CN107564615A - A kind of Aviation cable - Google Patents

A kind of Aviation cable Download PDF

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Publication number
CN107564615A
CN107564615A CN201710882334.XA CN201710882334A CN107564615A CN 107564615 A CN107564615 A CN 107564615A CN 201710882334 A CN201710882334 A CN 201710882334A CN 107564615 A CN107564615 A CN 107564615A
Authority
CN
China
Prior art keywords
layer
optical fiber
copper
cable
power line
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Withdrawn
Application number
CN201710882334.XA
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Chinese (zh)
Inventor
石存岭
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.)
Chengdu Xin Chen Aviation Technology Co Ltd
Original Assignee
Chengdu Xin Chen Aviation Technology 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 Chengdu Xin Chen Aviation Technology Co Ltd filed Critical Chengdu Xin Chen Aviation Technology Co Ltd
Priority to CN201710882334.XA priority Critical patent/CN107564615A/en
Publication of CN107564615A publication Critical patent/CN107564615A/en
Withdrawn legal-status Critical Current

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Abstract

The invention discloses a kind of Aviation cable, it is related to composite cable technical field, the present invention includes a plurality of power line, a plurality of optical fiber cable and a strengthening core, plastic-coated steel belt layer, inner insulating layer, screen layer A, flame retardant coating, damp-proof layer, armor and external insulation layer are enclosed with successively outside a plurality of power line, a plurality of optical fiber cable and a strengthening core, gap in plastic-coated steel belt layer is filled with waterproof paste, and every power line includes being disposed with copper conductor, conductor shield and crosslinked polyetylene insulated layer from inside to outside;The advantages of present invention is simple in construction, shield effectiveness is good, moistureproof compared with common optoelectronic composite cable.

Description

A kind of Aviation cable
Technical field
The present invention relates to composite cable technical field, more particularly to a kind of Aviation cable.
Background technology
Optoelectronic composite cable makees transmission line suitable for broadband access network system, is a kind of new access way, its light harvesting Fine, transmission of electricity copper cash can solve the problems, such as broadband access, equipment electricity consumption, signal transmission in one.
Traditional cable and optical fiber are mostly split, and optoelectronic composite cable structure is less, and scheming logical photoelectric compound cable has External diameter is small, in light weight, and occupy little space (series of problems that could be solved with more cables under normal circumstances, can use one herein Root composite rope replaces), the communication cable of data is transmitted, pay much attention to communication quality, and the electromagnetism for coming from outside is done Disturb, it is easy to cause error in data.
But in aerospace field, its anti-shielding ability of existing cable, signal is easily interfered, while also exists The shortcomings that moistureproof refractory ability is poor, tensile strength is weak.
The content of the invention
It is an object of the invention to:In order to solve common photoelectricity meet cable shield effectiveness it is bad, moisture effect is poor asks Topic, the present invention provide a kind of isolation effect good, moistureproof Aviation cable.
The present invention specifically uses following technical scheme to achieve these goals:
A kind of Aviation cable, including a plurality of power line, a plurality of optical fiber cable and a strengthening core, a plurality of power line, a plurality of light Plastic-coated steel belt layer, inner insulating layer, screen layer A, flame retardant coating, damp-proof layer, armor are enclosed with successively outside fine line and a strengthening core And external insulation layer, the gap in plastic-coated steel belt layer are filled with waterproof paste, every power line includes setting gradually from inside to outside There are copper conductor, conductor shield and crosslinked polyetylene insulated layer.
Further, the bar optical fiber cable includes optical fiber cable core, and optical fiber cable core outer wrapping Loose tube.
Further, it is cross-linking radiation polyolefine material that thickness is 0.8~1.6mm that the material of described inner insulating layer, which is, Or cross-linking radiation EP rubbers material.
Further, the flame retardant coating includes copper mesh, expanded granular layer, the mica layer set gradually from inside to outside, institute It is 0.25-0.63mm to state mica layer thickness, and the filament diameter of the copper mesh is 0.26-0.96mm.
Further, screen layer A includes the copper foil layer that thickness is 1.1um, and it is 10um~15um to be coated with thickness on copper foil layer Aluminium foil layer.
Further, screen layer A is the spiral wound screen layer that material is tinned copper wire.
Further, the strengthening core of copper-coated aluminium composite material by being made up.
Beneficial effects of the present invention are as follows:
1st, the present invention is simple in construction, and shield effectiveness is good, and damp-proof and fireproof performance is good, and overall structure is uncomplicated, lighter weight The advantages of, it is beneficial to use suitable for aviation.
2nd, screen layer A includes the copper foil layer that thickness is 1.1um, and the aluminium foil that thickness is 10um~15um is coated with copper foil layer Layer, this structure of screen layer can ensure screen layer under identical thickness, layers of copper used than traditional list using this structure Structure more saving copper material, has saved cost, and on the other hand, aluminium foil quality is lighter, so as to also reduce the weight of screen layer, the knot Structure avoids the problem of occurring exoperidium bulge when working out cable shield using tinsel or pierce through core.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention.
Embodiment
In order to which those skilled in the art are better understood from the present invention, below in conjunction with the accompanying drawings with following examples to the present invention It is described in further detail.
Embodiment 1
The present embodiment provides a kind of Aviation cable, it is characterised in that including a plurality of power line 1, a plurality of optical fiber cable 10 and one Bar strengthening core 2, it is characterised in that be enclosed with Clad Steel successively outside a plurality of power line 1, a plurality of optical fiber cable 10 and a strengthening core 2 Belt 3, inner insulating layer 4, screen layer A5, flame retardant coating 6, damp-proof layer 7, armor 8 and external insulation layer 9, the sky in plastic-coated steel belt layer 3 Waterproof paste 11 is filled with gap, every power line 1 includes being disposed with copper conductor 1-1, conductor shield 1-2 from inside to outside With crosslinked polyetylene insulated layer 1-3.
The present embodiment is simple in construction, and shield effectiveness is good, and damp-proof and fireproof performance is good, and overall structure is uncomplicated, lighter weight The advantages of, it is beneficial to use suitable for aviation.
Embodiment 2
The present embodiment is further optimized on the basis of embodiment 1, is specifically:
The bar optical fiber cable 10 includes optical fiber cable core 10-1, and optical fiber cable core 10-1 outer wrappings Loose tube 10-2.
It is that cross-linking radiation polyolefine material that thickness is 0.8~1.6mm or irradiation are handed over that the material of described inner insulating layer 4, which is, Join EP rubbers material.
Embodiment 3
The present embodiment is further optimized on the basis of embodiment 1 or 2, is specifically:
The flame retardant coating 4 includes copper mesh, expanded granular layer, the mica layer set gradually from inside to outside, the mica layer Thickness is 0.25-0.63mm, and the filament diameter of the copper mesh is 0.26-0.96mm.
Screen layer A5 includes the copper foil layer that thickness is 1.1um, and the aluminium foil layer that thickness is 10um~15um is coated with copper foil layer.
Screen layer A5 is the spiral wound screen layer that material is tinned copper wire.
The strengthening core 2 of copper-coated aluminium composite material by being made up.
Described above, only presently preferred embodiments of the present invention is not intended to limit the invention, patent protection model of the invention Enclose and be defined by claims, the equivalent structure change that every specification and accompanying drawing content with the present invention is made, similarly It should include within the scope of the present invention.

