CN207581889U - A kind of copper wire processing annealing device - Google Patents
A kind of copper wire processing annealing device Download PDFInfo
- Publication number
- CN207581889U CN207581889U CN201721367930.6U CN201721367930U CN207581889U CN 207581889 U CN207581889 U CN 207581889U CN 201721367930 U CN201721367930 U CN 201721367930U CN 207581889 U CN207581889 U CN 207581889U
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- CN
- China
- Prior art keywords
- copper wire
- wire processing
- annealing device
- fuselage
- end cap
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Abstract
The utility model discloses a kind of copper wire processing annealing devices,Including fuselage cover and firm banking,The top both sides of the firm banking are symmetrically installed with connection column,Bearing block is installed above the connection column,The bearing block is internally provided with fixing axle,The outer symmetrical of the fixing axle is arranged with driving gear,One of them described driving gear is connected with motor gear by gear teeth meshing,The motor gear is rotatably connected to servo motor by shaft,The servo motor is bolted to connection with firm banking,The utility model offers sliding slot in the inside of fuselage cover,And heating room is slidably connected by heating the sliding rail of outdoor with sliding slot,It can be skidded off by handle by room is heated from fuselage enclosure,It is convenient that inside is repaired when the present apparatus breaks down,And can room be heated by removal and the inside of the present apparatus is cleared up,Prevent internal dust from excessively influencing the efficiency of annealing.
Description
Technical field
The utility model belongs to copper wire processing technique field, and in particular to a kind of copper wire processing annealing device.
Background technology
Copper wire is heated slowly to certain temperature by copper wire annealing, keeps enough time, is then cooled down (usually with Reasonable Speed
Slow cooling, sometimes control cooling) a kind of copper wire heat treatment process.Purpose is to make by casting, forging rolling, weld or cut
The copper wire softening of processing is cut, improves plasticity and toughness, homogenizes chemical composition, residual stress is removed or obtains expected object
Rationality energy, annealing process with the difference of purpose there are many, as full annealed, isothermal annealing, homogenizing annealing, nodularization are moved back
Fire, removal stress annealing, recrystallization annealing and stabilizing annealing, magnetic-field annealing etc..
There are some defects, such as annealing device in use to be inconvenient to tear open for copper wire annealing device currently on the market
It unloads, repairs and clear up difficult and annealing device internal copper wire in annealing process and be difficult to thermally equivalent, easily influence copper wire
Quality.
Utility model content
The purpose of this utility model is to provide a kind of copper wire processing annealing device, to solve to carry in above-mentioned background technology
The annealing device gone out is inconvenient to dismantle, and repair and cleaning difficulty and the annealing device internal copper wire in annealing process are difficult to
It is even heated, easily the problem of the quality of influence copper wire.
To achieve the above object, the utility model provides following technical solution：A kind of copper wire processing annealing device, including
Fuselage cover and firm banking, the top both sides of the firm banking are symmetrically installed with connection column, the connection column
Top is equipped with bearing block, and the bearing block is internally provided with fixing axle, and the outer symmetrical of the fixing axle is arranged with actively
Gear, one of them described driving gear are connected with motor gear by gear teeth meshing, and the motor gear is rotated by shaft
Servo motor is connected with, the servo motor is bolted to connection with firm banking, close to even above the firm banking
The side for connecing column is equipped with AT89S52 controllers.
Preferably, the outside of the fuselage cover is provided with insulating layer, and the both sides external of the insulating layer is symmetrically installed with
Annular rack, two annular racks are connect with driving gear by gear teeth meshing, the inside setting of the fuselage cover
There is support base, the inner homogeneous of the support base is opened up there are four sliding slot, and the sliding slot slidably connects heating room by sliding rail.
Preferably, the inside installation of the heating room is uniformly equipped with electrically heated rod, and heats being internally provided with for room and move back
Fiery chamber, the heating room both sides are fixedly connected by fixed link with the connecting rod inside anneal chamber, the both ends of the connecting rod
Handle is mounted on, and the outer symmetrical of connecting rod is equipped with partition board.
Preferably, the fuselage cover is rotatably connected to end cap by hinge, and the inside of the end cap is equipped with windowpane,
And the side far from fuselage cover is provided with end cap fixed seat on end cap, the side of the end cap fixed seat is equipped with fixed column.
Preferably, the side far from end cap is equipped with fuselage fixed seat on the fuselage cover, the fuselage fixed seat
Inside offers mounting hole.
Preferably, the length of the fixed link is twice of the length of partition board.
Preferably, the servo motor and electrically heated rod are electrically connected with AT89S52 controllers.
The utility model compared with prior art, has the advantages that：
(1) the utility model offers sliding slot in the inside of fuselage cover, and heats room by heating the sliding rail of outdoor
It is slidably connected, can be skidded off room is heated from fuselage enclosure by handle with sliding slot, it is convenient when the present apparatus breaks down
Inside is repaired, and can room be heated by removal and the inside of the present apparatus is cleared up, prevents the excessive shadow of internal dust
Ring the efficiency to annealing.
