CN104867581A - Aviation control cable with aluminum current-guiding wire - Google Patents

Aviation control cable with aluminum current-guiding wire Download PDF

Info

Publication number
CN104867581A
CN104867581A CN201410066263.2A CN201410066263A CN104867581A CN 104867581 A CN104867581 A CN 104867581A CN 201410066263 A CN201410066263 A CN 201410066263A CN 104867581 A CN104867581 A CN 104867581A
Authority
CN
China
Prior art keywords
layer
aluminum
cable
aluminium
butyronitrile insulating
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
CN201410066263.2A
Other languages
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 CN201410066263.2A priority Critical patent/CN104867581A/en
Publication of CN104867581A publication Critical patent/CN104867581A/en
Pending legal-status Critical Current

Links

Landscapes

  • Insulated Conductors (AREA)

Abstract

The invention discloses an aviation control cable with an aluminum current-guiding wire. The aviation control cable with the aluminum current-guiding wire is composed of aluminum alloy conductors, an aluminum belt shielding layer, a nickel belt armored layer, a butyronitrile insulating layer, a low-smoke halogen-free polyolefin sheath layer and a crosslinked polyethylene sheath layer. The aluminum alloy conductors form seven groups of cable cores, each group of cable cores comprises two of the aluminum alloy conductors, the seven groups of cable cores are twisted together and extruded with the aluminum belt shielding layer, the aluminum belt shielding layer is wrapped with the nickel belt armored layer, the nickel belt armored layer is wrapped with the butyronitrile insulating layer, and the butyronitrile insulating layer is wrapped with the low-smoke halogen-free polyolefin sheath layer. The aviation control cable with the aluminum current-guiding wire has the advantages of good shielding and insulating performance, good bending resistance, high conductivity, high temperature resistance, and high magnetic interference resistance.

Description

A kind of aviation control cincture aluminium drainage thread cable
Technical field
The present invention relates to field of cables, particularly relate to a kind of aviation control cincture aluminium drainage thread cable.
Background technology
At present, at present, along with socioeconomic development, electric wire consumption increases rapidly, the quality requirement of cable is also constantly improved, such as in aviation, electric power, the cable used in the fields such as boats and ships, to shielding insulation performance, the resist bending performance of cable, conductance, high temperature resistant, the requirement of diamagnetic interference aspect of performance is high all especially.If the incomplete words that cable possesses, the work in these fields and benefit can be affected.
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, insulation shielding is effective, and diamagnetic interference is strong, resist bending aviation control cincture of good performance aluminium drainage thread cable.
The present invention takes following technical scheme to realize: a kind of aviation control cincture aluminium drainage thread cable, it is by aluminium alloy conductor, aluminium strip screen, nickel strap armour, butyronitrile insulating barrier, low-smoke halogen-free polyolefin restrictive coating and crosslinked polyethylene restrictive coating composition, described aluminium alloy conductor between two one group form one group of cable core, be seven groups altogether, one deck aluminium strip screen is extruded with outside seven groups of cable cores twist together, outer wrapping one deck nickel strap armour of described aluminium strip screen, outer wrapping one deck butyronitrile insulating barrier of described nickel strap armour, outer wrapping one deck low-smoke halogen-free polyolefin restrictive coating of described butyronitrile insulating barrier, an aluminium wire drainage thread is extruded with between described nickel strap armour and butyronitrile insulating barrier, described aluminium strip screen inside extrudes an aluminum metal flexible pipe.
The present invention has following beneficial effect in sum: this cable has good shielding insulation performance, resist bending performance, and conductance is high, also has high temperature resistant, the feature that diamagnetic interference is strong simultaneously.
Accompanying drawing explanation
Fig. 1 is cross-sectional structure schematic diagram of the present invention;
Wherein: 1, aluminium alloy conductor; 2, aluminium strip screen; 3, nickel strap armour; 4, butyronitrile insulating barrier; 5, low-smoke halogen-free polyolefin restrictive coating; 6, crosslinked polyethylene restrictive coating; 7, aluminium wire drainage thread; 8, aluminum metal flexible pipe.
Embodiment
As shown in Figure 1, a kind of aviation control cincture aluminium drainage thread cable, it is by aluminium alloy conductor 1, aluminium strip screen 2, nickel strap armour 3, butyronitrile insulating barrier 4, low-smoke halogen-free polyolefin restrictive coating 5 and crosslinked polyethylene restrictive coating 6 form, described aluminium alloy conductor 1 between two one group form one group of cable core, be seven groups altogether, one deck aluminium strip screen 2 is extruded with outside seven groups of cable cores twist together, outer wrapping one deck nickel strap armour 3 of described aluminium strip screen 2, outer wrapping one deck butyronitrile insulating barrier 4 of described nickel strap armour 3, outer wrapping one deck low-smoke halogen-free polyolefin restrictive coating 5 of described butyronitrile insulating barrier 4, an aluminium wire drainage thread 7 is extruded with between described nickel strap armour 3 and butyronitrile insulating barrier 4, described aluminium strip screen 2 inside extrudes an aluminum metal flexible pipe 8.
The above is the embodiment of the present invention, therefore all equivalences done according to structure, feature and the principle described in the present patent application scope change or modify, and are included in patent claim of the present invention.

