CN104882238B - A kind of wire resistor automatic coiling device - Google Patents

A kind of wire resistor automatic coiling device Download PDF

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Publication number
CN104882238B
CN104882238B CN201510218789.2A CN201510218789A CN104882238B CN 104882238 B CN104882238 B CN 104882238B CN 201510218789 A CN201510218789 A CN 201510218789A CN 104882238 B CN104882238 B CN 104882238B
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China
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resistance
coiling
clamping
winder
fuselage
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CN104882238A (en
Inventor
周立鸿
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Dongguan blue goose Electronic Co., Ltd.
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Dongguan Blue Goose Electronic Co Ltd
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Priority to CN201710405681.3A priority Critical patent/CN107123496B/en
Priority to CN201510218789.2A priority patent/CN104882238B/en
Publication of CN104882238A publication Critical patent/CN104882238A/en
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01CRESISTORS
    • H01C17/00Apparatus or processes specially adapted for manufacturing resistors
    • H01C17/04Apparatus or processes specially adapted for manufacturing resistors adapted for winding the resistive element

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  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Hand Tools For Fitting Together And Separating, Or Other Hand Tools (AREA)
  • Coil Winding Methods And Apparatuses (AREA)

Abstract

The present invention relates to resistance Winder field, specifically a kind of wire resistor automatic coiling device, including fuselage, resistance clamping device, Winder, clamping motor and coiling electric motor, described fuselage includes left supported plate and right supported plate, described resistance clamping device is arranged on the left supported plate of fuselage, described Winder is arranged on the right supported plate of fuselage, described clamping motor is located at resistance clamping device left side, described coiling electric motor is located at Winder right side, the effect of described resistance clamping device is to clamp different inner diameters wire resistor, the Winder carries out coiling around resistance motion using wire winding pole to resistance, multiple resistance clamping devices are installed on the left supported plate of fuselage, there is corresponding Winder to correspond therewith simultaneously.The present invention compensate for that existing resistance Winder mechanism is complex and equipment cost shortcoming high, there is provided a kind of simple structure, equipment cost are low, and once can be around the resistance Winder of multiple resistance.

