CN210640448U - 400T punch press modulus of continuity aviation plug that possesses quick replacement - Google Patents
400T punch press modulus of continuity aviation plug that possesses quick replacement Download PDFInfo
- Publication number
- CN210640448U CN210640448U CN201921512274.3U CN201921512274U CN210640448U CN 210640448 U CN210640448 U CN 210640448U CN 201921512274 U CN201921512274 U CN 201921512274U CN 210640448 U CN210640448 U CN 210640448U
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- wall
- punch press
- fixedly connected
- aviation plug
- continuity
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Abstract
The utility model discloses a 400T punch press modulus of continuity aviation plug that possesses quick replacement, including examining the inspection line, examine the one end of inspecting the line and pass through adapter sleeve fixedly connected with installation head, it includes the sinle silk to examine the inspection line, the outer wall cover of sinle silk is equipped with insulating cover, and insulating cover's outer wall cover is equipped with the lag, tin solder layer fixedly connected with circuit board is passed through to the one end of sinle silk, two of one side fixedly connected with of sinle silk are participated in to the circuit board, the middle part fixedly connected with skid resistant course of installation head outer wall, the right side of skid resistant course just is located fixedly connected with limiting plate on the outer wall of installation head, and swing joint has the dust-stopping cover on the right side of limiting plate. This 400T punch press modulus of continuity aviation plug that possesses quick replacement through will examining the line welding to the plug, when changing the modulus of continuity at every turn, only need can accomplish the installation with the plug insert socket, has improved work efficiency.
Description
Technical Field
The utility model relates to the technical field of mold, specifically be a 400T punch press modulus of continuity aviation plug that possesses quick replacement.
Background
The progressive die, also called progressive die and skip die, means that a press machine completes multiple processes of punching die at several different positions in one stroke in sequence, a punched part is formed step by step in the progressive die, continuous forming is a process method with centralized processes, multiple processes of trimming, notching, grooving, punching, plastic deformation, blanking and the like can be completed on a pair of dies, and multiple punching processes are arranged in a certain sequence to perform continuous punching according to the actual requirements of the punched part.
The existing 400T punching machine is in work, wiring is needed when the progressive die is replaced every time, the operation process is complex, meanwhile, wiring possibly has an insecure condition, certain potential safety hazards exist, the work efficiency is low, and therefore the 400T punching machine progressive die aviation plug with the quick replacement function is designed to solve the problems.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art, the utility model provides a 400T punch press modulus of continuity aviation plug that possesses quick replacement has solved current 400T punch press and is carrying out the during operation, all need wiring when changing the modulus of continuity at every turn, and operation process is loaded down with trivial details, and the wiring probably has insecure condition simultaneously, has certain potential safety hazard, problem that work efficiency is low.
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: A400T punching machine progressive die aviation plug with quick replacement comprises a detection wire, wherein one end of the detection wire is fixedly connected with an installation head through a connecting sleeve, the detection wire comprises a wire core, the outer wall of the wire core is sleeved with an insulating sleeve, the outer wall of the insulating sleeve is sleeved with a protective sleeve, one end of the wire core is fixedly connected with a circuit board through a tin welding layer, one side of the circuit board, away from the wire core, is fixedly connected with two pins, the middle part of the outer wall of the installation head is fixedly connected with an anti-slip layer, the right side of the anti-slip layer is fixedly connected with a limiting plate on the outer wall of the installation head, the right side of the limiting plate is movably connected with a dust blocking cover on the outer wall of the installation head, the right side of the outer wall of the installation head is sleeved with a, two jacks are formed in the inner bottom wall of the mounting groove, and a clamping groove matched with the clamping ring is formed in the middle of the inner side wall of the mounting groove.
Preferably, the connecting sleeve is a cylindrical structure, the detection line penetrates through the connecting sleeve, a left opening of the connecting sleeve is matched with the outer diameter of the detection line, and an installation head is clamped in a right opening of the connecting sleeve.
Preferably, the insulating sleeve is made of rubber.
Preferably, the sinle silk runs through the inside that the soldering layer extends to the tin solder layer and is connected with the circuit board, the fixed outside that covers at the sinle silk of tin solder layer.
Preferably, the mounting groove is matched with the mounting head, and the insertion hole is matched with the plug pin.