Claims (1)

1. an aviation control cincture aluminium drainage thread cable, it is by aluminium alloy conductor, aluminium strip screen, nickel strap armour, butyronitrile insulating barrier, low-smoke halogen-free polyolefin restrictive coating and crosslinked polyethylene restrictive coating composition, it is characterized in that: described aluminium alloy conductor between two one group form one group of cable core, be seven groups altogether, one deck aluminium strip screen is extruded with outside seven groups of cable cores twist together, outer wrapping one deck nickel strap armour of described aluminium strip screen, outer wrapping one deck butyronitrile insulating barrier of described nickel strap armour, outer wrapping one deck low-smoke halogen-free polyolefin restrictive coating of described butyronitrile insulating barrier, an aluminium wire drainage thread is extruded with between described nickel strap armour and butyronitrile insulating barrier, described aluminium strip screen inside extrudes an aluminum metal flexible pipe.
CN201410066263.2A 2014-02-26 2014-02-26 Aviation control cable with aluminum current-guiding wire Pending CN104867581A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410066263.2A CN104867581A (en) 2014-02-26 2014-02-26 Aviation control cable with aluminum current-guiding wire

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410066263.2A CN104867581A (en) 2014-02-26 2014-02-26 Aviation control cable with aluminum current-guiding wire

Publications (1)

Publication Number Publication Date
CN104867581A true CN104867581A (en) 2015-08-26

Family

ID=53913360

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410066263.2A Pending CN104867581A (en) 2014-02-26 2014-02-26 Aviation control cable with aluminum current-guiding wire

Country Status (1)

Country Link
CN (1) CN104867581A (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008275075A (en) * 2007-04-27 2008-11-13 Toyota Motor Corp Gas supply system
CN201402653Y (en) * 2009-05-04 2010-02-10 江苏亨通电力电缆有限公司 Offshore oil platform non-halogen low-smoke flame-retardant oil-resistant meter cable
CN202930116U (en) * 2012-11-06 2013-05-08 安徽南洋电缆有限公司 Aluminium alloy conductor soft power cable

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008275075A (en) * 2007-04-27 2008-11-13 Toyota Motor Corp Gas supply system
CN201402653Y (en) * 2009-05-04 2010-02-10 江苏亨通电力电缆有限公司 Offshore oil platform non-halogen low-smoke flame-retardant oil-resistant meter cable
CN202930116U (en) * 2012-11-06 2013-05-08 安徽南洋电缆有限公司 Aluminium alloy conductor soft power cable

Similar Documents

Publication Publication Date Title
CN103871609A (en) Perfluorinated-ethylene insulating protecting-cover wire
CN103871581A (en) Waterproof insulating armoring wire for tunnels
CN203760141U (en) Drainage wire-contained armoured insulated cable
CN203721223U (en) Ship control shielding and armored cable
CN203746504U (en) Electromagnetic-interference-preventing cold-resistant and anti-freezing cable
CN204480742U (en) A kind of high temperature resistant compensating cable
CN103928118A (en) Electromagnetic-interference-resistant, cold-resistant and antifreeze cable
CN203562227U (en) A metallurgy high-temperature-resistant power cable
CN203491014U (en) Aluminium-alloy conductor power cable
CN103915205A (en) Rated voltage traction cable
CN203721280U (en) Cross-linked polyethylene sheathed cable
CN104867581A (en) Aviation control cable with aluminum current-guiding wire
CN203746495U (en) Armor shielding flexible wire for tunnel and square
CN203760140U (en) Anti-drawing wire-contained armoured low-smoke halogen-free sheath cable
CN203552772U (en) Power cable with ethylene propylene rubber (EPR) insulating layer and armored sheath
CN103928163A (en) Metallurgical high-temperature-resistant power cable
CN103928117A (en) Cable resisting electromagnetic interference, acid and base
CN104867602A (en) Marine shielded-armored cable with current-guiding wire
CN103886938A (en) Ship control shielding and armored cable
CN104867600A (en) Ship control current guiding cable
CN104733100A (en) Low-smoke zero-halogen shielded cable
CN103915157A (en) Armor insulation cable with drainage wires
CN104867580A (en) Marine shielded-insulated cable with current-guiding wire
CN104867544A (en) Shielding, armored, insulating and current-guiding cable for ships
CN104867550A (en) Marine shielded-armored cable with metal hose

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20150826