Claims (7)

1. a kind of Aviation cable, it is characterised in that including a plurality of power line (1), a plurality of optical fiber cable (10) and a strengthening core (2), it is characterised in that a plurality of power line (1), a plurality of optical fiber cable (10) and a strengthening core (2) are enclosed with Clad Steel successively outside Belt (3), inner insulating layer (4), screen layer A (5), flame retardant coating (6), damp-proof layer (7), armor (8) and external insulation layer (9), apply Gap in plastic-steel belt (3) is filled with waterproof paste (11), and every power line (1) includes being disposed with copper from inside to outside Conductor (1-1), conductor shield (1-2) and crosslinked polyetylene insulated layer (1-3).
2. Aviation cable according to claim 1, it is characterised in that the bar optical fiber cable (10) includes optical fiber cable core (10- 1), optical fiber cable core (10-1) outer wrapping Loose tube (10-2).
3. Aviation cable according to claim 1, it is characterised in that it is thickness that the material of described inner insulating layer (4), which is, Cross-linking radiation polyolefine material or cross-linking radiation EP rubbers material for 0.8~1.6mm.
4. Aviation cable according to claim 1, it is characterised in that the flame retardant coating (4) includes setting successively from inside to outside Copper mesh, expanded granular layer, the mica layer put, the mica layer thickness are 0.25-0.63mm, the filament diameter of the copper mesh For 0.26-0.96mm.
5. Aviation cable according to claim 1 or 2, it is characterised in that screen layer A (5) includes the copper that thickness is 1.1um Layers of foil, the aluminium foil layer that thickness is 10um~15um is coated with copper foil layer.
6. according to the Aviation cable described in claim 1,2 or 3, it is characterised in that screen layer A (5) is that material is tinned copper wire Spiral wound screen layer.
7. Aviation cable according to claim 1, it is characterised in that the strengthening core (2) is by copper-coated aluminium composite material It is made.
CN201710882334.XA 2017-09-26 2017-09-26 A kind of Aviation cable Withdrawn CN107564615A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710882334.XA CN107564615A (en) 2017-09-26 2017-09-26 A kind of Aviation cable

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710882334.XA CN107564615A (en) 2017-09-26 2017-09-26 A kind of Aviation cable

Publications (1)

Publication Number Publication Date
CN107564615A true CN107564615A (en) 2018-01-09

Family

ID=60981825

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710882334.XA Withdrawn CN107564615A (en) 2017-09-26 2017-09-26 A kind of Aviation cable

Country Status (1)

Country Link
CN (1) CN107564615A (en)

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Application publication date: 20180109

WW01 Invention patent application withdrawn after publication