Preferably, the anti-skid layer is provided with groined grains on the outer part.
Preferably, one side of the dust-blocking cover is provided with a ferrule which is sleeved on the outer wall of the mounting head, and the other side of the dust-blocking cover is provided with a cover plate which is matched with one side of the mounting head, which is positioned on the pin.
Advantageous effects
The utility model provides a 400T punch press modulus of continuity aviation plug that possesses quick replacement. Compared with the prior art, the method has the following beneficial effects:
(1) this 400T punch press modulus of continuity aviation plug that possesses quick replacement, through detecting the line welding to the plug on, when changing the modulus of continuity at every turn, need not to carry on loaded down with trivial details wiring work again, only need to insert the plug and can accomplish the installation with the socket, the change mode of traditional punch press modulus of continuity of comparison, work efficiency is higher, and easy operation is convenient, it is also more firm reliable to connect, through being provided with snap ring and draw-in groove, when pegging graft with the plug again, can realize pulling out fast of plug and insert, accomplish the quick replacement of modulus of continuity, and the work efficiency is improved.
(2) This 400T punch press modulus of continuity aviation plug that possesses quick replacement through being provided with the adapter sleeve, and the connection that can fasten is examined line and installation head, has guaranteed not breaking away from of installation head to can realize examining that the line is linked together with the socket.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the internal structure of the inspection line of the present invention;
fig. 3 is a cross-sectional view of the socket of the present invention.
In the figure: 1-detecting wire, 2-connecting sleeve, 3-mounting head, 4-wire core, 5-insulating sleeve, 6-protecting sleeve, 7-tin welding layer, 8-circuit board, 9-pin, 10-anti-slip layer, 11-limiting plate, 12-dust-blocking cover, 13-snap ring, 14-socket, 15-base, 16-mounting groove, 17-jack and 18-clamping groove.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: A400T punching machine progressive die aviation plug with quick replacement comprises a detection line 1, one end of the detection line 1 is fixedly connected with an installation head 3 through a connecting sleeve 2, the connecting sleeve 2 is set to be a cylindrical structure, the detection line 1 penetrates through the connecting sleeve 2, the left opening of the connecting sleeve 2 is matched with the outer diameter of the detection line 1, the right opening of the connecting sleeve 2 is clamped with the installation head 3, the detection line 1 comprises a wire core 4, the outer wall of the wire core 4 is sleeved with an insulating sleeve 5, the insulating sleeve 5 is made of rubber, the outer wall of the insulating sleeve 5 is sleeved with a protective sleeve 6, one end of the wire core 4 is fixedly connected with a circuit board 8 through a tin welding layer 7, the wire core 4 penetrates through the tin welding layer 7, extends to the inside of the tin welding layer 7 and is connected with the circuit board 8, the tin welding layer 7 is fixedly covered on the outside of the wire core 4, one side, the anti-skid layer 10 is provided with groined-shaped grains outside, the right side of the anti-skid layer 10 is fixedly connected with a limit plate 11 on the outer wall of the mounting head 3, the right side of the limit plate 11 on the outer wall of the mounting head 3 is movably connected with a dust-blocking cover 12, one side of the dust-blocking cover 12 is provided with a ferrule which is sleeved on the outer wall of the mounting head 3, the other side of the dust-blocking cover 12 is provided with a cover plate which is matched with one side of the mounting head 3 on the pins 9, the right side of the outer wall of the mounting head 3 is sleeved with a snap ring 13, the right side of the mounting head 3 is provided with a socket 14 outside, the socket 14 comprises a base 15, the left side wall of the base 15 is provided with a mounting groove 16, the inner bottom wall of the mounting groove 16 is provided with two jacks 17, the mounting groove 16 is, through will examining line 1 and welding to the plug, when changing the modulus of continuity at every turn, need not to carry on loaded down with trivial details wiring work again, only need insert socket 14 with the plug and can accomplish the installation, the change mode of traditional punch press modulus of continuity of comparison, work efficiency is higher, and easy operation is convenient, connect also more firmly reliably, through being provided with snap ring 13 and draw-in groove 18, when pegging graft the plug again, can realize pulling out the quick of plug and inserting, accomplish the quick replacement of modulus of continuity, work efficiency is improved, this 400T punch press modulus of continuity aviation plug that possesses quick replacement, through being provided with adapter sleeve 2, can fasten connect to examine line 1 and installation head 3, the non-breaking away from of installation head 3 has been guaranteed, thereby can realize examining that line 1 and socket 14 are linked together.
