CN107150923A - A kind of cable for aerospace wind - Google Patents
A kind of cable for aerospace wind Download PDFInfo
- Publication number
- CN107150923A CN107150923A CN201710584151.XA CN201710584151A CN107150923A CN 107150923 A CN107150923 A CN 107150923A CN 201710584151 A CN201710584151 A CN 201710584151A CN 107150923 A CN107150923 A CN 107150923A
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- cable
- rotating shaft
- rotating cylinder
- rotating
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H54/00—Winding, coiling, or depositing filamentary material
- B65H54/02—Winding and traversing material on to reels, bobbins, tubes, or like package cores or formers
- B65H54/40—Arrangements for rotating packages
- B65H54/54—Arrangements for supporting cores or formers at winding stations; Securing cores or formers to driving members
- B65H54/553—Both-ends supporting arrangements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H54/00—Winding, coiling, or depositing filamentary material
- B65H54/70—Other constructional features of yarn-winding machines
- B65H54/72—Framework; Casings; Coverings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2701/00—Handled material; Storage means
- B65H2701/30—Handled filamentary material
- B65H2701/34—Handled filamentary material electric cords or electric power cables
Abstract
The invention discloses a kind of cable for aerospace wind, including working plate, the left and right sides at the top of the working plate has been fixedly connected with connecting plate, and two mutually close sides of connecting plate are connected with rotating shaft, one end of the close connecting plate of the rotating shaft is fixedly connected with mounting cup, rotating cylinder is fixedly connected with the surface of the rotating shaft, set on the surface of rotating cylinder for concave surface, thread groove is offered on the surface of the rotating cylinder, and it is fixedly connected with U-board between two rotating shafts, rubber ring is socketed with the surface of the U-board, and the slide bar below rotating shaft is fixedly connected between two connecting plates.The present invention rotates U-board, and rotated by setting rotating shaft, rotating cylinder, U-board and rubber ring so that rotating shaft rotates, and rotates rotating cylinder, makes to be wrapped in the cable on rotating cylinder and is easy to winding, and two rotating cylinders, convenient to be wound cable simultaneously, efficiency is faster.
Description
Technical field
The present invention relates to space flight and aviation technical field, specially a kind of cable for aerospace wind.
Background technology
Aero-Space are the modern technologies of a high integrity, be related to many branches of learning and subjects, it include aviation and
Two big branches of space flight.But usually using self-locking nut in the industries such as Aero-Space, but using cable when it
Before need to be wound with device.
But present cable for space flight and aviation wind, when winding cable, cable is inconvenient to wind, and can make electricity
Cable drops down, can influence the cable of Aero-Space and can not effectively be installed, and make cable in a jumble be placed on ground
On, it has not been convenient to arrange, make cable for aerospace in-convenience in use.
The content of the invention
（One）The technical problem of solution
In view of the shortcomings of the prior art, the invention provides a kind of cable for aerospace wind, solve but present
Cable for space flight and aviation wind, winding cable when, cable is inconvenient to wind, and cable can be made to drop down, can influence
The cable of Aero-Space can not be installed effectively, and make the placement of cable in a jumble on the ground, it has not been convenient to arranged, made
Cable for aerospace inconvenient problem with use.
（Two）Technical scheme
To achieve the above object, the present invention provides following technical scheme：A kind of cable for aerospace wind, including work
The left and right sides at the top of plate, the working plate has been fixedly connected with connecting plate, and the mutually close side activity of two connecting plates
Rotating shaft is connected with, one end of the close connecting plate of the rotating shaft is fixedly connected with mounting cup, the surface of the rotating shaft fixed company
It is connected on rotating cylinder, the surface of rotating cylinder and is set for concave surface, is offered on the surface of the rotating cylinder between thread groove, and two rotating shafts
It is fixedly connected with U-board, the surface of the U-board and is socketed with rubber ring, and position is fixedly connected between two connecting plates
It is fixedly connected with the top of two sliding blocks, the sliding block and is fixedly connected with slide bar below rotating shaft, the surface of the slide bar
Annulus, the bottom of the circle ring inner wall, which is fixedly connected with U-shaped block, the inner surface of the U-shaped block, is fixedly connected with rubber blanket, two
Fixed plate is fixedly connected between individual sliding block, and spring, the bullet are fixedly connected with the left of the sliding block on the left of slide bar
It is fixedly connected between the other end of spring and connecting plate.
