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CN203706703U - Cable for transmitting electricity to airplane - Google Patents

Cable for transmitting electricity to airplane Download PDF

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Publication number
CN203706703U
CN203706703U CN201320859405.1U CN201320859405U CN203706703U CN 203706703 U CN203706703 U CN 203706703U CN 201320859405 U CN201320859405 U CN 201320859405U CN 203706703 U CN203706703 U CN 203706703U
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CN
China
Prior art keywords
phase
core
cores
cable
cable core
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.)
Withdrawn - After Issue
Application number
CN201320859405.1U
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Chinese (zh)
Inventor
宋明明
刘永红
刘春昉
邓春艳
刘惠华
黄佳
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.)
TEBIAN ELECTRICAL APPARATUS DEYANG CABLE CO Ltd
Original Assignee
TEBIAN ELECTRICAL APPARATUS DEYANG CABLE 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 TEBIAN ELECTRICAL APPARATUS DEYANG CABLE CO Ltd filed Critical TEBIAN ELECTRICAL APPARATUS DEYANG CABLE CO Ltd
Priority to CN201320859405.1U priority Critical patent/CN203706703U/en
Application granted granted Critical
Publication of CN203706703U publication Critical patent/CN203706703U/en
Anticipated expiration legal-status Critical
Withdrawn - After Issue legal-status Critical Current

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Abstract

The utility model discloses a cable for transmitting electricity to an airplane. The cable comprises a cable core, a polyester wire mesh belt wrapping reinforced layer, an inner sheath layer, an aramid wire mesh weaving reinforced layer and an outer sheath layer, the polyester wire mesh belt wrapping reinforced layer. The inner sheath layer, the aramid wire mesh weaving reinforced layer and the outer sheath layer are sequentially wrapped at the periphery of the cable core from inside to outside. The cable core includes a three-phase power cable core and six groups of control cable cores. The three-phase power cable core is totally provided with seven insulated wire cores, wherein one wire core is neutral and is arranged at the center, and the rest six wire cores are phase wire cores and are circumferentially and uniformly arranged at the periphery of the neutral wire core. The six phase wire cores are divided into an A phase, a B phase and a C phase. Each phase includes two wire cores, and the six phase wire cores are arranged at intervals according to the sequence of the A phase, the B phase and the C phase. A 180-degree included angle is formed between the two wire cores of each phase respectively. The control cable cores are arranged at the peripheries of the phase wire cores. The control cable cores and the power cable core are concentrically arranged. The six groups of control cable cores are arranged corresponding to six adjacent positions formed by the six phase wire cores respectively. The cable is specially used for transmitting electric energy to the airplane by airport ground service and transmitting detection signals.

