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CN103854783A - Lac cable for airplane lamp illumination - Google Patents

Lac cable for airplane lamp illumination Download PDF

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Publication number
CN103854783A
CN103854783A CN201310391574.1A CN201310391574A CN103854783A CN 103854783 A CN103854783 A CN 103854783A CN 201310391574 A CN201310391574 A CN 201310391574A CN 103854783 A CN103854783 A CN 103854783A
Authority
CN
China
Prior art keywords
cable
layer
lac
fire
wrapped
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
CN201310391574.1A
Other languages
Chinese (zh)
Inventor
樊玉广
陈龙
朱静波
朱彤
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 HUALING CABLE GROUP Co Ltd
Original Assignee
ANHUI HUALING 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 HUALING CABLE GROUP Co Ltd filed Critical ANHUI HUALING CABLE GROUP Co Ltd
Priority to CN201310391574.1A priority Critical patent/CN103854783A/en
Publication of CN103854783A publication Critical patent/CN103854783A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a Lac cable for airplane lamp illumination. The Lac cable mainly comprises three sets of cable cores, an insulating layer, a wire armoring layer and an outer sheath layer. The three sets of the cable cores are arranged in the insulating layer in an extruding mode. Each cable core is composed of an aluminum conductor, an insulation shielding layer, a fire-proof layer and an inner sheath. The insulation shielding layers wrap the aluminum conductors. The fire-proof layers wrap the insulation shielding layers. The inner sheaths wrap the fire-proof layers. The wire armoring layers wrap the insulating layer. The Lac cable is wide in use and long in service life, has the advantages of being excellent in resistance to heat, fire, weather, water, gasoline, engine oil and strong acid-base solution, and also has the advantages of being resistant to tearing, aging and wear and protecting the environment.

Description

A kind of aircraft lamp lighting lac cable
Technical field
The present invention relates to field of cables, relate in particular to a kind of aircraft lamp lighting lac cable.
Background technology
Along with the development of aviation industry, the continuous increase of the world and domestic airport, the construction of subway, track traffic, the development of national shipbuilding industry, also more and more higher to the requirement of electric wire, the especially conductivity of electric wire and fire-resistant requirement.The purposes of the special lac cable of aircraft is extremely extensive: be mainly used in Mobile illumination equipment, the aircraft low-voltage circuit of aircraft, airport, subway, track traffic, boats and ships etc., freeway surveillance and control device line is installed with, highway, line, road High-Pole Lamp line for electronic police.
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 aircraft lamp lighting lac cable with resistance to gasoline, resistance to machine oil and strong acid-base resistance solution property.
The present invention takes following technical scheme to realize: a kind of aircraft lamp lighting lac cable, it mainly comprises three groups of cable cores, insulating barrier, wire armoring layer and external sheath layer, in described insulating barrier, be extruded with three groups of cable cores, every group of cable core is all made up of aluminium conductor, insulation screen, flame retardant coating and inner sheath, described aluminium conductor is wrapped with insulation screen, described insulation screen is wrapped with flame retardant coating, described flame retardant coating is wrapped with described inner sheath, and described insulating barrier is wrapped with described wire armoring layer.
In described flame retardant coating, be provided with aluminium alloy tension silk.
Described inner sheath is polyurethane inner sheath.
Described external sheath layer is glass fiber braiding lacquer coating.
The present invention has following beneficial effect in sum: the present invention is of many uses, long service life, also there is heat-resisting, fire-resistant, weather row, water-fast excellence, resistance to gasoline, machine oil, strong acid-base solution property, also there is the features such as tear-proof, ageing-resistant, wear-resisting, environmental protection.
Accompanying drawing explanation
Fig. 1 is cross-sectional structure schematic diagram of the present invention;
Wherein: 1, aluminium conductor; 2, insulation screen; 3, flame retardant coating; 4, inner sheath; 5, insulating barrier; 6, wire armoring layer; 7, external sheath layer; 8, aluminium alloy tension silk.
Embodiment
As shown in Figure 1, a kind of aircraft lamp lighting lac cable, it mainly comprises three groups of cable cores, insulating barrier 5, wire armoring layer 6 and external sheath layer 7, in described insulating barrier 5, be extruded with three groups of cable cores, every group of cable core is all made up of aluminium conductor 1, insulation screen 2, flame retardant coating 3 and inner sheath 4, and aluminium conductor 1 is wrapped with insulation screen 2, and insulation screen 2 is wrapped with flame retardant coating 3, flame retardant coating 3 is wrapped with described inner sheath 4, and insulating barrier 5 is wrapped with wire armoring layer 6.
Embodiment: be provided with aluminium alloy tension silk 8 in flame retardant coating 4.
Inner sheath 4 is polyurethane inner sheath.
External sheath layer 7 is glass fiber braiding lacquer coating.
The above is embodiments of the 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 (4)