It is preferred that, the spring is located on the outer surface of slide bar.
It is preferred that, the length of the fixed plate and the equal length of rotating cylinder.
It is preferred that, the quantity of the U-shaped block is 12, and six U-shaped blocks are one group, every group of six U-shaped blocks and circle
The center of ring is symmetrical arranged for symmetrical centre.
It is preferred that, it is coarse setting on the surface of the rubber ring.
It is preferred that, the gap of the thread groove is two centimetres.
（Three）Beneficial effect
The invention provides a kind of cable for aerospace wind.Possesses following beneficial effect：
（1）, the present invention by setting rotating shaft, rotating cylinder, U-board and rubber ring, rotate U-board, and rotated so that rotating shaft is revolved
Turn, rotate rotating cylinder, make to be wrapped in the cable on rotating cylinder and be easy to winding, and two rotating cylinders, it is convenient to be wound cable simultaneously,
Efficiency is faster.
（2）, the present invention by setting annulus, U-shaped block, rubber blanket and fixed plate so that the cable of Aero-Space is being twined
Around when, U-shaped block is pierced into one end, and rubber blanket makes cable for aerospace more resistant.
（3）, the present invention by setting slide bar, sliding block and spring so that sliding block can be moved on slide bar, and pass through profit
With the elastic reaction of spring, sliding block is unclamped, resets sliding block, and facilitate adjustment position.
（4）, the present invention by setting rotating cylinder and thread groove so that the cable of Aero-Space is absorbed in the inside of thread groove,
So that the cable of Aero-Space is more stablized, make more to stablize when winding.
Brief description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is enlarged drawing at A in Fig. 1.
In figure：1 working plate, 2 connecting plates, 3 rotating shafts, 4 mounting cups, 5 rotating cylinders, 6 thread grooves, 7 U-boards, 8 rubber rings, 9 are slided
Bar, 10 sliding blocks, 11 annulus, 12 U-shaped blocks, 13 rubber blankets, 14 fixed plates, 15 springs.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
As shown in Figure 1-2, the present invention provides a kind of technical scheme：A kind of cable for aerospace wind, including work
Make plate 1, the left and right sides at the top of working plate 1 has been fixedly connected with connecting plate 2, and the mutually close side of two connecting plates 2 is lived
Dynamic to be connected with rotating shaft 3, one end of the close connecting plate 2 of rotating shaft 3, which is fixedly connected with mounting cup 4, the surface of rotating shaft 3, to be fixedly connected
Have on rotating cylinder 5, the surface of rotating cylinder 5 for concave surface setting so that rotating cylinder 5 is when the cable of space flight and aviation is wound so that aviation
The cable of space flight is difficult skew, is difficult to drop out, is easy to offer screw thread on the use of wind, the surface of rotating cylinder 5
Groove 6, the gap of thread groove 6 is two centimetres, by setting rotating cylinder 5 and thread groove 6 so that the cable of Aero-Space is absorbed in screw thread
The inside of groove 6 so that the cable of Aero-Space is more stablized, makes more to stablize when winding, and between two rotating shafts 3
It is fixedly connected with U-board 7, the surface of U-board 7 and is socketed with rubber ring 8, is coarse setting on the surface of rubber ring 8, passes through
Rotating shaft 3, rotating cylinder 5, U-board 7 and rubber ring 8 are set, U-board 7 is rotated, and rotated so that rotating shaft 3 rotates, and revolves rotating cylinder 5
Turn, the cable being wrapped on rotating cylinder 5 is easy to winding, and two rotating cylinders 5 are convenient to be wound cable simultaneously, efficiency faster,
And it is fixedly connected between two connecting plates 2 on the slide bar 9 positioned at the lower section of rotating shaft 3, the surface of slide bar 9 and is fixedly connected with two
Sliding block 10, the top of sliding block 10 is fixedly connected with annulus 11, and the bottom of the inwall of annulus 11 is fixedly connected with U-shaped block 12, U-shaped block 12
Quantity be 12, and six U-shaped blocks 12 are one group, and the center of every group of six U-shaped blocks 12 and annulus 11 is in symmetrical
The heart is symmetrical arranged, and the cable of space flight and aviation is inserted into any one U-shaped block 12 so that the cable of Aero-Space is more
Plus stably, more stablize when making winding, be fixedly connected with rubber blanket 13 on the inner surface of U-shaped block 12, two sliding blocks 10 it
Between be fixedly connected with fixed plate 14, by setting annulus 11, U-shaped block 12, rubber blanket 13 and fixed plate 14 so that Aero-Space use
Cable winding when, U-shaped block 12 is pierced into one end, and rubber blanket 13 makes cable for aerospace more resistant, fixed plate
14 length and the equal length of rotating cylinder 5, and the left side of the sliding block 10 positioned at the left side of slide bar 9 is fixedly connected with spring 15, bullet
Spring 15 is located on the outer surface of slide bar 9, is fixedly connected between the other end and connecting plate 2 of spring 15, by setting slide bar 9, sliding
Block 10 and spring 15 so that sliding block 10 can be moved on slide bar 9, and by using the elastic reaction of spring 15, unclamp and slide
Block 10, resets sliding block 10, and facilitate adjustment position.