Description

A kind of to aircraft transmission of electricity cable
Technical field
The utility model relates to cable, is specially one to aircraft transmission of electricity cable, is exclusively used in airport ground service to aircraft transmission of electric energy and transmission detection signal.
Background technology
Aircraft needs often to arrive ground electric energy supplement, and when behind aircraft landing airplane parking area, airport ground workers transmit electricity to aircraft with cable.Due to aircraft utilization be the intermediate frequency three phase mains of voltage 115/200V, frequency 400Hz, and transmission of electricity process also need monitoring, therefore cable is had to specific (special) requirements, mainly:
1, energy transmission of electric energy and detection control signal simultaneously;
2, the voltage of three phase mains, electric current, electric capacity, impedance (induction reactance, capacitive reactance) must keep balance;
3, the voltage drop of course of conveying must not be greater than 2V;
4, because cable will pull on ground, there are enough tensile strength and resistance to wear;
5, owing to wanting rolling after cable power transmission on reel, must there is good flexibility;
6, because cable is that environment uses, need there is heat-resisting, cold-resistant, anti-ultraviolet property in the open;
7, fire safety grade in airport is very high, and cable need possess anti-flammability, oil resistant, low cigarette.
8, because cable is wanted often to contact with personnel, need environmental protection, Halogen, nontoxicity.
The current domestic cable product appearance that meets above-mentioned requirements that there is no, have abroad the airport corollary equipment company of a GAVOTEC by name to have similar cable product, but the said firm is externally secret, cannot obtain technical information, cause China's dependence on import still so far, affect airport construction localization process.
Summary of the invention
It is a kind of to aircraft transmission of electricity cable that the utility model provides, and to accelerate China's airport construction localization process, its technical scheme is:
A kind of to aircraft transmission of electricity cable, comprise cable core and be sequentially coated on from inside to outside the wrapped reinforced layer of dacron thread guipure, inner restrictive coating, aramid fiber screen knitting reinforced layer, the external sheath layer of cable core periphery; Described cable core comprises three-phase power cable core and control cable core, and described three-phase power cable core is for carrying three-phase 400Hz intermediate frequency electric power to aircraft, and described control cable core is for transmission of control signals; Described three-phase power cable core has 7 insulated wire cores, wherein one is neutral core, is arranged in center, and all the other 6 is phase wire core, be looped around neutral core periphery, circumferentially be uniformly distributed, be arranged in concentric circles state with neutral core, 6 phase wire cores are divided into A, B, C three-phase, two of every phases, 6 phase wire cores are pressed A, B, the alternate layout of C phase sequence, and two cores of each phase are all symmetrical, at a distance of 180 o; Described control cable core is arranged in phase wire core periphery, is circumferentially uniformly distributed, and is arranged in concentric circles state with electric power cable core, totally 6 groups of this control cable cores, respectively corresponding 66 adjacent regions that phase wire core forms.
The insulated wire cores of described electric power cable core is made up of conductor and the insulating barrier that is coated on conductor periphery, and described conductor is closed with stranded technique and made by bundle by multiply annealed copper wire, forms the hierarchy of multiple concentric circles.
Described insulating barrier is made up of TPE elastomeric material.
In the insulated wire cores of described electric power cable core, there is tension rope, wherein, in phase wire core, have a tension rope, be positioned at conductor center, in neutral core, have 3 tension ropes, be positioned at the subcenter layer of conductor, be circumferentially uniformly distributed, with 3 alternate layouts of annealed copper wire of this layer.
Described tension rope is setline or high strength PE silk thread, and wherein setline is the shuffling netting twine that adopts weaving to make; High strength PE silk thread is the sub-thread PE line that is closed multiply PE silk thread that technique makes or diameter and be not less than 0.3mm by bundle.
Described 6 groups of each groups of control cable core have 4 insulated wire cores and a tension rope, and tension rope is positioned at central authorities, and 4 insulated wire cores are looped around tension rope periphery, are circumferentially uniformly distributed; Described insulated wire cores is made up of conductor and the insulating barrier that is coated on conductor periphery, described conductor is closed with stranded technique and is made by bundle by multiply annealed copper wire, described insulating barrier is made up of TPE elastomeric material, described tension rope is setline or high strength PE silk thread, and wherein setline is the shuffling netting twine that adopts weaving to make; High strength PE silk thread is the sub-thread PE line that is closed multiply PE silk thread that technique makes or diameter and be not less than 0.3mm by bundle.