1. an aircraft lamp lighting lac cable, it mainly comprises three groups of cable cores, insulating barrier, wire armoring layer and external sheath layer, it is characterized in that: in described insulating barrier, be extruded with three groups of cable cores, every group of cable core is all made up of aluminium conductor, insulation screen, flame retardant coating and inner sheath, described aluminium conductor is wrapped with insulation screen, described insulation screen is wrapped with flame retardant coating, and described flame retardant coating is wrapped with described inner sheath, and described insulating barrier is wrapped with described wire armoring layer.
2. aircraft lamp lighting lac cable according to claim 1, is characterized in that: in described flame retardant coating, be provided with aluminium alloy tension silk.
3. aircraft lamp lighting lac cable according to claim 1, is characterized in that: described inner sheath is polyurethane inner sheath.
4. aircraft lamp lighting lac cable according to claim 1, is characterized in that: described external sheath layer is glass fiber braiding lacquer coating.
CN201310391574.1A 2013-09-02 2013-09-02 Lac cable for airplane lamp illumination Pending CN103854783A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310391574.1A CN103854783A (en) 2013-09-02 2013-09-02 Lac cable for airplane lamp illumination

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310391574.1A CN103854783A (en) 2013-09-02 2013-09-02 Lac cable for airplane lamp illumination

Publications (1)

Publication Number Publication Date
CN103854783A true CN103854783A (en) 2014-06-11

Family

ID=50862328

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310391574.1A Pending CN103854783A (en) 2013-09-02 2013-09-02 Lac cable for airplane lamp illumination

Country Status (1)

Country Link
CN (1) CN103854783A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109599207A (en) * 2018-10-10 2019-04-09 江苏泰祥电线电缆有限公司 A kind of novel fire-resistant cable for ship

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB998633A (en) * 1963-07-19 1965-07-21 Ass Elect Ind Flexible electric cable for aircraft
CN201984891U (en) * 2011-03-25 2011-09-21 江苏天地龙电缆有限公司 Quakeproof power cable
JP2011228122A (en) * 2010-04-20 2011-11-10 Furukawa Electric Co Ltd:The Cable for ship
CN202549434U (en) * 2012-03-20 2012-11-21 安徽恒晶电缆集团有限公司 Airplane Lac cable
CN203490994U (en) * 2013-09-02 2014-03-19 安徽华菱电缆集团有限公司 Lacquered wire for airplane lamp illumination

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB998633A (en) * 1963-07-19 1965-07-21 Ass Elect Ind Flexible electric cable for aircraft
JP2011228122A (en) * 2010-04-20 2011-11-10 Furukawa Electric Co Ltd:The Cable for ship
CN201984891U (en) * 2011-03-25 2011-09-21 江苏天地龙电缆有限公司 Quakeproof power cable
CN202549434U (en) * 2012-03-20 2012-11-21 安徽恒晶电缆集团有限公司 Airplane Lac cable
CN203490994U (en) * 2013-09-02 2014-03-19 安徽华菱电缆集团有限公司 Lacquered wire for airplane lamp illumination

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109599207A (en) * 2018-10-10 2019-04-09 江苏泰祥电线电缆有限公司 A kind of novel fire-resistant cable for ship

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Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20140611