In use, one of U-shaped block 12 is pierced into one end of cable for aerospace by user, and connect with rotating cylinder 5
Connect, sliding block 10 is moved on slide bar 9, rotate U-board 7, and rotated so that rotating shaft 3 rotates, and rotates rotating cylinder 5, makes winding
Cable on rotating cylinder 5 is easy to winding, and convenient to be wound cable simultaneously, efficiency is faster.
It can to sum up obtain,（1）, the present invention by setting rotating shaft 3, rotating cylinder 5, U-board 7 and rubber ring 8, rotate U-board 7, and
Rotated so that rotating shaft 3 rotates, rotate rotating cylinder 5, the cable being wrapped on rotating cylinder 5 is easy to winding, and two rotating cylinders
5, convenient to be wound cable simultaneously, efficiency is faster.
（2）, the present invention by setting annulus 11, U-shaped block 12, rubber blanket 13 and fixed plate 14 so that Aero-Space
Cable is when winding, and U-shaped block 12 is pierced into one end, and rubber blanket 13 makes cable for aerospace more resistant.
（3）, the present invention by setting slide bar 9, sliding block 10 and spring 15 so that sliding block 10 can be moved on slide bar 9, and
And by using the elastic reaction of spring 15, unclamp sliding block 10, reset sliding block 10, and facilitate adjustment position.
（4）, the present invention by setting rotating cylinder 5 and thread groove 6 so that the cable of Aero-Space is absorbed in the interior of thread groove 6
Portion so that the cable of Aero-Space is more stablized, makes more to stablize when winding.
It should be noted that herein, such as first and second or the like relational terms are used merely to a reality
Body or operation make a distinction with another entity or operation, and not necessarily require or imply these entities or deposited between operating
In any this actual relation or order.Moreover, term " comprising ", "comprising" or its any other variant are intended to
Nonexcludability is included, so that process, method, article or equipment including a series of key elements not only will including those
Element, but also other key elements including being not expressly set out, or also include being this process, method, article or equipment
Intrinsic key element.In the absence of more restrictions, the key element limited by sentence " including a reference structure ", is not arranged
Except also there is other identical element in the process including the key element, method, article or equipment.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of changes, modification can be carried out to these embodiments, replace without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of cable for aerospace wind, including working plate（1）, it is characterised in that：The working plate（1）Top
The left and right sides has been fixedly connected with connecting plate（2）, and two connecting plates（2）Mutually close side is connected with rotating shaft（3）,
The rotating shaft（3）Close connecting plate（2）One end be fixedly connected with mounting cup（4）, the rotating shaft（3）Surface on fixed connect
It is connected to rotating cylinder（5）, rotating cylinder（5）Surface on for concave surface set, the rotating cylinder（5）Surface on offer thread groove（6）, and
Two rotating shafts（3）Between be fixedly connected with U-board（7）, the U-board（7）Surface on be socketed with rubber ring（8）, and two
Individual connecting plate（2）Between be fixedly connected with positioned at rotating shaft（3）The slide bar of lower section（9）, the slide bar（9）Surface on be fixedly connected
There are two sliding blocks（10）, the sliding block（10）Top be fixedly connected with annulus（11）, the annulus（11）The bottom of inwall is consolidated
Surely it is connected with U-shaped block（12）, the U-shaped block（12）Inner surface on be fixedly connected with rubber blanket（13）, two sliding blocks（10）It
Between be fixedly connected with fixed plate（14）, and positioned at slide bar（9）The sliding block in left side（10）Left side be fixedly connected with spring（15）,
The spring（15）The other end and connecting plate（2）Between be fixedly connected.
