CN108806839A - A kind of compound aviation conductor structure and preparation method thereof - Google Patents
A kind of compound aviation conductor structure and preparation method thereof Download PDFInfo
- Publication number
- CN108806839A CN108806839A CN201810476789.6A CN201810476789A CN108806839A CN 108806839 A CN108806839 A CN 108806839A CN 201810476789 A CN201810476789 A CN 201810476789A CN 108806839 A CN108806839 A CN 108806839A
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- CN
- China
- Prior art keywords
- conductor
- internal layer
- outer layer
- sensation
- roots
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Classifications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B7/00—Insulated conductors or cables characterised by their form
- H01B7/0009—Details relating to the conductive cores
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B13/00—Apparatus or processes specially adapted for manufacturing conductors or cables
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B13/00—Apparatus or processes specially adapted for manufacturing conductors or cables
- H01B13/02—Stranding-up
- H01B13/0271—Alternate stranding processes
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B5/00—Non-insulated conductors or conductive bodies characterised by their form
- H01B5/08—Several wires or the like stranded in the form of a rope
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Ropes Or Cables (AREA)
Abstract
The present invention provides a kind of compound aviation conductor structures, including the internal layer set gradually from the inside to the outside, middle level and outer layer, the internal layer is made of first conductor, by three first conductors and three, the second conductor is spaced and wrappage around internal layer is constituted in middle level, outer layer is spaced by the first conductor of the six roots of sensation and the second conductor of the six roots of sensation and is constituted around middle level, first conductor includes the first internal layer and the first outer layer, first internal layer is made of a first conductor strand unit, first outer layer is made of the six roots of sensation the first conductor strand cell rings around the first internal layer, second conductor includes the second internal layer and the second outer layer, second internal layer is made of a second conductor strand unit, second outer layer is made of the six roots of sensation the second conductor strand cell rings around the second internal layer.Advantage is：By substituting traditional tinned wird or silver-coated copper wire, the weight of whole conductor is effectively reduced, in addition by using two kinds of staggered modes of conductor, efficiently solves the defect for being susceptible to creep when aluminium conductor crimping.
Description
Technical field
The present invention relates to conductor strand technical fields more particularly to a kind of compound aviation conductor structure and preparation method thereof.
Background technology
Aeronautics and space aircraft is in earth atmosphere and the movable general name of the navigation of space.The hair of aerospace cause
Exhibition is the science and technology leap progress of 20th century, the result that social production is advanced by leaps and bounds.The achievement of aerospace has concentrated science skill
Numerous New TownMovements of art.Aerospace operations so far, although being also that the mankind leave the initial several of the earth this cradle
Step, but its effect all produces politics, economic, military affairs down to human society life far beyond science and technology field
Far-reaching influence extensively.Wherein, it usually requires to use a large amount of electronic equipment in aircraft, and these electronic equipments is normal
Operation be unable to do without conductor, currently, the production and processing of existing aviation conductor needs to be twisted by multiple conducting wires, and leads
Mostly traditional tinned wird or silver-coated copper wire employed in line, and then the overall weight of conductor is increased, and lead to entirety
The weight of aircraft increases.
Invention content
To solve the above problems, the invention discloses a kind of compound aviation conductor structure and preparation method thereof, effectively reduce
The weight of whole conductor, and solve the defect that creep is susceptible to when aluminium conductor crimping.
In order to reach object above, the present invention provides the following technical solutions：
A kind of compound aviation conductor structure, it is characterised in that：Including internal layer, middle level and the outer layer set gradually from the inside to the outside, institute
It states internal layer to be made of first conductor, the middle level is spaced by three first conductors and three second conductors and surround
Internal layer is constituted, and the outer layer is spaced by the first conductor of the six roots of sensation and the second conductor of the six roots of sensation and constitutes around middle level, and described the
One conductor includes the first internal layer and the first outer layer by being set gradually outside interior cause, and first internal layer is by first conductor strand
Unit is constituted, and first outer layer is made of the six roots of sensation the first conductor strand cell rings around the first internal layer, and second conductor includes
By the second internal layer and the second outer layer set gradually outside interior cause, second internal layer is made of a second conductor strand unit,
Second outer layer is made of the six roots of sensation the second conductor strand cell rings around the second internal layer.
