CN103943243A - Pressure-resistant aeronautic current lead - Google Patents

Pressure-resistant aeronautic current lead Download PDF

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Publication number
CN103943243A
CN103943243A CN201410114490.8A CN201410114490A CN103943243A CN 103943243 A CN103943243 A CN 103943243A CN 201410114490 A CN201410114490 A CN 201410114490A CN 103943243 A CN103943243 A CN 103943243A
Authority
CN
China
Prior art keywords
layer
polyethylene sheath
chlorosulfonated polyethylene
resistant
sheath layer
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.)
Pending
Application number
CN201410114490.8A
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Chinese (zh)
Inventor
夏振振
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.)
WUXI JINHUA CABLE MATERIAL Co Ltd
Original Assignee
WUXI JINHUA CABLE MATERIAL 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 WUXI JINHUA CABLE MATERIAL Co Ltd filed Critical WUXI JINHUA CABLE MATERIAL Co Ltd
Priority to CN201410114490.8A priority Critical patent/CN103943243A/en
Publication of CN103943243A publication Critical patent/CN103943243A/en
Pending legal-status Critical Current

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  • Manufacturing Of Electric Cables (AREA)
  • Insulated Conductors (AREA)

Abstract

The invention discloses a pressure-resistant aeronautic current lead. The pressure-resistant aeronautic current lead is composed of control wire cores, a chlorosulfonated polyethylene sheath layer, a tinned copper tape shielding layer, a polytetrafluoroethylene insulating layer and an aluminum armor polyethylene sheath layer, wherein the control wire cores are extruded in the chlorosulfonated polyethylene sheath layer, the number of the control wire cores is three, each control wire core is composed of a polyester fiber layer as a middle layer, an ethylene-propylene rubber insulating layer wrapped outside the polyester fiber layer and four tinned nickel conductor cable cores extruded inside the ethylene-propylene rubber insulating layer, and the chlorosulfonated polyethylene sheath layer is wrapped in the tinned copper tape shielding layer. The pressure-resistant aeronautic current lead is good in bending resistance, good in heat radiation effect and resistant to high temperature, acid, alkali and low temperature, and further has the advantages of being high in oxidation resistance and pressure resistance.

Description

A kind of withstand voltage aviation drainage electric wire
Technical field
The invention belongs to electric wire field, relate in particular to a kind of withstand voltage aviation drainage electric wire.
Background technology
At present, along with Chinese society expanding economy, electric wire electric wire consumption increases rapidly, the quality requirement of electric wire is also constantly improved, such as the electric wire using in the fields such as aviation boats and ships, to the high and low temperature resistance of electric wire, the resistance to pull resistance of resistance to compression, acid and alkali-resistance, cold-resistant high temperature resistant and non-oxidizability aspect, require all high especially.
Summary of the invention
In order to overcome the defect of above-mentioned prior art, the object of this invention is to provide a kind of high temperature resistant, cold-resistant, the withstand voltage aviation drainage electric wire that resistance to compression pull resistance is strong.
The present invention takes following technical scheme to realize: a kind of withstand voltage aviation drainage electric wire, it is by controlling core, chlorosulfonated polyethylene sheath layer, tin-coated copper strip screen, teflon insulation layer and aluminium strip armouring pe sheath layer form, it is inner that described control core is extruded in chlorosulfonated polyethylene sheath layer, be provided with three groups, described control core is by the layer of polyester fiber as intermediate layer, four groups of zinc-plated nickel conductor cable cores that are wrapped in the ethylene propylene rubber insulated layer outside layer of polyester fiber and are extruded within ethylene propylene rubber insulated layer form, outside described chlorosulfonated polyethylene sheath layer, wrap up one deck tin-coated copper strip screen, between described chlorosulfonated polyethylene sheath layer and tin-coated copper strip screen, be extruded with three zinc-plated aluminium wire drainage threads.
The present invention has following beneficial effect in sum: this kind of electric wire resistance to bend(ing) is strong, and good heat dissipation effect is high temperature resistant, and acid and alkali-resistance is cold-resistant, also has non-oxidizability strong, the advantage that the resistance to pull resistance of resistance to compression is strong simultaneously.
Accompanying drawing explanation
Fig. 1 is cross-sectional structure schematic diagram of the present invention;
Wherein: 1, control core; 11, layer of polyester fiber; 12, ethylene propylene rubber insulated layer; 13, zinc-plated nickel conductor cable core; 2, chlorosulfonated polyethylene sheath layer; 3, tin-coated copper strip screen; 4, teflon insulation layer; 5, aluminium strip armouring pe sheath layer; 6, zinc-plated aluminium wire drainage thread.
Embodiment
As shown in Figure 1, a kind of withstand voltage aviation drainage electric wire, it is by controlling core 1, chlorosulfonated polyethylene sheath layer 2, tin-coated copper strip screen 3, teflon insulation layer 4 and aluminium strip armouring pe sheath layer 5 form, described control core 1 is extruded in chlorosulfonated polyethylene sheath layer 2 inside, be provided with three groups, described control core 1 is by the layer of polyester fiber 11 as intermediate layer, four groups of zinc-plated nickel conductor cable cores 13 that are wrapped in the ethylene propylene rubber insulated layer 12 outside layer of polyester fiber 11 and are extruded within ethylene propylene rubber insulated layer 12 form, outside described chlorosulfonated polyethylene sheath layer 2, wrap up one deck tin-coated copper strip screen 3, between described chlorosulfonated polyethylene sheath layer 2 and tin-coated copper strip screen 3, be extruded with three zinc-plated aluminium wire drainage threads 6.
The above is the embodiment of the present invention, and the equivalence of doing according to structure, feature and principle described in the present patent application scope therefore all changes or modifies, and is included in patent claim of the present invention.

