CN205508614U - Flying trident coiling machine walk line structure device - Google Patents

Flying trident coiling machine walk line structure device Download PDF

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Publication number
CN205508614U
CN205508614U CN201620084381.0U CN201620084381U CN205508614U CN 205508614 U CN205508614 U CN 205508614U CN 201620084381 U CN201620084381 U CN 201620084381U CN 205508614 U CN205508614 U CN 205508614U
Authority
CN
China
Prior art keywords
flying trident
motor
tensioner
synchronous pulley
wound rotor
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
Application number
CN201620084381.0U
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Chinese (zh)
Inventor
芮翔
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.)
Jiangsu Orient Printing Equipment Co Ltd
Original Assignee
Jiangsu Orient Printing Equipment 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 Jiangsu Orient Printing Equipment Co Ltd filed Critical Jiangsu Orient Printing Equipment Co Ltd
Priority to CN201620084381.0U priority Critical patent/CN205508614U/en
Application granted granted Critical
Publication of CN205508614U publication Critical patent/CN205508614U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a flying trident coiling machine walk line structure device mainly comprises wound rotor, flying trident, synchronous pulley, servo motor, tensioner, line of defence dish, step motor I, shaft coupling, ball feed table and step motor II, step motor on be equipped with the wound rotor, wound rotor the right is equipped with the flying trident, flying trident the right is equipped with servo motor, the last synchronous pulley that is equipped with of servo motor, synchronous pulley and flying trident interconnect, servo motor downside are equipped with ball feed table, ball feed table the right is equipped with the shaft coupling, the coupling joint is on step motor II, step motor II the right is equipped with the tensioner, tensioner right side downside is equipped with line of defence dish, the utility model discloses the structure connects the list, and the wire winding is stable, and production efficiency is high.

Description

The Wiring structure device of flying trident coil winding machine
Technical field
This utility model belongs to coil winding machine technical field, is specifically related to the Wiring structure device of a kind of flying trident coil winding machine.
Background technology
Flying trident coil winding machine is exactly that the object of wire is wound into the machine on specific workpiece.Current electric equipment products, need to turn to coil with copper cash or enamel-covered wire mostly.During the work of this kind of coil winding machine, generally specific workpiece is fixed on tool, and workpiece circumferentially rotates being wound on by line of moving with circumference with tool becomes coil on specific workpiece.Existing coil winding machine mostly can only to the bigger motor of some volume ratios, commutator, transformator, etc. electromagnetic component coil be wound, smaller to some components and parts, such as core coil can be had cannot to reach effective high-volume processing as the minimum of the electronic shaft core of clock and watch, utilize existing coil winding machine that minimum coil and superfine coiling are added and be easy to broken string man-hour, and winding efficiency is low, in the urgent need to the Winder that a simple in construction clamp is stable.
Utility model content
The purpose of this utility model is to provide the Wiring structure device of a kind of flying trident coil winding machine, has solved deficiency present in such scheme.
In order to achieve the above object, technical solution adopted in the utility model is:
A kind of Wiring structure device of flying trident coil winding machine, main by wound rotor, flying trident, synchronous pulley, servomotor, tensioner, anti-drum, motor I, shaft coupling, ball-screw feeding platform and motor II composition, described motor is provided with wound rotor, flying trident it is provided with on the right of wound rotor, servomotor it is provided with on the right of flying trident, servomotor is provided with synchronous pulley, synchronous pulley is connected with each other with flying trident, ball-screw feeding platform it is provided with on the downside of servomotor, it is provided with shaft coupling on the right of ball-screw feeding platform, shaft coupling is connected on motor II, it is provided with tensioner on the right of motor II, tensioner lower right side is provided with anti-drum.
It is connected with each other by guide wheel between described tensioner and anti-drum.
This utility model structure order, around line stabilization, production efficiency is high.
Accompanying drawing explanation
Fig. 1 is this utility model structural representation;
1-wound rotor;2-flying trident;3-synchronous pulley;4-servomotor;5-tensioner;The anti-drum of 6-;7-motor I;8-shaft coupling;9-ball-screw feeding platform;10-motor II.
Detailed description of the invention
The utility model is further described with detailed description of the invention below in conjunction with the accompanying drawings.
As shown in Figure 1, a kind of Wiring structure device of flying trident coil winding machine, main by wound rotor 1, flying trident 2, synchronous pulley 3, servomotor 4, tensioner 5, anti-drum 6, motor I 7, shaft coupling 8, ball-screw feeding platform 9 and motor II10 composition, described motor I 7 is provided with wound rotor 1, flying trident 2 it is provided with on the right of wound rotor 1, servomotor 4 it is provided with on the right of flying trident 2, servomotor 4 is provided with synchronous pulley 3, synchronous pulley 3 is connected with each other with flying trident 2, ball-screw feeding platform 9 it is provided with on the downside of servomotor 4, shaft coupling 8 it is provided with on the right of ball-screw feeding platform 9, shaft coupling 8 is connected on motor II 10, tensioner 5 it is provided with on the right of motor II 10, tensioner 5 lower right side is provided with anti-drum 6;It is connected with each other by guide wheel between described tensioner 5 and anti-drum 6.

