CN103886937A - Insulating and armored current guiding cable for aviation - Google Patents

Insulating and armored current guiding cable for aviation Download PDF

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Publication number
CN103886937A
CN103886937A CN201410071163.9A CN201410071163A CN103886937A CN 103886937 A CN103886937 A CN 103886937A CN 201410071163 A CN201410071163 A CN 201410071163A CN 103886937 A CN103886937 A CN 103886937A
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CN
China
Prior art keywords
nickel
core
conductor
polyvinyl chloride
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.)
Pending
Application number
CN201410071163.9A
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Chinese (zh)
Inventor
叶骥
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 HONGQI CABLE GROUP Co Ltd
Original Assignee
ANHUI HONGQI 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 HONGQI CABLE GROUP Co Ltd filed Critical ANHUI HONGQI CABLE GROUP Co Ltd
Priority to CN201410071163.9A priority Critical patent/CN103886937A/en
Publication of CN103886937A publication Critical patent/CN103886937A/en
Pending legal-status Critical Current

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Abstract

The invention discloses an insulating and armored current guiding cable for aviation. The insulating and armored current guiding cable for the aviation is composed of aluminium conductor cable cores, a nickel conductor cable core, a copper conductor cable core, a polyvinyl chloride insulating layer, a nickel strap armor layer, a chloroprene rubber sheath layer and a tin-coated steel strap armor layer. The aluminium conductor cable cores, the nickel conductor cable core and the copper conductor cable core are all arranged in the polyvinyl chloride insulating layer in a pressing wrapping mode, the nickel strap armor layer wraps the outer side of the polyvinyl chloride insulating layer, the chloroprene rubber sheath layer wraps the outer side of the nickel strap armor layer, and the two sets of the aluminium conductor cable cores are arranged. The cable is light, convenient to convey, resistant to bending, good in insulating effect, excellent in anti-seismic property, strong in airtightness and good in conductivity.

Description

A kind of aviation is with insulating and armouring leading cable
Technical field
The invention belongs to field of cables, relate in particular to insulation and armouring leading cable for a kind of aviation.
Background technology
Along with expanding economy, electric wire consumption increases rapidly, change also increasing, but also more and more can not meet the demand of social every field, boats and ships, aviation, power plant, metallurgy and field of petrochemical industry be extensive use cable all, now, there is a kind of cable, be the cable that is specifically applied to boats and ships, be also optionally used in some other field, fully met demand.
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 lightweightly, insulation effect is good, and anti-seismic performance, air-tightness are strong, insulation and armouring leading cable for aviation that electric conductivity is excellent.
The present invention is insulation and the armouring leading cable for a kind of aviation of taking following technical scheme to realize, and it is made up of aluminium conductor core, nickel conductor thread core, copper conductor core, polyvinyl chloride insulation layer, nickel strap armour, chloroprene rubber sheath layer and zinc-plated steel band armour.Described aluminium conductor core, nickel conductor thread core and copper conductor core are all extruded in polyvinyl chloride insulation layer inside, outside described polyvinyl chloride insulation layer, wrap up one deck nickel strap armour, outside described nickel strap armour, wrap up one deck chloroprene rubber sheath layer, described aluminium conductor core is set to two groups, described nickel conductor thread core by nickel conductor, be wrapped in the butyronitrile insulating barrier outside nickel conductor and the nickel strap armour that is wrapped in outside butyronitrile insulating barrier forms.
Described polyvinyl chloride insulation layer inside is also extruded with a tinned copper wire drainage thread.
The present invention has following beneficial effect in sum: this kind of cable is lightweight, convenient transport, and resistance to bending, insulation effect is good, also has superior anti-seismic performance, air-tightness is strong, the feature that electric conductivity is excellent.
Brief description of the drawings
Fig. 1 is cross-sectional structure schematic diagram of the present invention;
Wherein: 1, aluminium conductor core; 2, nickel conductor thread core; 3, copper conductor core; 4, polyvinyl chloride insulation layer; 5, nickel strap armour; 6, chloroprene rubber sheath layer; 7, zinc-plated steel band armour; 8, tinned copper wire drainage thread.
Embodiment
As shown in Figure 1, insulation and armouring leading cable for a kind of aviation, it is made up of aluminium conductor core 1, nickel conductor thread core 2, copper conductor core 3, polyvinyl chloride insulation layer 4, nickel strap armour 5, chloroprene rubber sheath layer 6 and zinc-plated steel band armour 7.Described aluminium conductor core 1, nickel conductor thread core 2 and copper conductor core 3 are all extruded in polyvinyl chloride insulation layer 4 inside, outside described polyvinyl chloride insulation layer 4, wrap up one deck nickel strap armour 5, outside described nickel strap armour 5, wrap up one deck chloroprene rubber sheath layer 6, described aluminium conductor core 1 is set to two groups, described nickel conductor thread core 2 by nickel conductor, be wrapped in the butyronitrile insulating barrier outside nickel conductor and the nickel strap armour that is wrapped in outside butyronitrile insulating barrier forms.
Described polyvinyl chloride insulation layer 4 inside are also extruded with a tinned copper wire drainage thread 8.
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 (2)

