CN206991841U - A kind of all-wing aircraft mechanism of concentric lay conductor machine - Google Patents
A kind of all-wing aircraft mechanism of concentric lay conductor machine Download PDFInfo
- Publication number
- CN206991841U CN206991841U CN201720450778.1U CN201720450778U CN206991841U CN 206991841 U CN206991841 U CN 206991841U CN 201720450778 U CN201720450778 U CN 201720450778U CN 206991841 U CN206991841 U CN 206991841U
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- CN
- China
- Prior art keywords
- wing aircraft
- solid wire
- dancing wheel
- main shaft
- lay conductor
- 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.)
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Abstract
The utility model discloses a kind of all-wing aircraft mechanism of concentric lay conductor machine, it is arranged on the main shaft of concentric lay conductor machine, the main shaft is provided with two rewind discs, the all-wing aircraft mechanism includes six all-wing aircraft arms being distributed centered on the main shaft, each all-wing aircraft arm is provided with the dancing wheel for alignment buffer tension variation, directly surrounded correspondingly by the dancing wheel on six all-wing aircraft arms by the six roots of sensation solid wire released on two rewind discs, the dancing wheel is driven by motor and swung, the motor can control the swing angle of the dancing wheel according to the tension variation of the solid wire, so that the tension stability of the solid wire.It is arranged such, the all-wing aircraft mechanism of concentric lay conductor machine provided by the utility model, it can avoid the friction between line and line, the problem of avoiding cabling not smooth.
Description
Technical field
Wire twisting equipment technical field is the utility model is related to, more specifically to a kind of wingflying aircraft of concentric lay conductor machine
Structure.
Background technology
Two disk storage lines are usually mounted with concentric lay conductor owner axle of the prior art, are distinguished simultaneously on two disk storage lines
Release three wires, it is generally the case that all-wing aircraft mechanism of the prior art has two all-wing aircraft arm configurations, each all-wing aircraft arm configuration
On be designed with guide roller group, and each disk storage line is corresponding with an all-wing aircraft arm configuration, i.e., three released on each disk storage line
Root wire exports around the guide roller group of corresponding all-wing aircraft arm configuration simultaneously.
So, all-wing aircraft mechanism of the prior art it is unilateral walk three lines, three lines are twisted from group guide wheel export simultaneously
Close, because three lines have length variation phenomenon, in order to be compensated to the length phenomenon of solid wire, concentric lay conductor of the prior art
Machine is typically provided with wire storage device.
Solid wire is released, after wire storage device by all-wing aircraft arm, then is twisted, because solid wire needs in the prior art
To be wound repeatedly in wire storage device, solid wire, which is crossed, to be bent through more, and large effect is caused to the quality of wire rod.In addition, storage
Guide wheel on line apparatus sets more, causes compact-sized complexity, cabling space is smaller.
In order to overcome above mentioned problem, a kind of brand-new all-wing aircraft mechanism is devised in the prior art, i.e., all-wing aircraft mechanism is set
Six all-wing aircraft arms, be designed with guide roller group on each all-wing aircraft arm, by each solid wire for being released on rewind disc respectively after-combustion to
In the guide roller group of different all-wing aircraft arms, i.e., the guide roller group of each all-wing aircraft arm bypasses a solid wire.
In addition, straining pulley is designed with each all-wing aircraft arm, and straining pulley is slidably disposed on directly by support shaft
On line guide rail, elastic component is supported between all-wing aircraft arm and support shaft, when the single line tension on around straining pulley changes,
The balance of elastic component and single line tension changes, and elastic component drives support shaft to be led along straight line under the elastic force effect of elastic component
Rail is slided, to reach new balance, and the length of line is can compensate for when straining pulley moves.It is arranged such, it is not necessary to which storage line is set
Device, you can compensated to the length of solid wire.
However, this kind of all-wing aircraft mechanism of the prior art, during disk storage line unwrapping wire, three wires of releasing first pass around same
Organize guide wheel and then be separately dispensed on each all-wing aircraft arm.This kind of scheme, if three wire emitting rates on disk storage line differ
Cause, the friction between line and line can be caused, the problem of causing cabling to have some setbacks.
Therefore, how to solve all-wing aircraft mechanism of the prior art, easily cause the friction between line and line and cabling has some setbacks
The problem of smooth, turn into those skilled in the art's important technological problems to be solved.
Utility model content
In view of this, the purpose of this utility model is to provide a kind of all-wing aircraft mechanism of concentric lay conductor machine, and it can be avoided
Friction between line and line, the problem of avoiding cabling not smooth.
A kind of all-wing aircraft mechanism of concentric lay conductor machine provided by the utility model, is arranged on the main shaft of concentric lay conductor machine, institute
State main shaft and be provided with two rewind discs, the all-wing aircraft mechanism includes six all-wing aircraft arms being distributed centered on the main shaft, each
The all-wing aircraft arm is provided with the dancing wheel for alignment buffer tension variation, by the six roots of sensation solid wire released on two rewind discs
Directly surround correspondingly and driven and swung by motor by the dancing wheel on six all-wing aircraft arms, the dancing wheel,
The motor can control the swing angle of the dancing wheel according to the tension variation of the solid wire, so that the solid wire
Tension stability.