Claims (2)

1. the Wiring structure device of a flying trident coil winding machine, main by wound rotor, flying trident, synchronous pulley, servomotor, tensioner, anti-drum, motor I, shaft coupling, ball-screw feeding platform and motor II composition, it is characterized in that: described motor is provided with wound rotor, flying trident it is provided with on the right of wound rotor, servomotor it is provided with on the right of flying trident, servomotor is provided with synchronous pulley, synchronous pulley is connected with each other with flying trident, ball-screw feeding platform it is provided with on the downside of servomotor, it is provided with shaft coupling on the right of ball-screw feeding platform, shaft coupling is connected on motor II, it is provided with tensioner on the right of motor II, tensioner lower right side is provided with anti-drum.
The Wiring structure device of flying trident coil winding machine the most according to claim 1, it is characterised in that: it is connected with each other by guide wheel between described tensioner and anti-drum.
CN201620084381.0U 2016-01-28 2016-01-28 Flying trident coiling machine walk line structure device Expired - Fee Related CN205508614U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620084381.0U CN205508614U (en) 2016-01-28 2016-01-28 Flying trident coiling machine walk line structure device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620084381.0U CN205508614U (en) 2016-01-28 2016-01-28 Flying trident coiling machine walk line structure device

Publications (1)

Publication Number Publication Date
CN205508614U true CN205508614U (en) 2016-08-24

Family

ID=56723191

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620084381.0U Expired - Fee Related CN205508614U (en) 2016-01-28 2016-01-28 Flying trident coiling machine walk line structure device

Country Status (1)

Country Link
CN (1) CN205508614U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106899152A (en) * 2017-04-16 2017-06-27 赵洁 A kind of copper factor round trip flight fork rotor winding machine high
CN109573724A (en) * 2018-12-07 2019-04-05 武汉普惠海洋光电技术有限公司 Coil winding machine
CN110690798A (en) * 2018-07-05 2020-01-14 上海大精电子科技有限公司 Straight strip expansion type motor winding machine
CN111302141A (en) * 2020-02-25 2020-06-19 刘晓淇 Horizontal winding machine for outer rotor of motor
CN114220652A (en) * 2022-02-21 2022-03-22 苏州智伟信自动化科技有限公司 Multi-connected hollow coil winding structure

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106899152A (en) * 2017-04-16 2017-06-27 赵洁 A kind of copper factor round trip flight fork rotor winding machine high
CN110690798A (en) * 2018-07-05 2020-01-14 上海大精电子科技有限公司 Straight strip expansion type motor winding machine
CN109573724A (en) * 2018-12-07 2019-04-05 武汉普惠海洋光电技术有限公司 Coil winding machine
CN111302141A (en) * 2020-02-25 2020-06-19 刘晓淇 Horizontal winding machine for outer rotor of motor
CN114220652A (en) * 2022-02-21 2022-03-22 苏州智伟信自动化科技有限公司 Multi-connected hollow coil winding structure

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160824

Termination date: 20190128