CN103137254A - Novel aviation cable protecting cover - Google Patents

Novel aviation cable protecting cover Download PDF

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Publication number
CN103137254A
CN103137254A CN2011103901453A CN201110390145A CN103137254A CN 103137254 A CN103137254 A CN 103137254A CN 2011103901453 A CN2011103901453 A CN 2011103901453A CN 201110390145 A CN201110390145 A CN 201110390145A CN 103137254 A CN103137254 A CN 103137254A
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CN
China
Prior art keywords
aramid fiber
protective jacket
novel aviation
monofilament
fiber bundle
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Application number
CN2011103901453A
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Chinese (zh)
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CN103137254B (en
Inventor
张春红
黄宗汉
董书惠
黄瑞昌
李英
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.)
Shenyang Liming Aero Engine Group Co Ltd
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Shenyang Liming Aero Engine Group Co Ltd
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Publication date
Application filed by Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN201110390145.3A priority Critical patent/CN103137254B/en
Publication of CN103137254A publication Critical patent/CN103137254A/en
Application granted granted Critical
Publication of CN103137254B publication Critical patent/CN103137254B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The invention provides a novel aviation cable protecting cover which is characterized in that firstly, an aramid fiber bundle serves as a core wire, silver plating copper flat silk wires 2 are wound outside of the aramid fiber bundle, the aramid fiber bundle 1 and the silver plating copper flat silk wires 2 are mutually twisted and wound at the angle of alpha to form monofilaments 3, the monofilaments are woven according to a rule of same distribution, and a cable protecting cover 30 with certain density and various standards is formed by the monofilaments with different numbers of strands and different numbers of monofilaments in each strand in a woven mode. The novel aviation cable protection cover has the advantages that compared with a traditional metal protecting cover, weight is reduced by 30% to 50%, a character is soft, cables are flexible in assembly and installation on an engine, an adaptor is eliminated in cable manufacture, manufacture is simple and convenient to achieve, and structure is simple.

