CN206986586U - A kind of Aviation Steel Wire Rope - Google Patents
A kind of Aviation Steel Wire Rope Download PDFInfo
- Publication number
- CN206986586U CN206986586U CN201720781063.4U CN201720781063U CN206986586U CN 206986586 U CN206986586 U CN 206986586U CN 201720781063 U CN201720781063 U CN 201720781063U CN 206986586 U CN206986586 U CN 206986586U
- Authority
- CN
- China
- Prior art keywords
- steel wire
- wire rope
- main body
- buffer structure
- axial cord
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses a kind of Aviation Steel Wire Rope, including chaining, buffer structure, steel wire rope main body and axial cord, the two of the buffer structure are provided with buffing pad, and the middle position on the inside of buffing pad is connected by buffer spring, connected at marginal position on the inside of the buffer spring by deformed bar, the both ends of the buffer structure are all provided with fixed block by second bearing, and middle position of the fixed block away from buffer structure one end is provided with steel wire rope main body, the fixed block is all provided with two first reinforcements at the marginal position away from buffer structure one end.It is of the present utility model to be internally provided with axial cord, and it is raised that reinforcement is provided with the outside of axial cord, the intensity of axial cord can effectively be improved, so as to improve the intensity of steel wire rope, three strands of outer ring rope strands are wound with the outside of axial cord, and rope strand is mutually entwined by three steel wires, further increases the intensity of steel wire rope.
Description
Technical field
Technical field of aerospace is the utility model is related to, specially a kind of Aviation Steel Wire Rope.
Background technology
Aircraft cable mainly to control the rudder of aircraft, aileron, engine, landing gear, compass needle rectifier etc.,
Aircraft cable is higher than general ordinary steel rope because use environment is special, it is safe and reliable to require and can use for a long time
Performance requirement, current Aviation Steel Wire Rope does not have preferable cushioning effect, when the power of steel wire rope hand to suddenly change, hold
Larger injury is easily caused to steel wire rope, and current steel wire rope is consolidated without structure that is preferably fixed and installing, steel wire rope
Fixed and connection by the way of knotting, uses inconvenience mostly.
Utility model content
The purpose of this utility model is to provide a kind of Aviation Steel Wire Rope, asked with solve to propose in above-mentioned background technology
Topic.
To achieve the above object, the utility model provides following technical scheme：A kind of Aviation Steel Wire Rope, including chaining,
Buffer structure, steel wire rope main body and axial cord, the two of the buffer structure is provided with buffing pad, and the interposition on the inside of buffing pad
Put place to connect by buffer spring, connected at the marginal position on the inside of the buffer spring by deformed bar, the buffering
The both ends of structure are all provided with fixed block, and middle position installation of the fixed block away from buffer structure one end by second bearing
There is steel wire rope main body, the fixed block is all provided with two first reinforcements at the marginal position away from buffer structure one end, and
The one end of first reinforcement away from fixed block is fixed on the outside of steel wire rope main body, and the steel wire rope main body is away from buffer structure
One end is all installed by connecting seat and chaining, is provided with two groups of fixed seats on the outside of the chaining, and pass through first in fixed seat
Bearing is provided with hook, and the steel wire rope main body is internally provided with axial cord, and three bursts of outer rings are wound with the outside of axial cord
Rope strand, and outer ring rope strand is internally provided with three steel wires mutually wound.
Preferably, antifriction band is provided with the inside of the chaining.
Preferably, the surface of the hook is coated with skid resistant course.
Preferably, it is raised that three groups of reinforcements are provided with the outside of the axial cord.
Preferably, the connecting seat is all provided with two second reinforcements close to one end of steel wire rope main body, and second adds
The one end of strengthening tendons away from connecting seat is all fixed in steel wire rope main body.
Compared with prior art, the beneficial effects of the utility model are：
(1) Aviation Steel Wire Rope is internally provided with axial cord, and it is raised to be provided with reinforcement on the outside of axial cord, can be with
The effective intensity for improving axial cord, so as to improve the intensity of steel wire rope, is wound with three strands of outer ring rope strands on the outside of axial cord, and
Rope strand is mutually entwined by three steel wires, further increases the intensity of steel wire rope.