Described inner restrictive coating is made by extrusion process with PUR elastomer polymer or ethylene-propylene rubber mixture.Described external sheath layer is major ingredient with PUR elastomer polymer or ethylene-propylene rubber mixture material, and luminous agent, UV absorbers, fire retardant are auxiliary material, make by extrusion process.Described luminous agent is rare earth based aluminic acid zinc salt.
The beneficial effects of the utility model:
1. the utility model has medium frequency electric line of force core and controls core, can guarantee, in for aircraft transmission of electric energy, also can transmit detection control signal, and voltage power supply frequency is 400Hz.
2. the utility model is designed to two-wire by three-phase power core dexterously, each is a pair of mutually, make various cores can be concentric circles layered arrangement, the relative position of all cores is all symmetrical, any similar core equates to the distance of round dot, and mutual inductance each other, to hold be mutually balance.
3. conductor of the present utility model is to be mixed and formed by copper cash and tension rope, and main push-towing rope core is closely surrounded with dacron thread guipure outward, and inner sheath is woven with aramid fiber silk screen outward, and whole cable tensile strength is very high, possesses the excellent anti-performance that pulls.
4. what conductor of the present utility model adopted is that thin copper single line bundle closes technique, tension rope, insulation and sheath material are organic polymer body or mixture is made, flexibility is good, the minimum bending radius that cable can reach is 4 ~ 5 times of outside diameters of cable, this outside diameter of cable 40 ± 1mm, can coil at diameter and be not less than on the reel of 200 mm, and the drum diameter that airport is used is 400 mm, can coil easily.
5. power line core conductor adopts the thin red copper wire harness of multiply to close, and its resistivity is very low, and every double structure that adopts mutually, and cross-sectional area of conductor is long-pending enough large, and the lower voltage of transmission of electricity process, in 2V, meets instructions for use.
6. in sheath material formula of the present utility model, there are luminous agent, UV absorbers, flame-retardant additive, can meet noctilucence, uvioresistant and the characteristic such as fire-retardant, wherein, luminous agent rare earth based aluminic acid zinc salt extinction on daytime, illuminating at night, when transmit electricity night, cable has visuality; Flame-retardant additive produces naked light can prevent cable fire accident time; Meet the requirement of airport security administrative provisions.UV absorbers can absorb ultraviolet light, the outdoor environment for use of appropriate cable, and insulation is difficult for aging.
7. material weatherability is good, is applicable to any airport of China, under condition at all seasons, all can use safely.
The utility model has thoroughly changed China aircraft power transmission cable and has relied on for a long time the present situation of import, has accelerated the paces of airport construction domestic manufacture of key equipment.
Accompanying drawing explanation
Fig. 1 is the structural representation of this cable.
Fig. 2 is the structural representation of this cable control cable core.
Fig. 3 is the structural representation of this cable electric power cable core.
In figure, the implication of each code name: 1-controls cable core; 2-electric power cable core phase line insulated wire cores; The neutral insulated wire cores of 3-electric power cable core; The wrapped reinforced layer of 4-dacron thread guipure, 5-inner restrictive coating, 6-aramid fiber yarn mesh grid reinforced layer, 7-external sheath layer, 8-controls cable core insulated wire cores conductor, and 9-controls cable core insulated wire cores insulating barrier, 10-controls cable core tension rope, the tension rope of 11-power cables core insulation core, the conductor of 12-power cables core insulation core, the insulating barrier of 13-power cables core insulation core.
Embodiment
Below in conjunction with accompanying drawing, this cable is further illustrated.
Referring to Fig. 1: this cable comprises cable core and is sequentially coated on from inside to outside the wrapped reinforced layer 4 of dacron thread guipure, inner restrictive coating 5, aramid fiber screen knitting reinforced layer 6, the external sheath layer 7 of cable core periphery; Described cable core comprises three-phase power cable core and control cable core 1, and described three-phase power cable core is for carrying three-phase 400Hz intermediate frequency electric power to aircraft, and described control cable core is for transmission of control signals; Described three-phase power cable core has 7 insulated wire cores, wherein one is neutral core 3, is arranged in center, and all the other 6 is phase wire core 2, be looped around the periphery of neutral core 3, circumferentially be uniformly distributed, be arranged in concentric circles state with neutral core 3,6 phase wire cores 2 are divided into A, B, C three-phase, two of every phases, 6 phase wire cores are pressed A, B, the alternate layout of C phase sequence, and two cores of each phase are all symmetrical, at a distance of 180 o; Described control cable core 1 is arranged in phase wire core periphery, is circumferentially uniformly distributed, and is arranged in concentric circles state with electric power cable core, totally 6 groups of this control cable cores, respectively corresponding 66 adjacent regions that phase cable core 2 forms.