Description

A kind of Novel aviation cable protective jacket
Technical field
The present invention relates to the cable protective field, relate in particular to a kind of Novel aviation cable protective jacket.
Background technology
Traditional engine uses metal knitted protective jacket, and skin is wire, and internal layer is the fluoroplastics inner sleeve, and on whole cable, the protective jacket specification is different, and bifurcation connects with the aluminum adapter; Protective jacket this as assembly, upper surface cover has the nut that is connected with adapter, is connected with metal lining between nut and protective jacket, metal lining is on protective jacket, and this protective jacket has increased the weight of the weight of cable, and quality is harder, can not be arbitrarily crooked, assembling and repetition maintainability are poor.
Summary of the invention
The technical problem that the present invention solves is: a kind of Novel aviation cable protective jacket is provided, and lightweight, quality is soft, and stronger flexibility is arranged, and is simple in structure.
Technical program of the present invention lies in: a kind of Novel aviation cable protective jacket is provided, has it is characterized in that: first take aramid fiber bundle 1 as heart yearn, twine silver-plated copper flat filament line 2 outward, both mutually revolve sth. made by twisting and be entwined monofilament 3 to twine wrap angle sigma,
Described wrap angle sigma=the tg that twines -1h /π (D+d);
H is the pitch that is wrapped (mm),
D is aramid fiber bundle 1 external diameter approximation (mm),
D is silver-plated copper flat filament line 2 external diameter approximations (mm);
The rule braiding that monofilament 3 is arranged with identical by different number of share of stocks, per share middle different monofilament radicals, is woven into and has certain density, the cable protective kit 30 of different size.
Described aramid fiber bundle 1, be PPTA, the preferred Twaron 111 industrial aramid fiber long filaments of type 420dtex, 1dtex refers to that this fiber material of 1g pulls into the diameter of the silk of the long even thickness of ten thousand metres, and 420dtex represents that the aramid fiber that this synnema is 1.5dtex by 420 every thicknesses forms.
Described silver-plated copper flat filament line 2 is the yellow looping silk with filamentary silver, and width is 0.16mm~0.17mm, and thickness is 0.04mm~0.05mm, silver thickness>2.1 μ m, resistivity<0.018 Ω mm 2 /M(20 ℃), percentage elongation<18%.
The serviceability temperature of described Novel aviation cable protective jacket is :-60 ℃~200 ℃.
Beneficial effect of the present invention: Novel aviation cable protective jacket provided by the invention is compared with the traditional metal protective jacket, alleviate 30%~50% on weight, quality is soft, make cable assembly and be equipped with stronger flexibility on engine, on making, cable cancelled adapter, simple for production, simple in structure.
Description of drawings
Fig. 1 is the looping process schematic diagram that monofilament is used in Novel aviation cable protective jacket braiding of the present invention.
Fig. 2 is Novel aviation cable protecting jacket structure schematic diagram of the present invention.
Fig. 3 is traditional metal protective jacket partial cables assembly schematic diagram, and wherein 10 is adapters, the 20th, and the metal protection cover.
Fig. 4 is that Novel aviation cable protective jacket of the present invention uses view.
Fig. 5 is Novel aviation cable protective jacket weaving parameter list of the present invention.
Embodiment
Illustrate content of the present invention below in conjunction with accompanying drawing 1~5 and embodiment.
Novel aviation cable protective jacket 30 provided by the invention is formed by monofilament 3 braidings, described monofilament 3 is take aramid fiber bundle 1 as heart yearn, twine silver-plated copper flat filament line 2 outward, described aramid fiber bundle 1, be PPTA, the preferred industrial aramid fiber long filament of 420dtex (1dtex is the diameter that this fiber material of 1g pulls into the silk of the long even thickness of ten thousand metres, and 420dtex is that the aramid fiber that a synnema is 1.5dtex by 420 every thicknesses forms); In the preferred embodiment of the present invention, the line density of aramid fiber bundle 1 used (dtex) is 448, fracture strength (CN/dtex) is 19.1, elongation at break (%) 2.47; The ultimate strength CV(% of described silver-plated copper flat filament line 2) be 2.39, elongation at break (%) is 3.24.
Fig. 1 is the looping process schematic diagram that monofilament is used in Novel aviation cable protective jacket braiding of the present invention, adopt high-speed wrapping machine, under the rotating speed of 30000 rev/mins, aramid fiber bundle 1 and silver-plated copper flat filament line 2 are revolved to twist with the fingers mutually be wound in monofilament, silver-plated copper flat filament line 2 specifications are 0.17mm * 0.05mm, and the 100mm wire is wound around number of times 120~130, winding direction to the right, finished product external diameter 0.25mm~0.29mm, weight is not more than 0.12g/m, twines wrap angle sigma=tg -1h /π (D+d); H is the pitch that is wrapped (mm), and D is aramid fiber bundle 1 external diameter approximation (mm), and d is silver-plated copper flat filament line 2 external diameter approximations (mm); In monofilament 3 braiding processes, aramid fiber bundle 1 must not have any distortion, must not twist, and silver-plated copper flat filament line 2 wants tight looping on aramid fiber bundle 1, and the looping pitch is even, and silver-plated copper flat filament line 2 must not fracture, arch camber, loose or knotting, damage etc.
Fig. 2 is Novel aviation cable protecting jacket structure schematic diagram of the present invention, can see the A-A cross section monofilament situation of arranging; Fig. 5 is Novel aviation cable protective jacket weaving parameter list of the present invention, press product requirement and formulate weaving, monofilament 3 has been compiled into certain density with identical rule of arranging, have the Novel aviation cable protective jacket of 2 * 4,3 * 6,6 * 10,24 * 32 4 kinds of specifications, the weaving parameter as shown in Figure 5.
Fig. 4 is that Novel aviation cable protective jacket of the present invention uses view, Fig. 3 is traditional metal protective jacket partial cables assembly schematic diagram, and wherein 10 is adapters, the 20th, and the metal protection cover, compare with the traditional metal protective jacket, Novel aviation cable protective jacket advantage of the present invention is as follows:
First, quality gently makes novel cable be superior to other engine cables, need between the traditional metal protective jacket to realize cable branch with metal adaptor 10, and novel cable as shown in Figure 4 cable branch realize with the wrapping line, the crust of whole cable all need not the intervention of metal object, and then having alleviated the weight of engine, the novel cable assembly is 72% of metal protection cover cable assembly weight.
The second, good assembling, the Novel aviation cable protective jacket is very soft, can be arbitrarily crooked, thereby can be crooked fixing flexibly in the process of making cable, have more flexibility.
The 3rd, core has more the repetition maintainability, and the bifurcation of metal protection cover cable has adapter 10, and the wire core is kept in adapter, will take adapter in maintenance process apart and could use the surplus core, causes inconvenient maintenance; Novel cable employing wrapping line is branch fixedly, and quality is soft, and length requirement is loose, its core and two directly is contained in cable, and neither impact assembling can needn't be decomposed cable again when maintenance, directly place under repair at the cable branch place, and can repeat to repair, so maintainability is strong.
The above is only preferred embodiment of the present invention, is not to limit application range of the present invention; All other do not break away from the equivalence of completing under disclosed essence and change or modify, and all should be included in following claims scope.