In technical scheme provided by the utility model, all-wing aircraft mechanism is set into six all-wing aircraft arms, set on each all-wing aircraft arm
There is dancing wheel, by each solid wire for being released on rewind disc directly on the dancing wheel on corresponding all-wing aircraft arm.By
In technical scheme provided by the utility model, dancing wheel is designed with each all-wing aircraft arm, motor can drive dancing wheel to carry out
Swing, to change the power that dancing wheel is pressed on solid wire, and then the tension force of solid wire can be controlled.In addition, with the prior art
Unlike, all-wing aircraft mechanism provided by the utility model, needed not move through after being released due to three lines on rewind disc same
Guide wheel group is assigned on each all-wing aircraft arm again after releasing, in this way, the problem of avoiding friction and the not smooth cabling between line and line.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only
It is some embodiments of the utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is the partial schematic diagram of concentric lay conductor machine in the utility model embodiment；
In Fig. 1：
Main shaft -11, all-wing aircraft mechanism -12, rewind disc -13.
Embodiment
The purpose of present embodiment is to provide a kind of concentric lay conductor machine, and it can avoid storage line of the prior art
The problem of device causes to adversely affect single line mass, and the less problem of cabling space.
Hereinafter, embodiment is illustrated referring to the drawings.In addition, embodiments illustrated below is not to described in claim
Utility model content rise any restriction effect.In addition, the full content of the composition represented by example below is not limited to conduct
Necessary to the solution of utility model described in claim.
It refer to Fig. 1, a kind of concentric lay conductor machine that present embodiment provides, including main shaft 11, it is fixedly installed on master
All-wing aircraft mechanism 12 on axle 11 and the rewind disc 13 being arranged on by bearing on main shaft 11.
In the present embodiment, all-wing aircraft mechanism 12 includes six all-wing aircraft arms being distributed centered on main shaft 11, on each all-wing aircraft arm
It is direct correspondingly by the six roots of sensation solid wire released on two rewind discs 13 provided with the dancing wheel for alignment buffer tension variation
The dancing wheel being passed around on six all-wing aircraft arms, dancing wheel are driven by motor and swung, and motor can become according to the tension force of solid wire
Change the swing angle of control dancing wheel, so that the tension stability of solid wire.
It is arranged such, in the technical scheme that the present embodiment provides, all-wing aircraft mechanism 12 is set into six all-wing aircraft arms, each all-wing aircraft
Dancing wheel is designed with arm, by the dance of each solid wire for being released on rewind disc 13 directly on corresponding all-wing aircraft arm
Step on wheel.Due in technical scheme provided by the utility model, dancing wheel is designed with each all-wing aircraft arm, motor can drive dance
Step wheel to be swung, to change the power that dancing wheel is pressed on solid wire, and then the tension force of solid wire can be controlled.In addition, with showing
Unlike having in technology, all-wing aircraft mechanism 12 provided by the utility model, after being released due to three lines on rewind disc 13 not
Need to assign to again on each all-wing aircraft arm after same guide wheel group is released, in this way, avoiding the friction between line and line and walking
The problem of line is not smooth.
The foregoing description of the disclosed embodiments, professional and technical personnel in the field are enable to realize or new using this practicality
Type.A variety of modifications to these embodiments will be apparent for those skilled in the art, determine herein
The General Principle of justice can be realized in other embodiments in the case where not departing from spirit or scope of the present utility model.Cause
This, the utility model is not intended to be limited to the embodiments shown herein, and is to fit to and principles disclosed herein
The most wide scope consistent with features of novelty.
Claims (1)
1. a kind of all-wing aircraft mechanism of concentric lay conductor machine, is arranged on the main shaft of concentric lay conductor machine, the main shaft is provided with two again
Drum, it is characterised in that the all-wing aircraft mechanism includes six all-wing aircraft arms being distributed centered on the main shaft, each all-wing aircraft
Arm is provided with the dancing wheel for alignment buffer tension variation, is corresponded by the six roots of sensation solid wire released on two rewind discs
Ground, which directly surrounds, to be driven by motor and swung by the dancing wheel on six all-wing aircraft arms, the dancing wheel, the motor
The swing angle of the dancing wheel can be controlled according to the tension variation of the solid wire, so that the tension force of the solid wire is steady
It is fixed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720450778.1U CN206991841U (en) | 2017-04-26 | 2017-04-26 | A kind of all-wing aircraft mechanism of concentric lay conductor machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720450778.1U CN206991841U (en) | 2017-04-26 | 2017-04-26 | A kind of all-wing aircraft mechanism of concentric lay conductor machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206991841U true CN206991841U (en) | 2018-02-09 |
Family
ID=61393045
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720450778.1U Expired - Fee Related CN206991841U (en) | 2017-04-26 | 2017-04-26 | A kind of all-wing aircraft mechanism of concentric lay conductor machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206991841U (en) |
-
2017
- 2017-04-26 CN CN201720450778.1U patent/CN206991841U/en not_active Expired - Fee Related
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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: 20200426 |
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| CF01 | Termination of patent right due to non-payment of annual fee |