During operation, when carrying out the change of modulus of continuity, because it is welded in aviation plug to examine and examine line 1, need not manually to carry out loaded down with trivial details wiring operation, operating personnel only need pull out the plug and insert the operation and can accomplish the job requirement under the different operating condition, when needing to change the modulus of continuity, only need pull out the plug, after the change of accomplishing the modulus of continuity, peg graft the plug again in socket 14, the change of modulus of continuity has been accomplished promptly, traditional wiring operation compares, the change efficiency of modulus of continuity has been improved greatly, and the design of snap ring 13 and draw-in groove 18, make plug grafting convenient to detach when firm.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides a 400T punch press modulus of continuity aviation connector that possesses quick replacement, is including examining and examining line (1), the one end of examining and examining line (1) is through adapter sleeve (2) fixedly connected with installation head (3), its characterized in that: the detection line (1) comprises a wire core (4), an insulating sleeve (5) is sleeved on the outer wall of the wire core (4), a protective sleeve (6) is sleeved on the outer wall of the insulating sleeve (5), one end of the wire core (4) is fixedly connected with a circuit board (8) through a tin welding layer (7), one side, far away from the wire core (4), of the circuit board (8) is fixedly connected with two pins (9), the middle of the outer wall of the mounting head (3) is fixedly connected with an anti-slip layer (10), the right side of the anti-slip layer (10) is fixedly connected with a limiting plate (11) on the outer wall of the mounting head (3), the right side of the limiting plate (11) is movably connected with a dust blocking cover (12) on the outer wall of the mounting head (3), a clamping ring (13) is sleeved on the right side of the outer wall of the mounting head (, socket (14) include base (15), mounting groove (16) have been seted up on the left side wall of base (15), two jack (17) have been seted up to the inner diapire of mounting groove (16), draw-in groove (18) with snap ring (13) looks adaptation are seted up at the middle part of mounting groove (16) inside wall.
2. The progressive die aviation plug for 400T punch press with quick change of claim 1, wherein: the connecting sleeve (2) is arranged to be of a cylindrical structure, the detecting line (1) penetrates through the connecting sleeve (2), the left opening of the connecting sleeve (2) is matched with the outer diameter of the detecting line (1), and the right opening of the connecting sleeve (2) is clamped with the mounting head (3).
3. The progressive die aviation plug for 400T punch press with quick change of claim 1, wherein: the insulating sleeve (5) is made of rubber.
4. The progressive die aviation plug for 400T punch press with quick change of claim 1, wherein: sinle silk (4) run through tin solder layer (7) and extend to the inside of tin solder layer (7) and be connected with circuit board (8), fixed the covering in the outside of sinle silk (4) of tin solder layer (7).
5. The progressive die aviation plug for 400T punch press with quick change of claim 1, wherein: the mounting groove (16) is matched with the mounting head (3), and the insertion hole (17) is matched with the pin (9).
6. The progressive die aviation plug for 400T punch press with quick change of claim 1, wherein: the anti-skid layer (10) is provided with groined grains on the outer part.
7. The progressive die aviation plug for 400T punch press with quick change of claim 1, wherein: and a ferrule is arranged on one side of the dust blocking cover (12), the ferrule is sleeved on the outer wall of the mounting head (3), a cover plate is arranged on the other side of the dust blocking cover (12), and the cover plate is matched with one side, located on the pin (9), of the mounting head (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921512274.3U CN210640448U (en) | 2019-09-11 | 2019-09-11 | 400T punch press modulus of continuity aviation plug that possesses quick replacement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921512274.3U CN210640448U (en) | 2019-09-11 | 2019-09-11 | 400T punch press modulus of continuity aviation plug that possesses quick replacement |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210640448U true CN210640448U (en) | 2020-05-29 |
Family
ID=70797041
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921512274.3U Expired - Fee Related CN210640448U (en) | 2019-09-11 | 2019-09-11 | 400T punch press modulus of continuity aviation plug that possesses quick replacement |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210640448U (en) |
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2019
- 2019-09-11 CN CN201921512274.3U patent/CN210640448U/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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200529 Termination date: 20200911 |