Claims (5)

1. a Novel aviation cable protective jacket, is characterized in that: take aramid fiber bundle (1) as heart yearn, twine silver-plated copper flat filament line (2) outward, both mutually revolve sth. made by twisting and form monofilament (3); The rule braiding that monofilament (3) is arranged with identical by different number of share of stocks, per share middle different monofilament radicals, is woven into and has certain density, the cable protective kit of different size (30).
2. Novel aviation cable protective jacket as claimed in claim 1, it is characterized in that: described aramid fiber bundle (1) is PPTA, the industrial aramid fiber long filament of 420dtex.
3. Novel aviation cable protective jacket as claimed in claim 1, it is characterized in that: described silver-plated copper flat filament line (2), width are 0.16mm~0.17mm, thickness is 0.04mm~0.05mm, silver thickness>2.1 μ m, resistivity<0.018 Ω mm 2 /M(20 ℃), percentage elongation<18%.
4. Novel aviation cable protective jacket as claimed in claim 1, it is characterized in that: the serviceability temperature of described Novel aviation cable protective jacket is :-60 ℃~200 ℃.
In a Novel aviation cable protective jacket braiding process with the looping method of monofilament, it is characterized in that: monofilament (3) be heart yearn by aramid fiber bundle (1), twines silver-plated copper flat filament line (2) outward, both mutually revolve sth. made by twisting and be entwined monofilament (3) to twine wrap angle sigma,
Described wrap angle sigma=the tg that twines -1h /π (D+d);
H is the pitch that is wrapped (mm),
D is aramid fiber bundle (1) external diameter approximation (mm),
D is silver-plated copper flat filament line (2) external diameter approximation (mm).
CN201110390145.3A 2011-12-01 2011-12-01 A kind of Aeronautical cable protective sleeve Expired - Fee Related CN103137254B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201110390145.3A CN103137254B (en) 2011-12-01 2011-12-01 A kind of Aeronautical cable protective sleeve

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201110390145.3A CN103137254B (en) 2011-12-01 2011-12-01 A kind of Aeronautical cable protective sleeve

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CN103137254A true CN103137254A (en) 2013-06-05
CN103137254B CN103137254B (en) 2016-06-01

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106229053A (en) * 2016-09-20 2016-12-14 芜湖航天特种电缆厂股份有限公司 Tension, wave prevention sleeve high temperature resistant, fire-retardant, soft and preparation method thereof
CN108899139A (en) * 2018-06-13 2018-11-27 江西瑞金金字电线电缆有限公司 A kind of weaving method of Aviation cable protective case
CN109659079A (en) * 2018-11-02 2019-04-19 广州凯恒科塑有限公司 Thin-wall wave-proof sleeve for aerospace and preparation method thereof

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101494098A (en) * 2008-12-15 2009-07-29 安徽滨江电缆股份有限公司 High temperature resistant compensating cable
CN201307435Y (en) * 2008-12-12 2009-09-09 四川明星电缆股份有限公司 Shielded type radiation-resistant soft control cable
CN201438390U (en) * 2009-06-19 2010-04-14 沈阳黎明航空发动机(集团)有限责任公司 Aeronautical cable protective sleeve
CN101702956A (en) * 2007-03-29 2010-05-05 瑞拉特斯有限公司 Protective sheath for cables, tubes and the like

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101702956A (en) * 2007-03-29 2010-05-05 瑞拉特斯有限公司 Protective sheath for cables, tubes and the like
CN201307435Y (en) * 2008-12-12 2009-09-09 四川明星电缆股份有限公司 Shielded type radiation-resistant soft control cable
CN101494098A (en) * 2008-12-15 2009-07-29 安徽滨江电缆股份有限公司 High temperature resistant compensating cable
CN201438390U (en) * 2009-06-19 2010-04-14 沈阳黎明航空发动机(集团)有限责任公司 Aeronautical cable protective sleeve

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106229053A (en) * 2016-09-20 2016-12-14 芜湖航天特种电缆厂股份有限公司 Tension, wave prevention sleeve high temperature resistant, fire-retardant, soft and preparation method thereof
CN108899139A (en) * 2018-06-13 2018-11-27 江西瑞金金字电线电缆有限公司 A kind of weaving method of Aviation cable protective case
CN109659079A (en) * 2018-11-02 2019-04-19 广州凯恒科塑有限公司 Thin-wall wave-proof sleeve for aerospace and preparation method thereof
CN109659079B (en) * 2018-11-02 2022-04-05 广州凯恒科塑有限公司 Thin-wall wave-proof sleeve for aerospace and preparation method thereof

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Granted publication date: 20160601

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