Described inner restrictive coating 5 use PUR elastomer polymers or ethylene-propylene rubber mixture are made by extrusion process.
Described external sheath layer 7 use PUR elastomer polymers or ethylene-propylene rubber mixture material are major ingredient, and luminous agent, UV absorbers, fire retardant are auxiliary material, make by extrusion process.
Described luminous agent is rare earth based aluminic acid zinc salt.
Referring to Fig. 3: the insulated wire cores 2,3 of described electric power cable core is made up of conductor 12 and the insulating barrier 13 that is coated on conductor 12 peripheries, and described conductor 12 is closed with stranded technique and made by bundle by multiply annealed copper wire, forms the hierarchy of multiple concentric circles.Described insulating barrier 13 is made up of TPE elastomeric material.
In the insulated wire cores 2,3 of described electric power cable core, there is tension rope 11, wherein, in phase wire core 2, have a tension rope, be positioned at conductor 12 center, in neutral core 3, have 3 tension ropes, be positioned at the subcenter layer of conductor 12, circumferentially be uniformly distributed, with 3 alternate layouts of annealed copper wire of this layer.Described tension rope 11 is setline or high strength PE silk thread, and wherein setline is the shuffling netting twine that adopts weaving to make; High strength PE silk thread is the sub-thread PE line that is closed multiply PE silk thread that technique makes or diameter and be not less than 0.3mm by bundle.
Referring to Fig. 2: described 6 groups of each groups of control cable core have 4 insulated wire cores and a tension rope 10, and tension rope 10 is positioned at central authorities, and 4 insulated wire cores are looped around tension rope periphery, are circumferentially uniformly distributed; Described insulated wire cores is made up of conductor 8 and the insulating barrier 9 that is coated on conductor 8 peripheries, described conductor 8 is closed with stranded technique and is made by bundle by multiply annealed copper wire, described insulating barrier 9 is made up of TPE elastomeric material, described tension rope 10 is setline or high strength PE silk thread, and wherein setline is the shuffling netting twine that adopts weaving to make; High strength PE silk thread is the sub-thread PE line that is closed multiply PE silk thread that technique makes or diameter and be not less than 0.3mm by bundle.
The manufacture method of this cable, comprises the steps:
(1), manufacture respectively electric power cable core and control cable core:
-manufacture electric power cable core:
A. annealed copper wire and tension rope are lined up a branch ofly by close-packed arrays mode, upper stranding machine is stranded, makes twisted wire;
B. at twisted wire surface extrusion molding TPE elastomeric material insulating barrier, make an insulated wire cores; Manufacture according to this 7 insulated wire cores; Described insulating barrier is when batching additive color mother, and A, B, C three-phase and neutral insulated wire cores be respectively by red, yellow, blue, black color matching, to identify when wiring;
-production control cable core
A. annealed copper wire is lined up a branch ofly by close-packed arrays mode, upper stranding machine is stranded, makes twisted wire;
B. at twisted wire surface extrusion molding TPE elastomeric material insulating barrier, make insulated wire cores;
C. 4 insulated wire cores and 1 tension rope are lined up a branch ofly, tension rope is positioned at central authorities, and 4 insulated wire cores are looped around tension rope periphery, and upper stranding machine is stranded, makes 1 group of control cable core; Manufacture according to this 6 groups of control cable cores;
(2), 7 insulated wire cores and 6 groups of control cable cores of electric power cable core are lined up to 3 layers by arranged in concentric circles mode, wherein, layer centered by the neutral insulated wire cores of electric power cable core, 6 phase line insulated wire cores are intermediate layer, 6 groups of control cable cores are outer, and upper stranding machine is stranded, makes compound cable core;
(3), at the peripheral wrapped dacron thread guipure reinforced layer of compound cable core;
(4), at the peripheral extrusion molding PUR elastomer polymer of terylene silk net reinforced layer or ethylene-propylene rubber mixture inner restrictive coating, dacron thread guipure and extrusion molding material are bonded as one, the muscle in dacron thread guipure formation inner sheath;
(5), at the peripheral braiding of inner restrictive coating aramid fiber silk screen reinforced layer;
(6) be, major ingredient at the peripheral extrusion molding of aramid fiber silk screen reinforced layer with PUR elastomer polymer or ethylene-propylene rubber mixture material, the external sheath layer that luminous agent, UV absorbers, fire retardant are auxiliary material, aramid fiber yarn mesh grid and extrusion molding material are bonded as one, and aramid fiber yarn mesh grid forms the muscle in oversheath.
So far, this cables manufacturing comes to an end.