Further, it is arranged with protection pipe outside first conductor and the second conductor.
Further, the aluminium conductor that the first conductor strand unit is a diameter of 0.45mm is twisted unit.
Further, the copper clad aluminum conductor that the second conductor strand unit is a diameter of 0.45mm is twisted unit.
A kind of preparation method of compound aviation conductor structure, it is characterised in that：By the way of staggeredly twisted or welding.
Compared with prior art, the beneficial effects of the present invention are：By substituting traditional tinned wird or silver-coated copper wire,
The weight for effectively reducing whole conductor, so as to be aeronautical product loss of weight, in addition by using two kinds of staggered sides of conductor
Formula efficiently solves the defect that creep is susceptible to when aluminium conductor crimping.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of compound aviation conductor structure of the present invention and preparation method thereof.
Fig. 2 is the structural schematic diagram of the first conductor in a kind of compound aviation conductor structure of the present invention and preparation method thereof.
Fig. 3 is the structural schematic diagram of the second conductor in a kind of compound aviation conductor structure of the present invention and preparation method thereof.
Reference numerals list：
1- internal layers, the middle levels 2-, 3- outer layers, the first conductors of 4-, the second conductors of 5-, 6- the first conductor strand units, the second conductors of 7-
Twisted unit.
Specific implementation mode
With reference to the accompanying drawings and detailed description, the present invention is furture elucidated, it should be understood that following specific implementation modes are only
For illustrating the present invention rather than limiting the scope of the invention.It should be noted that word " preceding " used in the following description,
" rear ", "left", "right", "up" and "down" refer to that the direction in attached drawing, word "inner" and "outside" refer respectively to direction or remote
Direction from geometric center of specific component.
As shown, a kind of compound aviation conductor structure, including the internal layer 1, middle level 2 and the outer layer that set gradually from the inside to the outside
3, internal layer 1 is made of first conductor 4, and middle level is spaced by three first conductors 4 and three second conductors 5 and surround
Internal layer 1 is constituted, and outer layer 3 is spaced by the first conductor of the six roots of sensation 4 and the second conductor of the six roots of sensation 5 and is constituted around middle level 2, and first leads
Body 4 includes the first internal layer and the first outer layer by being set gradually outside interior cause, and the first internal layer is by 6 structure of the first conductor strand unit
Be made of around the first internal layer the first conductor strand of six roots of sensation unit 6 at, the first outer layer, the second conductor 5 include by outside interior cause successively
The second internal layer and the second outer layer being arranged, the second internal layer are made of a second conductor strand unit 7, and the second outer layer is by the six roots of sensation
Two conductor strand units 7 are constituted around the second internal layer.
In the present embodiment, it is arranged with protection pipe outside the first conductor 4 and the second conductor 5.
In the present embodiment, the aluminium conductor that the first conductor strand unit 6 is a diameter of 0.45mm is twisted unit.
In the present embodiment, the copper clad aluminum conductor that the second conductor strand unit 7 is a diameter of 0.45mm is twisted unit.
A kind of preparation method of compound aviation conductor structure, it is characterised in that：By the way of staggeredly twisted or welding.
The present invention effectively reduces the weight of whole conductor by replacement traditional tinned wird or silver-coated copper wire, so as to
It is easy when efficiently solving aluminium conductor crimping in addition by using two kinds of conductor staggered modes for aeronautical product loss of weight
There is the defect of creep.
The technical means disclosed in the embodiments of the present invention is not limited only to the technological means disclosed in the above embodiment, further includes
By the above technical characteristic arbitrarily the formed technical solution of combination.It should be pointed out that for those skilled in the art
For, various improvements and modifications may be made without departing from the principle of the present invention, these improvements and modifications are also considered as
Protection scope of the present invention.