(2) the utility model is fixedly connected with connecting rod, the both sides peace of connecting rod in the inside of anneal chamber by fixed link
Equipped with partition board, the present apparatus can be made to drive the movement of internal copper wire rule while rotation, allow internal copper wire uniformly by
Heat improves the effect of annealing.
Description of the drawings
Fig. 1 is the structure diagram of the utility model；
Fig. 2 is the front view of the utility model；
Fig. 3 is the partial structural diagram of the utility model；
In figure：1- end caps fixed seat, 2- fixed columns, 3- end caps, 4- windowpanes, 5- insulating layers, 6- sliding slots, 7- annular tooths
Item, 8- fuselage covers, 9- sliding rails, 10- fuselages fixed seat, 11- mounting holes, 12- support bases, 13- bearing blocks, 14- fixing axles,
15- connections column, 16- firm bankings, 17- servo motors, 18- heating room, 19- electrically heated rods, 20- fixed links, 21- handles,
22- partition boards, 23-AT89S52 controllers, 24- motor gears, 25- driving gears, 26- anneal chambers, 27- connecting rods.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
It clearly and completely describes, it is clear that the described embodiments are only a part of the embodiments of the utility model rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are without making creative work
All other embodiments obtained shall fall within the protection scope of the present invention.
- 3 are please referred to Fig.1, the utility model provides a kind of technical solution：A kind of copper wire processing annealing device, including machine
Body shell 8 and firm banking 16, the top both sides of firm banking 16 are symmetrically installed with connection column 15, connect the upper of column 15
Side is equipped with bearing block 13, and bearing block 13 is internally provided with fixing axle 14, and the outer symmetrical of fixing axle 14 is arranged with driving tooth
Wheel 25, one of driving gear 25 are connected with motor gear 24 by gear teeth meshing, and the rotation of motor gear 24 passes through gear teeth band
Dynamic driving gear 25 rotates, and motor gear 24 is rotatably connected to servo motor 17, servo motor 17 and firm banking by shaft
16 are bolted to connection, and 16 top of firm banking is equipped with AT89S52 controllers 23 close to the side of connection column 15, uses
In control present apparatus normal work.
Further, the outside of fuselage cover 8 is provided with insulating layer 5, can anti-locking apparatus internal heat scatter and disappear, improve energy
The utilization rate in source, the both sides external of insulating layer 5 are symmetrically installed with annular rack 7, and two annular racks 7 are logical with driving gear 25
Gear teeth meshing connection is crossed, the rotation of driving gear 25 drives fuselage cover 8 to rotate by annular rack 7, and the inside of fuselage cover 8 is set
Support base 12 is equipped with, the inner homogeneous of support base 12 is opened up there are four sliding slot 6, and sliding slot 6 slidably connects heating room by sliding rail 9
18, sliding slot 6 and sliding rail 9 can heat room 18 in order to take out inside.
Further, the inside installation of heating room 18 is uniformly equipped with electrically heated rod 19, for adding to the present apparatus
Heat, raising annealing required temperature, and heating room 18 are internally provided with anneal chamber 26, for placing the copper wire for needing to anneal, add
18 both sides of hot cell are fixedly connected by fixed link 20 with the connecting rod 27 inside anneal chamber 26, and the both ends of connecting rod 27 are respectively mounted
There is handle 21, and the outer symmetrical of connecting rod 27 is equipped with partition board 22.
In addition to this, fuselage cover 8 is rotatably connected to end cap 3 by hinge, and the inside of end cap 3 is equipped with windowpane 4, just
In observation, and the side far from fuselage cover 8 is provided with end cap fixed seat 1 on end cap 3, and the side of end cap fixed seat 1 is equipped with
Fixed column 2.
Specifically, the side far from end cap 3 is equipped with fuselage fixed seat 10 on fuselage cover 8, fuselage fixed seat 10 it is interior
Portion offers mounting hole 11.
What deserves to be explained is the length of fixed link 20 is twice of the length of partition board 22.
Preferably, servo motor 17 and electrically heated rod 19 are electrically connected with AT89S52 controllers 23.
The operation principle and process for using of the utility model：After the copper wire processing is installed with annealing device, end is opened
Lid 3 adds in the copper wire for needing to anneal to the inside of anneal chamber 26, closes end cap 3, by fixed column 2 and mounting hole 11 that end cap 3 is close
Envelope, makes to work normally with the device that AT89S52 controllers 23 are electrically connected, electrically heated rod 19 by AT89S52 controllers 23
Work is internally heated anneal chamber 26, while the work of servo motor 17 drives motor gear 24 to turn clockwise by shaft
Dynamic, the rotation of motor gear 24 drives driving gear 25 to rotate by the gear teeth, and the rotation of driving gear 25 drives annular tooth by the gear teeth
Item 7 rotates clockwise, and the rotation of annular rack 7 drives fuselage cover 8 to rotate clockwise, and the rotation of fuselage cover 8 makes internal copper wire exist
It can be heated evenly under the action of partition board 22, after a period of time is rotated clockwise, motor tooth is made by AT89S52 controllers 23
Wheel 24 rotates counterclockwise, and motor gear 24 rotates counterclockwise drive, and the rotation of driving gear 25 drives annular rack 7 inverse by the gear teeth
Hour hands rotate, and the rotation of annular rack 7 drives fuselage cover 8 to rotate counterclockwise, and internal copper wire is heated, after the completion of heating,
Electrically heated rod 19 is made to be stopped by AT89S52 controllers 23,26 internal temperature of anneal chamber is made slowly to reduce, copper wire is carried out
Annealing is completed in cooling, after the completion of annealing, is opened end cap 3, is taken out copper wire.