(2) centre position of the Aviation Steel Wire Rope is provided with buffer structure, and buffer structure is provided at both ends with buffing pad,
And be attached between buffing pad by deformed bar, can play certain cushioning effect, on the inside of simultaneous buffering seat in
Between position connected by buffer spring, deformed bar can be aided in make it that buffering effect is more preferable.
(3) Aviation Steel Wire Rope is provided at both ends with chaining, can facilitate the both ends of steel wire rope being enclosed on specified location,
So that fixation and the installation enhanced convenience of steel wire rope, the outside of chaining is all provided with two groups of hooks, but according to circumstances selects
Hook or chaining so that the installation of steel wire rope is more flexible, while can also be easy to link together on two steel wire ropes so that
The use enhanced convenience of steel wire rope.
(4) hook of the Aviation Steel Wire Rope is arranged in mounting seat by clutch shaft bearing so that hook can freely revolve
Turn, situation about winding occurs in chaining when avoiding using, and is connected between buffer structure and steel wire rope main body by second bearing, makes
Obtain steel wire rope main body to be free to rotate, avoid steel wire rope main body from being effectively protected steel wire rope by larger torsion
Main body, so as to the service life of steel wire rope improved.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is buffer structure position of the present utility model schematic diagram；
Fig. 3 is sectional view of the present utility model.
In figure：1- is linked up with；2- clutch shaft bearings；3- fixed seats；4- chainings；5- connecting seats；The reinforcements of 6- first；7- is fixed
Block；8- deformed bars；9- buffer structures；10- buffing pads；11- second bearings；12- steel wire rope main bodys；The reinforcements of 13- second；
14- buffer springs；15- axial cords；16- outer rings rope strand；17- strengthens raised；18- steel wires.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Refer to Fig. 1-3, a kind of embodiment provided by the utility model：A kind of Aviation Steel Wire Rope, including it is chaining 4, slow
Structure 9, steel wire rope main body 12 and axial cord 15 are rushed, the two of buffer structure 9 is provided with buffing pad 10, and in the inner side of buffing pad 10
Between opening position connected by buffer spring 14, connected, played by deformed bar 8 at the marginal position of the inner side of buffer spring 14
Certain cushioning effect, the both ends of buffer structure 9 are all provided with fixed block 7 by second bearing 11, for installing steel wire rope master
Body 12 so that steel wire rope main body 12 be free to rotate, and middle position peace of the fixed block 7 away from the one end of buffer structure 9
Equipped with steel wire rope main body 12, fixed block 7 is all provided with two first reinforcements 6 at the marginal position away from the one end of buffer structure 9,
And first the one end of reinforcement 6 away from fixed block 7 be fixed on the outside of steel wire rope main body 12, steel wire rope main body 12 is tied away from buffering
All by the installation of connecting seat 5 and chaining 4, the inner side of chaining 4 is provided with antifriction band, the inner side of chaining 12 is played for one end of structure 9
Protective effect, connecting seat 5 are all provided with two second reinforcements 13, and the second reinforcement 13 close to one end of steel wire rope main body 12
One end away from connecting seat 5 is all fixed in steel wire rope main body 12, and connecting seat 5 and the junction of steel wire rope main body 12 are more firm
Gu the outside of chaining 4 is provided with two groups of fixed seats 3, and is provided with hook 1, clutch shaft bearing 2 by clutch shaft bearing 2 in fixed seat 3
Hook can be rotated freely, so that the installation enhanced convenience of steel wire rope, the surface for linking up with 1 is coated with skid resistant course, rises
To anti-skidding effect, hook is avoided to slip, steel wire rope main body 12 is internally provided with axial cord 15, and the outside of axial cord 15 is set
There are three groups of reinforcement projections 17 so that the structure of axial cord 15 is more stable, and the outside of axial cord 15 is wound with three bursts of outer rings
Rope strand 16, and outer ring rope strand 16 is internally provided with three steel wires mutually wound 18, can improve the intensity of outer ring rope strand 16.