Claims (5)
1. a kind of compound aviation conductor structure, it is characterised in that：Including the internal layer set gradually from the inside to the outside（1）, middle level（2）With
Outer layer（3）, the internal layer（1）By first conductor（4）It constitutes, the middle level is by three first conductors（4）And three
Two conductors（5）Spaced and wrappage around internal layer（1）It constitutes, the outer layer（3）By the first conductor of the six roots of sensation（4）And the six roots of sensation second is led
Body（5）Spaced and circular middle level（2）It constitutes, first conductor（4）It include the first internal layer by being set gradually outside interior cause
With the first outer layer, first internal layer is by a first conductor strand unit（6）It constitutes, first outer layer is led by the six roots of sensation first
Body is twisted unit（6）It is constituted around the first internal layer, second conductor（5）Include the second internal layer by setting gradually outside interior cause and
Second outer layer, second internal layer is by a second conductor strand unit（7）It constitutes, second outer layer is by the second conductor of the six roots of sensation
Twisted unit（7）It is constituted around the second internal layer.
2. a kind of compound aviation conductor structure according to claim 1, it is characterised in that：First conductor（4）With
Two conductors（5）It is arranged with protection pipe outside.
3. a kind of compound aviation conductor structure according to claim 2, it is characterised in that：The first conductor strand unit
（6）It is twisted unit for the aluminium conductor of a diameter of 0.45mm.
4. a kind of compound aviation conductor structure according to claim 2, it is characterised in that：The second conductor strand unit
（7）It is twisted unit for the copper clad aluminum conductor of a diameter of 0.45mm.
5. a kind of preparation method of compound aviation conductor structure, it is characterised in that：By the way of staggeredly twisted or welding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810476789.6A CN108806839A (en) | 2018-05-18 | 2018-05-18 | A kind of compound aviation conductor structure and preparation method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810476789.6A CN108806839A (en) | 2018-05-18 | 2018-05-18 | A kind of compound aviation conductor structure and preparation method thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108806839A true CN108806839A (en) | 2018-11-13 |
Family
ID=64092581
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810476789.6A Pending CN108806839A (en) | 2018-05-18 | 2018-05-18 | A kind of compound aviation conductor structure and preparation method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108806839A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202332363U (en) * | 2011-12-02 | 2012-07-11 | 衡阳恒飞电缆有限责任公司 | Cold-resistant and torsion-resistant flexible wind power cable for wind power generation |
| CN205384880U (en) * | 2015-12-26 | 2016-07-13 | 惠州乐庭电子线缆有限公司 | Conductor transposition structure |
| CN105931702A (en) * | 2016-06-27 | 2016-09-07 | 平高集团有限公司 | Fine-pitch flexible aluminum stranded wire and manufacturing method thereof |
| CN106251939A (en) * | 2016-08-30 | 2016-12-21 | 西安飞机工业（集团）亨通航空电子有限公司 | A kind of aircraft high-strength abrasion-proof high temperature resistant soft type wire |
| CN106448829A (en) * | 2014-05-22 | 2017-02-22 | 江苏亨通线缆科技有限公司 | Flexible stretch-proof robot cable |
-
2018
- 2018-05-18 CN CN201810476789.6A patent/CN108806839A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202332363U (en) * | 2011-12-02 | 2012-07-11 | 衡阳恒飞电缆有限责任公司 | Cold-resistant and torsion-resistant flexible wind power cable for wind power generation |
| CN106448829A (en) * | 2014-05-22 | 2017-02-22 | 江苏亨通线缆科技有限公司 | Flexible stretch-proof robot cable |
| CN205384880U (en) * | 2015-12-26 | 2016-07-13 | 惠州乐庭电子线缆有限公司 | Conductor transposition structure |
| CN105931702A (en) * | 2016-06-27 | 2016-09-07 | 平高集团有限公司 | Fine-pitch flexible aluminum stranded wire and manufacturing method thereof |
| CN106251939A (en) * | 2016-08-30 | 2016-12-21 | 西安飞机工业（集团）亨通航空电子有限公司 | A kind of aircraft high-strength abrasion-proof high temperature resistant soft type wire |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20181113 |