Description

A kind of wire resistor automatic coiling device
Technical field
The present invention relates to resistance Winder field, specifically a kind of wire resistor automatic coiling device.
Background technology
Wirewound resistor is constituted with resistance filament winding in insulation framework.Resistance wire is typically using with certain resistivity The alloy such as nickel chromium triangle, copper-manganese be made.Insulation framework be by ceramics, plastics, apply insulating layer coating the material such as metal be made it is tubular, flat Shape etc. is variously-shaped.Resistance wire on skeleton as needed can with one layer of coiling, also can coiling multilayer, or use noninductive winding Deng present invention is generally directed to the Winding Design of tubular dielectric skeleton.
The Winder of existing resistor coiling machine, generallys include a transmission group being connected with cursor and a coiling stepping horse Reach, transmission group is engaged by the threaded axostylus axostyle of tool with thread slider and coiling stepper motor;And micro computer master control system System, has generally included:CPU, memory module, input/output interface module, when m- tally control module, Input driver module and output driver module, the relation of above-mentioned each module are total by address bus, data/address bus and control Line, interconnects.
Although above-mentioned resistance Winder coiling effect is good, mechanism is complex, and equipment cost is higher, is not suitable for Small Cost Management, in consideration of it, the invention provides a kind of simple structure, equipment cost is low, and once can be around the one of multiple resistance Plant wire resistor automatic coiling device.
The content of the invention
In order to make up the deficiencies in the prior art, the invention provides a kind of wire resistor automatic coiling device, it compensate for Existing resistance Winder mechanism is complex and equipment cost shortcoming high, there is provided a kind of simple structure, equipment cost are low, And once can be around the resistance Winder of multiple resistance.
The technical solution adopted for the present invention to solve the technical problems is:A kind of wire resistor automatic coiling device, including Fuselage, resistance clamping device, Winder, clamping motor and coiling electric motor, described fuselage include left supported plate and right supported plate, institute The resistance clamping device stated is arranged on the left supported plate of fuselage, and described Winder is arranged on the right supported plate of fuselage, described Clamping motor be located at resistance clamping device left side, described coiling electric motor is located at Winder right side.
Described resistance clamping device includes screw rod, swivel nut, rotating mechanism and clamping gear, and described screw rod left side is fixed On left supported plate, screw rod right side is located at waist, and screw rod right side causes wire resistor when being located at the purpose of waist One end can penetrate resistance clamping device from fuselage left side, and screw rod right side is provided with cylindrical boss, described swivel nut and spiral shell Bar be intermeshed, during work, screw rod rotate cause swivel nut moved forward and backward on screw rod, described rotating mechanism be divided into left-hand rotation bar and Right-hand rotation bar, left-hand rotation bar left end is hinged with swivel nut, and right-hand rotation bar right-hand member is hinged with boss, and left-hand rotation bar middle part and right-hand rotation bar middle part It is hinged, and screw rod is uniformly provided with three rotating mechanisms along axis, during work, swivel nut is moved forward and backward, left-hand rotation bar and right-hand rotation bar Around hinge is mutually rotated, and is enclosed within the wire resistor on the outside of screw rod and is maintained static from inside is clamped in the presence of rotating mechanism, According to the difference of wire resistor internal diameter, the rotational angle of rotating mechanism is different, and described clamping gear is fixedly connected with screw rod, and folder Gear is held positioned at left supported plate left side, described clamping gear left side is installed with belt pulley, and described clamping motor passes through skin Band is connected with clamping gear, and clamping motor is fixedly mounted on ground by anchor (bolt) hole, and during work, clamping motor is rotated Clamping pinion rotation is driven, so that drive the screw rod being fixedly connected with clamping gear to rotate, and then band movable snail sleeve controls rotating mechanism Motion, clamp the purpose of different inner diameters wire resistor to reach, the effect of the resistance clamping device be by different inner diameters around Line resistance is fixed on fuselage.
Described Winder includes rotating shaft, coiling disk, wire winding pole and the fixed peace in the middle part of line gear, described rotating shaft On right supported plate, and rotating shaft and resistance clamping device the screw coaxial heart, the center of circle phase of rotating shaft left end face and coiling disk Be connected, described wire winding pole is oval mast, wire winding pole right side is fixedly connected with coiling disk left side edge, wire winding pole and screw rod it Between be spaced in more than 20 centimetres such that it is able to meet most wire resistors and be enclosed within when on screw rod, wire winding pole still with coiling electricity Resistance outer wall is at regular intervals so that wire winding pole can carry out next step coiling work, wire winding pole left side apart from fuselage left supported plate one to Two centimetres, during work, the resistive conductor of required winding is wound on wire winding pole in advance, then by wire winding pole around wire resistor Circular-rotation is done, so as to resistive conductor is wrapped on wire resistor, described rotating shaft right side is fixed with around line gear, around line gear Right side is installed with belt pulley, and described coiling electric motor is connected by belt with around line gear, and coiling electric motor is by ground Bolt holes are fixedly mounted on ground, during work, coiling electric motor rotate drive coiling pinion rotation, coiling pinion rotation drive around Line disk rotational, so that drive the wire winding pole for being connected in coiling disk border to be rotated around wire resistor outer wall, by resistive conductor It is wrapped on wire resistor, the Winder makes of being to carry out coiling work to the wire resistor being fixed on resistance clamping device Make.