Operation principle：Steel wire rope can be fixed on by specified location by chaining 4 first, and can be selective as needed
Use link up with 1 pair of steel wire rope and be fixed, steel wire rope can be arranged on by specified location by hook 1, first rotating shaft 2 can be with
So that hook 1 rotates freely so that fixed enhanced convenience, and chaining 4 will not tangled up and knotted, when steel wire rope is unexpected by power
When converting, middle buffer gear 9 can play preferable buffering effect, can pass through the He of deformed bar 8 of inside
The power that steel wire rope is subject to by buffer spring 14 is laid down, and avoids the power of suddenly change from damaging steel wire rope, when steel wire rope by
During torsion, second bearing 11 can dissolve torsion to fall, and avoid torsion from damaging steel wire rope.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and
And in the case of without departing substantially from spirit or essential attributes of the present utility model, it can realize that this practicality is new in other specific forms
Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new
The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained
All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation
Involved claim.
Claims (5)
1. a kind of Aviation Steel Wire Rope, including chaining (4), buffer structure (9), steel wire rope main body (12) and axial cord (15), its
It is characterised by：The two of the buffer structure (9) are provided with buffing pad (10), and the middle position on the inside of buffing pad (10) passes through
Buffer spring (14) connects, and is connected at the marginal position on the inside of the buffer spring (14) by deformed bar (8), described slow
The both ends for rushing structure (9) are all provided with fixed block (7) by second bearing (11), and fixed block (7) is away from buffer structure (9) one
The middle position at end is provided with steel wire rope main body (12), marginal position of the fixed block (7) away from buffer structure (9) one end
Place is all provided with two first reinforcements (6), and the one end of the first reinforcement (6) away from fixed block (7) is fixed on steel wire rope master
The outside of body (12), the one end of the steel wire rope main body (12) away from buffer structure (9) all pass through connecting seat (5) installation and chaining
(4) two groups of fixed seats (3), are installed on the outside of the chaining (4), and extension is provided with by clutch shaft bearing (2) in fixed seat (3)
Hook (1), the steel wire rope main body (12) are internally provided with axial cord (15), and are wound with the outside of axial cord (15) outside three strands
Rope strand (16) is enclosed, and outer ring rope strand (16) is internally provided with three steel wires mutually wound (18).
A kind of 2. Aviation Steel Wire Rope according to claim 1, it is characterised in that：It is provided with the inside of the chaining (4)
Antifriction band.
A kind of 3. Aviation Steel Wire Rope according to claim 1, it is characterised in that：The surface of the hook (1) is coated with
Skid resistant course.
A kind of 4. Aviation Steel Wire Rope according to claim 1, it is characterised in that：The outside of the axial cord (15) is set
There are three groups of reinforcements raised (17).
A kind of 5. Aviation Steel Wire Rope according to claim 1, it is characterised in that：The connecting seat (5) is close to steel wire rope
One end of main body (12) is all provided with two second reinforcements (13), and the one end of the second reinforcement (13) away from connecting seat (5)
All it is fixed in steel wire rope main body (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720781063.4U CN206986586U (en) | 2017-06-30 | 2017-06-30 | A kind of Aviation Steel Wire Rope |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720781063.4U CN206986586U (en) | 2017-06-30 | 2017-06-30 | A kind of Aviation Steel Wire Rope |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206986586U true CN206986586U (en) | 2018-02-09 |
Family
ID=61400457
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720781063.4U Expired - Fee Related CN206986586U (en) | 2017-06-30 | 2017-06-30 | A kind of Aviation Steel Wire Rope |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206986586U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113047072A (en) * | 2019-12-29 | 2021-06-29 | 盐城神力制绳有限公司 | Ultra-high molecular weight polyethylene cable |
-
2017
- 2017-06-30 CN CN201720781063.4U patent/CN206986586U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113047072A (en) * | 2019-12-29 | 2021-06-29 | 盐城神力制绳有限公司 | Ultra-high molecular weight polyethylene cable |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180209 Termination date: 20190630 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |