CN111696708A - Anti-interference Ethernet cable for aerospace - Google Patents

Anti-interference Ethernet cable for aerospace Download PDF

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Publication number
CN111696708A
CN111696708A CN202010465925.9A CN202010465925A CN111696708A CN 111696708 A CN111696708 A CN 111696708A CN 202010465925 A CN202010465925 A CN 202010465925A CN 111696708 A CN111696708 A CN 111696708A
Authority
CN
China
Prior art keywords
layer
interference
ethernet cable
aerospace
proof
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
CN202010465925.9A
Other languages
Chinese (zh)
Inventor
章新能
张丽
米春海
付利梅
吴天凤
谢飞
周刚
孙静
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.)
Wuhu Spaceflight Special Cable Factory Co Ltd
Original Assignee
Wuhu Spaceflight Special Cable Factory 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 Wuhu Spaceflight Special Cable Factory Co Ltd filed Critical Wuhu Spaceflight Special Cable Factory Co Ltd
Priority to CN202010465925.9A priority Critical patent/CN111696708A/en
Publication of CN111696708A publication Critical patent/CN111696708A/en
Pending legal-status Critical Current

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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B11/00Communication cables or conductors
    • H01B11/02Cables with twisted pairs or quads
    • H01B11/06Cables with twisted pairs or quads with means for reducing effects of electromagnetic or electrostatic disturbances, e.g. screens
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B7/00Insulated conductors or cables characterised by their form
    • H01B7/17Protection against damage caused by external factors, e.g. sheaths or armouring
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B7/00Insulated conductors or cables characterised by their form
    • H01B7/17Protection against damage caused by external factors, e.g. sheaths or armouring
    • H01B7/18Protection against damage caused by wear, mechanical force or pressure; Sheaths; Armouring
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B7/00Insulated conductors or cables characterised by their form
    • H01B7/17Protection against damage caused by external factors, e.g. sheaths or armouring
    • H01B7/18Protection against damage caused by wear, mechanical force or pressure; Sheaths; Armouring
    • H01B7/22Metal wires or tapes, e.g. made of steel

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Insulated Conductors (AREA)

Abstract

The invention discloses an anti-interference Ethernet cable for space navigation, which sequentially comprises the following components from outside to inside: the cable comprises a first sheath layer, a first shielding layer and a first wrapping layer; a cavity is formed in the first wrapping layer, a supporting framework is arranged in the cavity, and a plurality of side grooves are formed in the side surface of the supporting framework; an Ethernet cable core is arranged in the side groove and is respectively extruded with the side wall of the side groove and the first wrapping layer; the supporting framework is a foaming framework, and the foaming degree of the supporting framework is 20-40%. The interference-proof Ethernet cable for aerospace has excellent interference-proof performance.