Described resistance clamping device is at least uniformly provided with five along the left supported plate of fuselage, and resistance clamping device with around Line apparatus are corresponded, and are intermeshed between each clamping gear, are respectively intermeshed between line gear, during work, a clamping Pinion rotation drives each clamping pinion rotation, so as to drive each resistance clamping device to work, is enclosed within each resistance clamping device Wire resistor is clamped, and a coiling pinion rotation drives each coiling pinion rotation, so that drive each Winder to work, with Coiling work is carried out to the resistance on corresponding resistance clamping device, the purpose of above-mentioned design is so that invention can be simultaneously right Multiple resistance carry out coiling work.
The present invention is rotated using screw rod rotational band movable snail sleeve, and then clamps wire resistor, is transported around resistance using wire winding pole It is dynamic to carry out coiling, it is the relatively existing resistor coiling machine simple structure of the present invention, with low cost and once can be around multiple resistance, coiling Efficiency is preferable.
Brief description of the drawings
The present invention is further described with implementation method below in conjunction with the accompanying drawings.
Fig. 1 is structural representation of the invention;
Fig. 2 is the structural representation of resistance clamping device of the invention;
Fig. 3 is the structural representation of Winder of the invention;
Fig. 4 is resistance clamping device of the invention and corresponding Winder position relationship schematic diagram;
Fig. 5 is multiple resistance clamping device dimensional structure diagrams of the invention;
Fig. 6 is multiple Winder dimensional structure diagrams of the invention.
In figure:Fuselage 1, resistance clamping device 2, Winder 3, clamping motor 4, coiling electric motor 5, left supported plate 11, right branch Plate 12, screw rod 21, swivel nut 22, rotating mechanism 23, clamping gear 24, cylindrical boss 211, left-hand rotation bar 231, right-hand rotation bar 232, turn Axle 31, coiling disk 32, wire winding pole 33, around line gear 34.
Specific embodiment
In order that technological means, creation characteristic, reached purpose and effect that the present invention is realized are easy to understand, tie below Conjunction is specifically illustrating, and the present invention is expanded on further.
As shown in figure 1, a kind of wire resistor automatic coiling device of the present invention, including fuselage 1, resistance clamping device 2nd, Winder 3, clamping motor 4 and coiling electric motor 5, described fuselage 1 include left supported plate 11 and right supported plate 12, described resistance Clamping device 2 is arranged on the left supported plate 11 of fuselage 1, and described Winder 3 is arranged on the right supported plate 12 of fuselage 1, described Clamping motor 4 be located at the left side of resistance clamping device 2, described coiling electric motor 5 is located at the right side of Winder 3.
As depicted in figs. 1 and 2, a kind of wire resistor automatic coiling device of the present invention, described resistance clamping dress Putting 2 includes screw rod 21, swivel nut 22, rotating mechanism 23 and clamping gear 24, and the described left side of screw rod 21 is fixedly mounted on left supported plate On 11, the right side of screw rod 21 is located at the middle part of fuselage 1, and the right side of screw rod 21 causes wire resistor one end when being located at the purpose at the middle part of fuselage 1 Resistance clamping device 2 can be penetrated from the left side of fuselage 1, and the right side of screw rod 21 is provided with cylindrical boss 211, described swivel nut 22 It is intermeshed with screw rod 21, during work, screw rod 21 is rotated and causes that swivel nut 22 is moved forward and backward on screw rod 21, described rotating mechanism 23 points is left-hand rotation bar 231 and right-hand rotation bar 232, and the left end of left-hand rotation bar 231 is hinged with swivel nut 22, the right-hand member of right-hand rotation bar 232 and boss 211 It is hinged, and the middle part of left-hand rotation bar 231 is hinged with the middle part of right-hand rotation bar 232, and screw rod 21 is uniformly provided with three rotations along axis Mechanism 23, during work, swivel nut 22 is moved forward and backward, and left-hand rotation bar 231 is mutually rotated with the around hinge of right-hand rotation bar 232, is enclosed within outside screw rod 21 The wire resistor of side is clamped from inside in the presence of rotating mechanism 23 and maintains static, according to the difference of wire resistor internal diameter, The rotational angle of rotating mechanism 23 is different, and described clamping gear 24 is fixedly connected with screw rod 21, and clamping gear 24 is located at left branch The left side of plate 11, the described left side of clamping gear 24 is installed with belt pulley, and described clamping motor 4 passes through belt and clamping tooth Wheel 24 is connected, and clamping motor 4 is fixedly mounted on ground by anchor (bolt) hole, and during work, clamping motor 4 is rotated and drives folder Gear 24 is held to rotate, so that drive the screw rod 21 being fixedly connected with clamping gear 24 to rotate, and then band movable snail sleeve 22 controls rotating machine The motion of structure 23, the purpose of different inner diameters wire resistor is clamped to reach, and the effect of the resistance clamping device 2 is by different inner diameters Wire resistor fix on the fuselage 1.
As shown in figures 1 and 3, a kind of wire resistor automatic coiling device of the present invention, described Winder 3 is wrapped Include rotating shaft 31, coiling disk 32, wire winding pole 33 and be fixedly mounted on right supported plate 12 in the middle part of line gear 34, described rotating shaft 31 On, and rotating shaft 31 is concentric with the screw rod 21 of resistance clamping device 2, the left end face of rotating shaft 31 is mutually solid with the center of circle of coiling disk 32 Even, described wire winding pole 33 is oval mast, and the right side of wire winding pole 33 is fixedly connected with the left side edge of coiling disk 32, wire winding pole 33 and More than 20 centimetres are spaced between screw rod 21 such that it is able to meet most wire resistors and be enclosed within when on screw rod 21, wire winding pole 33 is still at regular intervals with wire resistor outer wall so that wire winding pole can carry out next step coiling work, the left side distance of wire winding pole 33 11 one to two centimetres of 1 left supported plate of fuselage, during work, the resistive conductor of required winding is wound on wire winding pole 33 in advance, then by around Line bar 33 does circular-rotation around wire resistor, and so as to resistive conductor is wrapped on wire resistor, described rotating shaft 31 is right Side is fixed with around line gear 34, and belt pulley is installed with around the right side of line gear 34, described coiling electric motor 5 by belt with around Line gear 34 is connected, and coiling electric motor 5 is fixedly mounted on ground by anchor (bolt) hole, during work, the rotational band of coiling electric motor 5 It is dynamic to be rotated around line gear 34, rotated around line gear 34 and drive coiling disk 32 to rotate, so as to drive be connected in the side of coiling disk 32 The wire winding pole 33 of edge is rotated around wire resistor outer wall, and resistive conductor is wrapped on wire resistor, and the Winder 3 does use It is that coiling work is carried out to the wire resistor being fixed on resistance clamping device 2.
As shown in Fig. 1, Fig. 4, Fig. 5 and Fig. 6, a kind of wire resistor automatic coiling device of the present invention, described electricity Resistance clamping device 2 is at least uniformly provided with five along the left supported plate 11 of fuselage 1, and resistance clamping device 2 is with Winder 3 one by one Correspondence, is intermeshed between each clamping gear 24, is respectively intermeshed between line gear 34, during work, a clamping gear 24 Rotate and drive each clamping gear 24 to rotate, so as to drive each resistance clamping device 2 to work, be enclosed within each resistance clamping device 2 Wire resistor is clamped, and one rotates drive and respectively rotated around line gear 34 around line gear 34, so as to drive the work of each Winder 3 Make, to carry out coiling work to the resistance on corresponding resistance clamping device 2, the purpose of above-mentioned design is so that invention can Coiling work is carried out to multiple resistance simultaneously.
During work, first be uniformly wrapped in each resistive conductor on the wire winding pole 33 of Winder 3 by workman, resistive conductor right-hand end Portion is fastened on wire winding pole 33, and then wire resistor is enclosed within resistance clamping device 2, and afterwards, resistance clamping device 2 works.
When resistance clamping device 2 works, clamping motor 4 is rotated and drives clamping tooth wheel 24 to rotate, so as to drive and clamping tooth The screw rods 21 that are fixedly connected with of wheel 24 are rotated, the rotational band movable snail sleeve 22 of screw rod 21 is moved forward and backward, and swivel nut 22 is moved forward and backward so that turned left Bar 231 is mutually rotated with the around hinge of right-hand rotation bar 232, be enclosed within the wire resistor in the outside of screw rod 21 in the presence of rotating mechanism 23 from Inside is clamped and maintains static, and according to the difference of wire resistor internal diameter, the rotational angle of rotating mechanism 23 is different, to reach clamping The purpose of different inner diameters wire resistor, meanwhile, a clamping gear 24 is rotated and drives each clamping gear 24 to rotate, so that each resistance Clamping device 2 works to clamp wire resistor, and after clamping wire resistor, workman is by the resistive conductor left end on wire winding pole 33 Tie up to wire resistor left end.
Then, Winder 3 is worked, and coiling electric motor 5 is rotated and drives coiling gear 34 to rotate, and is rotated around line gear 34 and driven Coiling disk 32 is rotated, so that drive the wire winding pole 33 for being connected in the edge of coiling disk 32 to be rotated around wire resistor outer wall, with Resistive conductor is from left to right wrapped on wire resistor, meanwhile, one rotates drive and is respectively rotated around line gear 34 around line gear 34, Carry out coiling with to wire resistor so as to each Winder 3 works.
The basic principles, principal features and advantages of the present invention have been shown and described above.The technical staff of the industry should Understand, the present invention is not limited to the above embodiments, the description in above-described embodiment and specification is to illustrate of the invention Principle, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, and these change and change Enter all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appending claims and its equivalent Define.

Claims (3)

1. a kind of wire resistor automatic coiling device, including fuselage (1), resistance clamping device (2), Winder (3), clamping electricity Machine (4) and coiling electric motor (5), it is characterised in that:Described fuselage (1) includes left supported plate (11) and right supported plate (12), described Resistance clamping device (2) on the left supported plate (11) of fuselage (1), the right side of described Winder (3) installed in fuselage (1) On support plate (12), positioned at resistance clamping device (2) left side, described coiling electric motor (5) is positioned at coiling for described clamping motor (4) Device (3) right side;Wherein:
Described resistance clamping device (2) includes screw rod (21), swivel nut (22), rotating mechanism (23) and clamping gear (24), institute Screw rod (21) left side stated is fixedly mounted on left supported plate (11), and screw rod (21) right side is located at fuselage (1) middle part, and screw rod (21) Right side is provided with cylindrical boss (211), and described swivel nut (22) is intermeshed with screw rod (21), described rotating mechanism (23) It is divided into left-hand rotation bar (231) and right-hand rotation bar (232), left-hand rotation bar (231) left end is hinged with swivel nut (22), right-hand rotation bar (232) right-hand member It is hinged with boss (211), and left-hand rotation bar (231) middle part is hinged with right-hand rotation bar (232) middle part, and screw rod (21) is equal along axis Even to be provided with three rotating mechanisms (23), described clamping gear (24) is fixedly connected with screw rod (21), and clamping gear (24) position In left supported plate (11) left side, described clamping gear (24) left side is installed with belt pulley, and described clamping motor (4) passes through Belt is connected with clamping gear (24), and clamping motor (4) is fixedly mounted on ground by anchor (bolt) hole.
2. a kind of wire resistor automatic coiling device according to claim 1, it is characterised in that:Described Winder (3) including rotating shaft (31), coiling disk (32), wire winding pole (33) and the fixation in the middle part of line gear (34), described rotating shaft (31) On right supported plate (12), and rotating shaft (31) is concentric with the screw rod (21) of resistance clamping device (2), rotating shaft (31) left-hand end Face is fixedly connected with the center of circle of coiling disk (32), and described wire winding pole (33) is oval mast, wire winding pole (33) right side and coiling Disk (32) left side edge is mutually solid, and even apart from (11) one to two centimetres of fuselage (1) left supported plate, described turns in wire winding pole (33) left side Axle (31) right side is fixed with around line gear (34), and belt pulley, described coiling electric motor are installed with around line gear (34) right side (5) it is connected with around line gear (34) by belt, and coiling electric motor (5) is fixedly mounted on ground by anchor (bolt) hole.
3. a kind of wire resistor automatic coiling device according to claim 1, it is characterised in that:Described resistance clamping dress Put (2) and five, and resistance clamping device (2) and Winder (3) are at least uniformly installed along the left supported plate (11) of fuselage (1) One correspondence, respectively clamps intermeshing between gear (24), is respectively intermeshed between line gear (34).
CN201510218789.2A 2015-05-01 2015-05-01 A kind of wire resistor automatic coiling device Active CN104882238B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201710405681.3A CN107123496B (en) 2015-05-01 2015-05-01 A kind of method for winding of wire resistor automatic coiling device
CN201510218789.2A CN104882238B (en) 2015-05-01 2015-05-01 A kind of wire resistor automatic coiling device

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Application Number Priority Date Filing Date Title
CN201510218789.2A CN104882238B (en) 2015-05-01 2015-05-01 A kind of wire resistor automatic coiling device

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CN104882238B true CN104882238B (en) 2017-07-07

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CN201710405681.3A Expired - Fee Related CN107123496B (en) 2015-05-01 2015-05-01 A kind of method for winding of wire resistor automatic coiling device

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111462973B (en) * 2020-05-21 2020-12-29 温州骐铭电子设备有限公司 Resistor winding machine for electronic component

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Publication number Priority date Publication date Assignee Title
US5806782A (en) * 1997-06-13 1998-09-15 U Gear Automatic Machinery Co., Ltd. Double track wire arranging device for winding machines
CN201369200Y (en) * 2008-11-18 2009-12-23 成都承宏机电有限公司 Precision parallel winding machine
CN202678015U (en) * 2012-06-01 2013-01-16 张家港市泓溢电源科技有限公司 Coiling device for special resistor board
CN203644489U (en) * 2013-10-18 2014-06-11 蚌埠市微欧电子科技有限责任公司 Novel resistor winder
CN204695896U (en) * 2015-05-01 2015-10-07 安庆安星电气有限公司 A kind of wire resistor automatic coiling device

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0590015A (en) * 1991-09-27 1993-04-09 Mitsunori Yokoyama Automatic resistance-wire winding machine
CN201590297U (en) * 2009-12-31 2010-09-22 刘德鸿 Coaxial winding device of high-pressure ignition wire core
CN102915817B (en) * 2012-10-30 2015-08-19 深圳市华力特电气股份有限公司 A kind of cylindrically coiled spring shape resistive element automatic assembly equipment

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5806782A (en) * 1997-06-13 1998-09-15 U Gear Automatic Machinery Co., Ltd. Double track wire arranging device for winding machines
CN201369200Y (en) * 2008-11-18 2009-12-23 成都承宏机电有限公司 Precision parallel winding machine
CN202678015U (en) * 2012-06-01 2013-01-16 张家港市泓溢电源科技有限公司 Coiling device for special resistor board
CN203644489U (en) * 2013-10-18 2014-06-11 蚌埠市微欧电子科技有限责任公司 Novel resistor winder
CN204695896U (en) * 2015-05-01 2015-10-07 安庆安星电气有限公司 A kind of wire resistor automatic coiling device

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CN107123496A (en) 2017-09-01
CN104882238A (en) 2015-09-02
CN107123496B (en) 2018-09-18

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