1. an aviation is with insulating and armouring leading cable, it is by aluminium conductor core, nickel conductor thread core, copper conductor core, polyvinyl chloride insulation layer, nickel strap armour, chloroprene rubber sheath layer and zinc-plated steel band armour composition, it is characterized in that: described aluminium conductor core, nickel conductor thread core and copper conductor core are all extruded in polyvinyl chloride insulation layer inside, outside described polyvinyl chloride insulation layer, wrap up one deck nickel strap armour, outside described nickel strap armour, wrap up one deck chloroprene rubber sheath layer, described aluminium conductor core is set to two groups, described nickel conductor thread core is by nickel conductor, be wrapped in the butyronitrile insulating barrier outside nickel conductor and be wrapped in the nickel strap armour composition outside butyronitrile insulating barrier.
2. insulation and armouring leading cable for aviation according to claim 1, is characterized in that: described polyvinyl chloride insulation layer inside is also extruded with a tinned copper wire drainage thread.
CN201410071163.9A 2014-03-01 2014-03-01 Insulating and armored current guiding cable for aviation Pending CN103886937A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410071163.9A CN103886937A (en) 2014-03-01 2014-03-01 Insulating and armored current guiding cable for aviation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410071163.9A CN103886937A (en) 2014-03-01 2014-03-01 Insulating and armored current guiding cable for aviation

Publications (1)

Publication Number Publication Date
CN103886937A true CN103886937A (en) 2014-06-25

Family

ID=50955788

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410071163.9A Pending CN103886937A (en) 2014-03-01 2014-03-01 Insulating and armored current guiding cable for aviation

Country Status (1)

Country Link
CN (1) CN103886937A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007045345A1 (en) * 2005-10-21 2007-04-26 Helu Kabel Gmbh Three-core cable
CN201758027U (en) * 2010-08-30 2011-03-09 扬州恒辉电缆有限公司 Impact-resistant lighteningproof special shielding cable
CN103310888A (en) * 2013-06-25 2013-09-18 江苏红峰电缆集团有限公司 Crosslinked polyethylene insulated power cable
CN103500611A (en) * 2013-08-26 2014-01-08 无锡市恒汇电缆有限公司 High-tensile-strength signal transmission drum cable
CN103578644A (en) * 2012-07-27 2014-02-12 上海上力电线电缆有限公司 Mining communication cable
CN203746448U (en) * 2014-03-01 2014-07-30 安徽红旗电缆集团有限公司 Aviation-used insulated and armored lead cable

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007045345A1 (en) * 2005-10-21 2007-04-26 Helu Kabel Gmbh Three-core cable
CN201758027U (en) * 2010-08-30 2011-03-09 扬州恒辉电缆有限公司 Impact-resistant lighteningproof special shielding cable
CN103578644A (en) * 2012-07-27 2014-02-12 上海上力电线电缆有限公司 Mining communication cable
CN103310888A (en) * 2013-06-25 2013-09-18 江苏红峰电缆集团有限公司 Crosslinked polyethylene insulated power cable
CN103500611A (en) * 2013-08-26 2014-01-08 无锡市恒汇电缆有限公司 High-tensile-strength signal transmission drum cable
CN203746448U (en) * 2014-03-01 2014-07-30 安徽红旗电缆集团有限公司 Aviation-used insulated and armored lead cable

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C06 Publication
PB01 Publication
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WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20140625

WD01 Invention patent application deemed withdrawn after publication