2. a kind of cable for aerospace wind according to claim 1, it is characterised in that：The spring（15）Position
In slide bar（9）Outer surface on.
3. a kind of cable for aerospace wind according to claim 1, it is characterised in that：The fixed plate（14）
Length and rotating cylinder（5）Equal length.
4. a kind of cable for aerospace wind according to claim 1, it is characterised in that：The U-shaped block（12）
Quantity be 12, and six U-shaped blocks（12）For one group, every group of six U-shaped blocks（12）With annulus（11）Center be
Symmetrical centre is symmetrical arranged.
5. a kind of cable for aerospace wind according to claim 1, it is characterised in that：The rubber ring（8）
Surface on be coarse setting.
6. a kind of cable for aerospace wind according to claim 1, it is characterised in that：The thread groove（6）
Gap be two centimetres.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710584151.XA CN107150923A (en) | 2017-07-18 | 2017-07-18 | A kind of cable for aerospace wind |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710584151.XA CN107150923A (en) | 2017-07-18 | 2017-07-18 | A kind of cable for aerospace wind |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107150923A true CN107150923A (en) | 2017-09-12 |
Family
ID=59797122
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710584151.XA Pending CN107150923A (en) | 2017-07-18 | 2017-07-18 | A kind of cable for aerospace wind |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107150923A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109052008A (en) * | 2018-08-30 | 2018-12-21 | 苏州胜璟电磁科技有限公司 | A kind of electromagnet production conducting wire wind |
| CN110526029A (en) * | 2019-09-03 | 2019-12-03 | 重庆泰山电缆有限公司 | Water blocking yarn pay off rack |
| CN110790079A (en) * | 2019-11-16 | 2020-02-14 | 湖南新耒传导材料科技有限公司 | Portable cable hank device |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204615253U (en) * | 2015-05-21 | 2015-09-02 | 国网山东莱州市供电公司 | A kind of hand wire bundling device |
| CN106744001A (en) * | 2017-03-13 | 2017-05-31 | 江苏宏宝集团有限公司 | A kind of helix groove reel for condenser tube of refrigerator winding |
| CN106847428A (en) * | 2017-03-30 | 2017-06-13 | 王慧超 | A kind of waste and old cable recovering apparatus of power engineering |
| CN106865339A (en) * | 2017-04-06 | 2017-06-20 | 盐城帝佳妮服饰有限公司 | A kind of weaving roller |
-
2017
- 2017-07-18 CN CN201710584151.XA patent/CN107150923A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204615253U (en) * | 2015-05-21 | 2015-09-02 | 国网山东莱州市供电公司 | A kind of hand wire bundling device |
| CN106744001A (en) * | 2017-03-13 | 2017-05-31 | 江苏宏宝集团有限公司 | A kind of helix groove reel for condenser tube of refrigerator winding |
| CN106847428A (en) * | 2017-03-30 | 2017-06-13 | 王慧超 | A kind of waste and old cable recovering apparatus of power engineering |
| CN106865339A (en) * | 2017-04-06 | 2017-06-20 | 盐城帝佳妮服饰有限公司 | A kind of weaving roller |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109052008A (en) * | 2018-08-30 | 2018-12-21 | 苏州胜璟电磁科技有限公司 | A kind of electromagnet production conducting wire wind |
| CN110526029A (en) * | 2019-09-03 | 2019-12-03 | 重庆泰山电缆有限公司 | Water blocking yarn pay off rack |
| CN110790079A (en) * | 2019-11-16 | 2020-02-14 | 湖南新耒传导材料科技有限公司 | Portable cable hank device |
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Legal Events
| 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 | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170912 |