Claims (1)

1. a withstand voltage aviation drainage electric wire, it is by controlling core, chlorosulfonated polyethylene sheath layer, tin-coated copper strip screen, teflon insulation layer and aluminium strip armouring pe sheath layer form, it is characterized in that: it is inner that described control core is extruded in chlorosulfonated polyethylene sheath layer, be provided with three groups, described control core is by the layer of polyester fiber as intermediate layer, four groups of zinc-plated nickel conductor cable cores that are wrapped in the ethylene propylene rubber insulated layer outside layer of polyester fiber and are extruded within ethylene propylene rubber insulated layer form, outside described chlorosulfonated polyethylene sheath layer, wrap up one deck tin-coated copper strip screen, between described chlorosulfonated polyethylene sheath layer and tin-coated copper strip screen, be extruded with three zinc-plated aluminium wire drainage threads.
CN201410114490.8A 2014-03-26 2014-03-26 Pressure-resistant aeronautic current lead Pending CN103943243A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410114490.8A CN103943243A (en) 2014-03-26 2014-03-26 Pressure-resistant aeronautic current lead

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410114490.8A CN103943243A (en) 2014-03-26 2014-03-26 Pressure-resistant aeronautic current lead

Publications (1)

Publication Number Publication Date
CN103943243A true CN103943243A (en) 2014-07-23

Family

ID=51190868

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410114490.8A Pending CN103943243A (en) 2014-03-26 2014-03-26 Pressure-resistant aeronautic current lead

Country Status (1)

Country Link
CN (1) CN103943243A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104319007A (en) * 2014-10-21 2015-01-28 安徽环宇电缆集团有限公司 Tensile temperature-resistant multi-core-pair shield cable for computer
CN104616767A (en) * 2015-01-30 2015-05-13 安徽万博电缆材料有限公司 Copper-plastic nickel strip armor ethylene-propylene sheath motor leading cable
CN104715831A (en) * 2015-02-27 2015-06-17 安徽华峰电缆集团有限公司 Antifreeze sheathing and shielding cable for aerospace use

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120000690A1 (en) * 2010-07-01 2012-01-05 General Cable Technologies Corporation Data cable with free stripping water blocking material
CN202275631U (en) * 2011-10-18 2012-06-13 安徽新宇缆业集团有限公司 Heatproof splash-resistant flexible cable
CN202549385U (en) * 2012-03-20 2012-11-21 安徽恒晶电缆集团有限公司 Three-core type control cable for ship
CN102810355A (en) * 2011-05-30 2012-12-05 扬州因特吉实业有限公司 Festoon flexible cable for automatic port loading and unloading machinery
CN202632825U (en) * 2012-06-05 2012-12-26 扬州华瑞电缆有限公司 Lightning-preventing special measurement and control cable
CN103021549A (en) * 2012-11-29 2013-04-03 安徽徽宁电器仪表集团有限公司 Water-proof anti-corrosion electric power flexible cable
CN203787171U (en) * 2014-03-26 2014-08-20 无为县金华电缆材料有限公司 Pressure-tolerant drainage electric wire for aviation

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120000690A1 (en) * 2010-07-01 2012-01-05 General Cable Technologies Corporation Data cable with free stripping water blocking material
CN102810355A (en) * 2011-05-30 2012-12-05 扬州因特吉实业有限公司 Festoon flexible cable for automatic port loading and unloading machinery
CN202275631U (en) * 2011-10-18 2012-06-13 安徽新宇缆业集团有限公司 Heatproof splash-resistant flexible cable
CN202549385U (en) * 2012-03-20 2012-11-21 安徽恒晶电缆集团有限公司 Three-core type control cable for ship
CN202632825U (en) * 2012-06-05 2012-12-26 扬州华瑞电缆有限公司 Lightning-preventing special measurement and control cable
CN103021549A (en) * 2012-11-29 2013-04-03 安徽徽宁电器仪表集团有限公司 Water-proof anti-corrosion electric power flexible cable
CN203787171U (en) * 2014-03-26 2014-08-20 无为县金华电缆材料有限公司 Pressure-tolerant drainage electric wire for aviation

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104319007A (en) * 2014-10-21 2015-01-28 安徽环宇电缆集团有限公司 Tensile temperature-resistant multi-core-pair shield cable for computer
CN104616767A (en) * 2015-01-30 2015-05-13 安徽万博电缆材料有限公司 Copper-plastic nickel strip armor ethylene-propylene sheath motor leading cable
CN104715831A (en) * 2015-02-27 2015-06-17 安徽华峰电缆集团有限公司 Antifreeze sheathing and shielding cable for aerospace use

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WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20140723

WD01 Invention patent application deemed withdrawn after publication