Claims (6)

1. to an aircraft transmission of electricity cable, it is characterized in that, comprise cable core and be sequentially coated on from inside to outside the wrapped reinforced layer of dacron thread guipure, inner restrictive coating, aramid fiber screen knitting reinforced layer, the external sheath layer of cable core periphery; Described cable core comprises three-phase power cable core and control cable core, and described three-phase power cable core is for carrying three-phase 400Hz intermediate frequency electric power to aircraft, and described control cable core is for transmission of control signals; Described three-phase power cable core has 7 insulated wire cores, wherein one is neutral core, is arranged in center, and all the other 6 is phase wire core, be looped around neutral core periphery, circumferentially be uniformly distributed, be arranged in concentric circles state with neutral core, 6 phase wire cores are divided into A, B, C three-phase, two of every phases, 6 phase wire cores are pressed A, B, the alternate layout of C phase sequence, and two cores of each phase are all symmetrical, at a distance of 180 o; Described control cable core is arranged in phase wire core periphery, is circumferentially uniformly distributed, and is arranged in concentric circles state with electric power cable core, totally 6 groups of this control cable cores, respectively corresponding 66 adjacent regions that phase wire core forms.
2. as claimed in claim 1 to aircraft transmission of electricity cable, it is characterized in that, the insulated wire cores of described electric power cable core is made up of conductor and the insulating barrier that is coated on conductor periphery, and described conductor is closed with stranded technique and made by bundle by multiply annealed copper wire, forms the hierarchy of multiple concentric circles.
3. as claimed in claim 2ly it is characterized in that to aircraft transmission of electricity cable, described insulating barrier is made up of TPE elastomeric material.
4. as claimed in claim 2 to aircraft transmission of electricity cable, it is characterized in that, in the insulated wire cores of described electric power cable core, there is tension rope, wherein, in phase wire core, there is a tension rope, be positioned at conductor center, in neutral core, there are 3 tension ropes, the subcenter layer that is positioned at conductor, is circumferentially uniformly distributed, with 3 alternate layouts of annealed copper wire of this layer.
5. as claimed in claim 4ly it is characterized in that to aircraft transmission of electricity cable, described tension rope is setline or high strength PE silk thread, and wherein setline is the shuffling netting twine that adopts weaving to make; High strength PE silk thread is the sub-thread PE line that is closed multiply PE silk thread that technique makes or diameter and be not less than 0.3mm by bundle.
6. as claimed in claim 1ly it is characterized in that to aircraft transmission of electricity cable, described 6 groups of each groups of control cable core have 4 insulated wire cores and a tension rope, and tension rope is positioned at central authorities, and 4 insulated wire cores are looped around tension rope periphery, are circumferentially uniformly distributed; Described insulated wire cores is made up of conductor and the insulating barrier that is coated on conductor periphery, described conductor is closed with stranded technique and is made by bundle by multiply annealed copper wire, described insulating barrier is made up of TPE elastomeric material, described tension rope is setline or high strength PE silk thread, and wherein setline is the shuffling netting twine that adopts weaving to make; High strength PE silk thread is the sub-thread PE line that is closed multiply PE silk thread that technique makes or diameter and be not less than 0.3mm by bundle.
CN201320859405.1U 2013-12-25 2013-12-25 Cable for transmitting electricity to airplane Withdrawn - After Issue CN203706703U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320859405.1U CN203706703U (en) 2013-12-25 2013-12-25 Cable for transmitting electricity to airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320859405.1U CN203706703U (en) 2013-12-25 2013-12-25 Cable for transmitting electricity to airplane

Publications (1)

Publication Number Publication Date
CN203706703U true CN203706703U (en) 2014-07-09

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CN201320859405.1U Withdrawn - After Issue CN203706703U (en) 2013-12-25 2013-12-25 Cable for transmitting electricity to airplane

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Country Link
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103646722A (en) * 2013-12-25 2014-03-19 特变电工(德阳)电缆股份有限公司 Cable for transmitting electricity to airplane and manufacturing method of cable
CN107148656A (en) * 2014-08-11 2017-09-08 克里斯多佛·史蒂德 cable
CN107667307A (en) * 2015-05-27 2018-02-06 普睿司曼股份公司 Aerial optical CA cable assembly
EP3279901A1 (en) * 2016-08-06 2018-02-07 CFW EMV-Consulting AG Current transmission device with at least one ac cable
EP3910650A1 (en) * 2020-05-11 2021-11-17 Lapp Engineering & Co. Shore-to-ship cable

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103646722A (en) * 2013-12-25 2014-03-19 特变电工(德阳)电缆股份有限公司 Cable for transmitting electricity to airplane and manufacturing method of cable
CN103646722B (en) * 2013-12-25 2016-08-17 特变电工(德阳)电缆股份有限公司 A kind of to aircraft transmission of electricity cable and manufacture method thereof
CN107148656A (en) * 2014-08-11 2017-09-08 克里斯多佛·史蒂德 cable
CN107148656B (en) * 2014-08-11 2019-10-01 克里斯多佛·史蒂德 Cable with a protective layer
CN107667307A (en) * 2015-05-27 2018-02-06 普睿司曼股份公司 Aerial optical CA cable assembly
CN107667307B (en) * 2015-05-27 2021-10-08 普睿司曼股份公司 Overhead Optical Cable Assemblies
EP3279901A1 (en) * 2016-08-06 2018-02-07 CFW EMV-Consulting AG Current transmission device with at least one ac cable
EP3910650A1 (en) * 2020-05-11 2021-11-17 Lapp Engineering & Co. Shore-to-ship cable

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Legal Events

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C14 Grant of patent or utility model
GR01 Patent grant
AV01 Patent right actively abandoned

Granted publication date: 20140709

Effective date of abandoning: 20160817

C25 Abandonment of patent right or utility model to avoid double patenting