CN201435246Y - Heat-resistant shielded cable for aviation - Google Patents

Heat-resistant shielded cable for aviation Download PDF

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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
Application number
CN2009201719100U
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Chinese (zh)
Inventor
刘东兵
张晓飞
刘应武
杭金宏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Anhui Lieta Cable Group Co Ltd
Original Assignee
Anhui Lieta Cable Group Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Anhui Lieta Cable Group Co Ltd filed Critical Anhui Lieta Cable Group Co Ltd
Priority to CN2009201719100U priority Critical patent/CN201435246Y/en
Application granted granted Critical
Publication of CN201435246Y publication Critical patent/CN201435246Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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

A kind of high temperature resistant aviation shielded type cable
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.
Conductor 1 adopts regular lay configuration, and the twisted wire pitch is between 10-12 times, has flexibility surface rounding property preferably to guarantee conductor, and insulating barrier is easily peeled off.
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.
CN2009201719100U 2009-05-05 2009-05-05 Heat-resistant shielded cable for aviation Expired - Fee Related CN201435246Y (en)

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

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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)

* Cited by examiner, † Cited by third party
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

Cited By (2)

* Cited by examiner, † Cited by third party
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

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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