Description

Anti-interference Ethernet cable for aerospace
Technical Field
The invention relates to a cable, in particular to an anti-interference Ethernet cable for space navigation.
Background
In the field of aerospace science and technology, an ethernet cable should have excellent interference prevention performance so as to obtain a better communication effect, interference capability generated by the ethernet cable is strongest due to a close distance between ethernet cable cores in the ethernet cable, but the interference capability cannot be weakened by changing the distance, and therefore, an interference prevention type ethernet cable with excellent interference prevention performance for aerospace is urgently needed.
Disclosure of Invention
The invention aims to provide an anti-interference Ethernet cable for aerospace, which has excellent anti-interference performance.
In order to achieve the above object, the present invention provides an interference-proof ethernet cable for aerospace, comprising, in order from outside to inside: the cable comprises a first sheath layer, a first shielding layer and a first wrapping layer; a cavity is formed in the first wrapping layer, a supporting framework is arranged in the cavity, and a plurality of side grooves are formed in the side face of the supporting framework; an Ethernet cable core is arranged in the side groove and is respectively extruded with the side wall of the side groove and the first wrapping layer; the supporting framework is a foaming framework, and the foaming degree of the supporting framework is 20-40%.
Preferably, a steel wire is embedded in the foaming type framework.
Preferably, the first shielding layer is a tinned copper wire braided layer.
Preferably, the first sheath layer is a soluble polytetrafluoroethylene layer.
Preferably, the first wrapping layer is formed by wrapping an expanded polytetrafluoroethylene film.
Preferably, the ethernet cable core includes from outside to inside: the second sheath layer, the second shielding layer, the second around covering and double strand copper conductor stranded conductor.
Preferably, the second shielding layer is a silver-plated copper wire braided layer.
Preferably, the second sheath layer is a soluble polytetrafluoroethylene layer.
Preferably, the thickness of the second sheath layer is 0.5mm-1 mm.
Preferably, the second wrapping layer is formed by wrapping an expanded polytetrafluoroethylene film.
Other features and advantages of the present invention, in accordance with the above teachings, are set forth in the following detailed description.
Additional features and advantages of the invention will be set forth in the detailed description which follows.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention and not to limit the invention. In the drawings:
fig. 1 is a block diagram of a preferred embodiment of an interference-proof ethernet cable for aerospace.
Description of the reference numerals
1 first sheath layer 2 first shielding layer
3 first 4 supporting frameworks around covering
5 steel wire 6 second sheath layer
7 second shielding layer 8 copper conductor stranded wire
Detailed Description
The following detailed description of embodiments of the invention refers to the accompanying drawings. It should be understood that the detailed description and specific examples, while indicating the present invention, are given by way of illustration and explanation only, not limitation.
In the present invention, unless otherwise specified, directional words included in terms such as "upper, lower, left, right, front, rear, inner, and outer" and the like merely represent the directions of the terms in a normal use state or are colloquially known by those skilled in the art, and should not be construed as limiting the terms.
Referring to fig. 1, the interference-proof ethernet cable for aerospace includes, in order from outside to inside: the cable comprises a first sheath layer 1, a first shielding layer 2 and a first wrapping layer 3; a cavity is formed in the first wrapping layer 3, a supporting framework 4 is arranged in the cavity, and a plurality of side grooves are formed in the side surface of the supporting framework 4; an Ethernet cable core is arranged in the side groove and is respectively extruded with the side wall of the side groove and the first wrapping layer 3; the supporting framework 4 is a foaming framework, and the foaming degree of the supporting framework 4 is 20-40%.
Through the implementation of the technical scheme, the supporting framework 4 adopts the foaming type framework with the foaming degree of 20-40%, the dielectric constant of the supporting framework 4 can be reduced, the insulation characteristic of the supporting framework 4 is improved, the anti-interference performance is improved, the mutual interference between all Ethernet cable cores in the cable can be reduced, the mutual interference between the cable cores can be reduced through the first shielding layer 2, the whole cable has excellent anti-interference performance, the arrangement of a plurality of side grooves is realized, and the first winding layer 3 is arranged on the outer layer, so that the production and the manufacturing of the cable can be facilitated.
In this embodiment, in order to enhance the bending resistance of the whole, it is preferable that the steel wire 5 is embedded in the foamed frame.
In this embodiment, the first shielding layer 2 is preferably a braided layer of tinned copper wire.
In this embodiment, preferably, the first sheath layer 1 is a soluble polytetrafluoroethylene layer.
In this embodiment, the first wrapping layer 3 is preferably formed by wrapping an expanded polytetrafluoroethylene film.
In this embodiment, preferably, the ethernet cable core includes, from outside to inside: second restrictive coating 6, second shielding layer 7, second around covering and double strand copper conductor stranded conductor 8.
In this embodiment, the second shielding layer 7 is preferably a silver-plated copper wire braided layer.
In this embodiment, preferably, the second sheath layer 6 is a soluble polytetrafluoroethylene layer.
In this embodiment, in order to reduce the overall weight, the thickness of the second sheath layer 6 should not be excessively large, and preferably, the thickness of the second sheath layer 6 is 0.5mm to 1 mm.
In this embodiment, preferably, the second wrapping layer is formed by wrapping an expanded polytetrafluoroethylene film.
The preferred embodiments of the present invention have been described in detail with reference to the accompanying drawings, however, the present invention is not limited to the specific details of the above embodiments, and various simple modifications can be made to the technical solution of the present invention within the technical idea of the present invention, and these simple modifications are within the protective scope of the present invention.
It should be noted that the various technical features described in the above embodiments can be combined in any suitable manner without contradiction, and the invention is not described in any way for the possible combinations in order to avoid unnecessary repetition.
In addition, any combination of the various embodiments of the present invention is also possible, and the same should be considered as the disclosure of the present invention as long as it does not depart from the spirit of the present invention.