While there has been shown and described that the embodiment of the utility model, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case of the principle and spirit for not departing from the utility model, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (7)
1. a kind of copper wire processing annealing device, including fuselage cover (8) and firm banking (16), it is characterised in that：It is described solid
The top both sides for determining pedestal (16) are symmetrically installed with connection column (15), and bearing is equipped with above the connection column (15)
Seat (13), the bearing block (13) are internally provided with fixing axle (14), and the outer symmetrical of the fixing axle (14) is arranged with master
Moving gear (25), one of them described driving gear (25) are connected with motor gear (24), the motor tooth by gear teeth meshing
Wheel (24) is rotatably connected to servo motor (17) by shaft, and the servo motor (17) is consolidated with firm banking (16) by bolt
Fixed connection, firm banking (16) top are equipped with AT89S52 controllers (23) close to the side of connection column (15).
2. a kind of copper wire processing annealing device according to claim 1, it is characterised in that：The fuselage cover (8)
Outside is provided with insulating layer (5), and the both sides external of the insulating layer (5) is symmetrically installed with annular rack (7), two annulars
Rack (7) is connect with driving gear (25) by gear teeth meshing, and the fuselage cover (8) is internally provided with support base
(12), the inner homogeneous of the support base (12) is opened up there are four sliding slot (6), and the sliding slot (6) is slidably connected by sliding rail (9)
There is heating room (18).
3. a kind of copper wire processing annealing device according to claim 2, it is characterised in that：It is described to heat the interior of room (18)
Portion's installation is uniformly equipped with electrically heated rod (19), and that heats room (18) is internally provided with anneal chamber (26), the heating room
(18) both sides are fixedly connected by fixed link (20) connecting rod (27) internal with anneal chamber (26), the connecting rod (27)
Both ends are mounted on handle (21), and the outer symmetrical of connecting rod (27) is equipped with partition board (22).
4. a kind of copper wire processing annealing device according to claim 2, it is characterised in that：The fuselage cover (8) is logical
It crosses hinge and is rotatably connected to end cap (3), the inside of the end cap (3) is equipped with windowpane (4), and far from fuselage on end cap (3)
The side of shell (8) is provided with end cap fixed seat (1), and the side of the end cap fixed seat (1) is equipped with fixed column (2).
5. a kind of copper wire processing annealing device according to claim 4, it is characterised in that：On the fuselage cover (8)
Side far from end cap (3) is equipped with fuselage fixed seat (10), and the inside of the fuselage fixed seat (10) offers mounting hole
(11)。
6. a kind of copper wire processing annealing device according to claim 3, it is characterised in that：The length of the fixed link (20)
Degree is twice of the length of partition board (22).
7. a kind of copper wire processing annealing device according to claim 1, it is characterised in that：The servo motor (17) and
Electrically heated rod (19) is electrically connected with AT89S52 controllers (23).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721367930.6U CN207581889U (en) | 2017-10-23 | 2017-10-23 | A kind of copper wire processing annealing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721367930.6U CN207581889U (en) | 2017-10-23 | 2017-10-23 | A kind of copper wire processing annealing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207581889U true CN207581889U (en) | 2018-07-06 |
Family
ID=62728195
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721367930.6U Expired - Fee Related CN207581889U (en) | 2017-10-23 | 2017-10-23 | A kind of copper wire processing annealing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207581889U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111254275A (en) * | 2020-03-09 | 2020-06-09 | 余堂勇 | Protective equipment for annealing of special-shaped copper strip |
| CN116970766A (en) * | 2023-07-27 | 2023-10-31 | 安徽永利成科技有限公司 | Die steel processing heat treatment equipment |
-
2017
- 2017-10-23 CN CN201721367930.6U patent/CN207581889U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111254275A (en) * | 2020-03-09 | 2020-06-09 | 余堂勇 | Protective equipment for annealing of special-shaped copper strip |
| CN111254275B (en) * | 2020-03-09 | 2021-10-01 | 胡超云 | Protective equipment for annealing of special-shaped copper strip |
| CN116970766A (en) * | 2023-07-27 | 2023-10-31 | 安徽永利成科技有限公司 | Die steel processing heat treatment equipment |
| CN116970766B (en) * | 2023-07-27 | 2024-03-12 | 安徽永利成科技有限公司 | Die steel processing heat treatment equipment |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180706 Termination date: 20181023 |