing-resistant, Halogen, without phosphorus, fire-retardant and softness, can adapt to the high temperature resistant aviation shielded type cable of multiple different operational environment.
The utility model technical solution problem adopts following technical scheme:
The high temperature resistant aviation of the utility model is that conductor is the lay configuration of many nickel plating, silver or zinc-plated soft copper monofilament with the design feature of shielded type cable, extrudes polyester-ether thermoplastic elastomer TPE-E insulating barrier and constitute insulated wire cores on conductor; Constitute cable conductor with single insulated wire cores or by the stranded stranding of many eradications edge core; Nickel plating, silver or tinned copper wire woven shield are set, and to extrude with the Polyetherimide on the top layer be the thin-walled restrictive coating of material outside cable conductor.
So aviation that the utility model is high temperature resistant also exists with the design feature of shielded type cable:
The conductor that described soft copper monofilament constitutes is chosen as the 2nd class conductor or the 5th class conductor that meets GB/T3956.
Described conductor adopts regular lay configuration, and the twisted wire pitch is between 10-12 times.
The sectional area of described conductor is 0.08～8mm
2
Described insulated wire cores is the 2-4 core.
Compared with the prior art, the utility model beneficial effect is embodied in:
1, the utility model adopts the conductor that nickel plating, silver or zinc-plated soft copper monofilament constitute, and can prevent the aging catalytic action of copper conductor to insulating barrier effectively, to guarantee the useful life of insulating barrier.Simultaneously, in plating nickel on surface, silver or the zinc-plated oxidation that also can effectively prevent soft copper monofilament conductor itself of soft copper monofilament, increase the security reliability in the use.
2, insulating material and sheath material are material with polyester-ether thermoplastic elastomer TPE-E material and Polyetherimide respectively in the utility model, have the chemical resistance of wide range, and it also has following performance:
(1) excellent heat resisting, heat-resisting peak reach 200 ℃, and lasting serviceability temperature is 150 ℃;
(2) splendid mar proof, electric property that it is good and mechanical performance satisfy the requirement of low-voltage cable fully;
(3) fabulous UV resistant performance;
(4) insulating barrier has lasting color retention after aging;
(5) have chemical substances such as favorable chemical resistance energy, ability mineral oil, soda acid, ozone;
(6) and have good flame retardancy, the sheath material oxygen index reaches 48, is higher than common fire proofing far away;
(7) insulation and sheath material mechanical performance and excellent electrical properties can be extruded thin layer, reduce cost, and reduce the cable volume;
(8) owing to be directly to extrude processing, do not need the equipment of extra preliminary treatment and reprocessing;
(9) because be thermoplastic, the processing of can regenerating, and the heat ageing process is very slow, and very big recycling value is arranged, and meets environmental protection spirit.
3, screen adopts the braided metal material in the utility model, and cable has shielding properties and softness preferably.
Description of drawings
Fig. 1 is the utility model list cored structure schematic diagram.
Fig. 2 is the utility model multicore structure schematic diagram.
Number in the figure: 1 conductor; 2 insulating barriers; 3 screens; 4 restrictive coatings.
Below by embodiment, the utility model is described in further detail in conjunction with the accompanying drawings.
Embodiment
Referring to Fig. 1, Fig. 2, in the present embodiment, conductor 1 is the lay configuration of many nickel plating, silver or zinc-plated soft copper monofilament, extrudes polyester-ether thermoplastic elastomer TPE-E insulating barrier 2 and constitute insulated wire cores on conductor 1; Constitute cable conductor with single insulated wire cores (shown in Figure 1) or by the stranded stranding of many eradications edge core (shown in Figure 2); Nickel plating, silver or tinned copper wire woven shield 3 are set, and to extrude with the Polyetherimide on the top layer be the thin-walled restrictive coating 4 of material outside cable conductor.
In concrete the enforcement, the corresponding structure setting also comprises:
The conductor that the soft copper monofilament constitutes is chosen as the 2nd class conductor or the 5th class conductor that meets GB/T3956.
The sectional area of conductor 1 is 0.08～8mm
2
As required, insulated wire cores is set to two-four-core usually, Figure 2 shows that three core insulation cores
Claims (5)
1, a kind of high temperature resistant aviation shielded type cable is characterized in that conductor (1) is the lay configuration of many nickel plating, silver or zinc-plated soft copper monofilament, extrudes polyester-ether thermoplastic elastomer TPE-E insulating barrier (2) and constitute insulated wire cores on conductor (1); Constitute cable conductor with single insulated wire cores or by the stranded stranding of many eradications edge core; Nickel plating, silver or tinned copper wire woven shield (3) are set, and to extrude with the Polyetherimide on the top layer be the thin-walled restrictive coating (4) of material outside described cable conductor.
2, high temperature resistant aviation shielded type cable according to claim 1 is characterized in that the conductor that described soft copper monofilament constitutes is chosen as the 2nd class conductor or the 5th class conductor that meets GB/T3956.
3, high temperature resistant aviation shielded type cable according to claim 1 is characterized in that described conductor (1) adopts regular lay configuration, and the twisted wire pitch is between 10-12 times.
4, high temperature resistant aviation shielded type cable according to claim 1, the sectional area that it is characterized in that described conductor (1) is 0.08～8mm
2
5, high temperature resistant aviation shielded type cable according to claim 1 is characterized in that described insulated wire cores is the 2-4 core.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201719100U CN201435246Y (en) | 2009-05-05 | 2009-05-05 | Heat-resistant shielded cable for aviation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201719100U CN201435246Y (en) | 2009-05-05 | 2009-05-05 | Heat-resistant shielded cable for aviation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201435246Y true CN201435246Y (en) | 2010-03-31 |
Family
ID=42054061
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009201719100U Expired - Fee Related CN201435246Y (en) | 2009-05-05 | 2009-05-05 | Heat-resistant shielded cable for aviation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201435246Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103617832A (en) * | 2013-11-27 | 2014-03-05 | 苏州东威科技有限公司 | High-temperature resistance shielding connection wire |
| CN103903690A (en) * | 2014-03-06 | 2014-07-02 | 安徽猎塔电缆集团有限公司 | Aviation cable |
-
2009
- 2009-05-05 CN CN2009201719100U patent/CN201435246Y/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103617832A (en) * | 2013-11-27 | 2014-03-05 | 苏州东威科技有限公司 | High-temperature resistance shielding connection wire |
| CN103903690A (en) * | 2014-03-06 | 2014-07-02 | 安徽猎塔电缆集团有限公司 | Aviation cable |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100331 Termination date: 20140505 |