Claims (10)

1. An interference-proof Ethernet cable for aerospace, characterized in that the interference-proof Ethernet cable for aerospace comprises from outside to inside in sequence: the cable comprises a first sheath layer (1), a first shielding layer (2) and a first wrapping layer (3);
a cavity is formed in the first wrapping layer (3), a supporting framework (4) is arranged in the cavity, and a plurality of side grooves are formed in the side surface of the supporting framework (4);
an Ethernet cable core is arranged in the side groove and is respectively extruded with the side wall of the side groove and the first wrapping layer (3);
the supporting framework (4) is a foaming framework, and the foaming degree of the supporting framework (4) is 20-40%.
2. The interference-proof ethernet cable for aerospace according to claim 1, wherein steel wires (5) are embedded in the foamed skeleton.
3. Aerospace interference-proof ethernet cable according to claim 1, wherein the first shielding layer (2) is a tinned copper wire braid.
4. Aerospace interference-proof ethernet cable according to claim 1, characterized in that the first jacket layer (1) is a layer of soluble polytetrafluoroethylene.
5. The interference-proof Ethernet cable for aerospace according to claim 1, wherein the first wrapping layer (3) is formed by wrapping an expanded polytetrafluoroethylene film.
6. The interference-proof ethernet cable for aerospace according to any of claims 1-5, wherein said ethernet core comprises from outside to inside: the cable comprises a second sheath layer (6), a second shielding layer (7), a second wrapping layer and a double-strand copper conductor stranded wire (8).
7. The interference-proof Ethernet cable for aerospace according to claim 6, wherein the second shielding layer (7) is a silver-plated copper-wire braided layer.
8. Aerospace interference-proof ethernet cable according to claim 1, wherein the second sheath layer (6) is a layer of soluble polytetrafluoroethylene.
9. Aerospace interference-proof ethernet cable according to claim 8, wherein the thickness of the second sheath layer (6) is 0.5mm-1 mm.
10. The interference-proof Ethernet cable for aerospace according to claim 1, wherein the second wrapping layer is formed by wrapping an expanded polytetrafluoroethylene film.
CN202010465925.9A 2020-05-28 2020-05-28 Anti-interference Ethernet cable for aerospace Pending CN111696708A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010465925.9A CN111696708A (en) 2020-05-28 2020-05-28 Anti-interference Ethernet cable for aerospace

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010465925.9A CN111696708A (en) 2020-05-28 2020-05-28 Anti-interference Ethernet cable for aerospace

Publications (1)

Publication Number Publication Date
CN111696708A true CN111696708A (en) 2020-09-22

Family

ID=72478690

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010465925.9A Pending CN111696708A (en) 2020-05-28 2020-05-28 Anti-interference Ethernet cable for aerospace

Country Status (1)

Country Link
CN (1) CN111696708A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201638602U (en) * 2010-01-11 2010-11-17 浙江兆龙线缆有限公司 Super six categories unshielded data cable
US20130269967A1 (en) * 2012-03-30 2013-10-17 General Cabletechnologies Corporation Gas encapsulated dual layer separator for a data communications cable
CN107342138A (en) * 2017-05-23 2017-11-10 芜湖航天特种电缆厂股份有限公司 Aerospace ethernet communication cable and preparation method thereof
CN208889377U (en) * 2018-11-16 2019-05-21 宏安集团有限公司 Surpass six type shielding data cables

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201638602U (en) * 2010-01-11 2010-11-17 浙江兆龙线缆有限公司 Super six categories unshielded data cable
US20130269967A1 (en) * 2012-03-30 2013-10-17 General Cabletechnologies Corporation Gas encapsulated dual layer separator for a data communications cable
CN107342138A (en) * 2017-05-23 2017-11-10 芜湖航天特种电缆厂股份有限公司 Aerospace ethernet communication cable and preparation method thereof
CN208889377U (en) * 2018-11-16 2019-05-21 宏安集团有限公司 Surpass six type shielding data cables

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SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
CB03 Change of inventor or designer information

Inventor after: Zhang Xinneng

Inventor after: Mi Chunhai

Inventor after: Fulimei

Inventor after: Wu Tianfeng

Inventor after: Xie Fei

Inventor after: Zhou Gang

Inventor after: Sun Jing

Inventor before: Zhang Xinneng

Inventor before: Zhang Li

Inventor before: Mi Chunhai

Inventor before: Fulimei

Inventor before: Wu Tianfeng

Inventor before: Xie Fei

Inventor before: Zhou Gang

Inventor before: Sun Jing

CB03 Change of inventor or designer information
RJ01 Rejection of invention patent application after publication

Application publication date: 20200922

RJ01 Rejection of invention patent application after publication