CN217442411U - Buckle type split pin wire with aviation connector and electronic digital detonator - Google Patents
Buckle type split pin wire with aviation connector and electronic digital detonator Download PDFInfo
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- CN217442411U CN217442411U CN202221292858.6U CN202221292858U CN217442411U CN 217442411 U CN217442411 U CN 217442411U CN 202221292858 U CN202221292858 U CN 202221292858U CN 217442411 U CN217442411 U CN 217442411U
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Abstract
The utility model discloses a take aviation joint electron digital detonator buckle formula components of a whole that can function independently foot line relates to the electron detonator field, including components of a whole that can function independently foot line main part, the one end of components of a whole that can function independently foot line main part is provided with the socket, and the one end of socket is connected with the aviation plug to the one end that the socket was kept away from to the aviation plug is connected with the detonator main part, the outer wall cover of aviation plug and socket is equipped with the adapter sleeve. The utility model provides an electron detonator and the not enough problem of components of a whole that can function independently foot line main part junction stability, the adapter sleeve through setting up can the block at the outer wall of aviation plug and socket, thereby protect electron detonator and components of a whole that can function independently foot line main part junction, first buckle through the socket outer wall cooperates with first interface, be convenient for fix socket and adapter sleeve, the inside second block of socket cooperates with the first draw-in groove of detonator main part outer wall, the realization is connected the purpose to detonator main part and components of a whole that can function independently foot line main part, the work efficiency of installation has been improved.
Description
Technical Field
The utility model relates to an electron detonator field specifically is a take aviation connector electron digital detonator buckle formula components of a whole that can function independently foot line.
Background
The electronic detonator is also called as an electronic digital detonator or an industrial digital detonator, the digital electronic detonator is used as a safe, reliable, high-precision, intelligent and environment-friendly detonating device with excellent performance, can meet the requirements of complex blasting engineering, the production and the application of the electronic detonator are expanded from the early rare and valuable mineral mining field to common mines and quarries, and the technical superiority of the electronic detonator is more and more widely recognized in the global blasting world.
The electronic detonator is detonated by connecting the split leg wire with the electronic detonator, and the split leg wire and the electronic detonator are usually installed and then used.
In the prior art, the electronic detonator and the split leg wire are usually connected by using threads, so that the use and the installation are troublesome, the stability of the connection part of the electronic detonator and the split leg wire is not enough, the electronic detonator is easy to shake, and the connection part of the electronic detonator and the split leg wire is easy to break to cause the damage problem when the electronic detonator and the split leg wire are inserted into explosive substances during use and installation.
Disclosure of Invention
Based on this, the utility model aims at providing a take aviation connector electron digital detonator buckle formula components of a whole that can function independently foot line to solve among the prior art electron detonator and components of a whole that can function independently foot line and use threaded connection usually, it is comparatively troublesome when using the installation, electron detonator and components of a whole that can function independently foot line junction stability are not enough, rock easily, insert when using the installation and make the technical problem that electron detonator and components of a whole that can function independently foot line junction fracture lead to the damage problem easily in the blasting thing.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a take aviation joint electron digital detonator buckle formula components of a whole that can function independently foot line, includes components of a whole that can function independently foot line main part, the one end of components of a whole that can function independently foot line main part is provided with the socket, and the one end of socket is connected with the aviation plug to the one end that the socket was kept away from to the aviation plug is connected with the detonator main part, the outer wall cover of aviation plug and socket is equipped with the adapter sleeve, first draw-in groove has been seted up to the outer wall of detonator main part, the outer wall of socket is fixed with first buckle, and the inside of socket is fixed with guide post and second buckle to the inside of socket is provided with the terminal mounting hole.
Through adopting above-mentioned technical scheme, the problem of electron detonator and components of a whole that can function independently leg wire main part junction stability is not enough has been solved, adapter sleeve through setting up can block at the outer wall of aviation plug and socket, thereby protect electron detonator and components of a whole that can function independently leg wire main part junction, first buckle through the socket outer wall cooperates with first interface, be convenient for fix socket and adapter sleeve, the inside second block of socket cooperates with the first draw-in groove of detonator main part outer wall, the realization is connected the purpose of detonator main part and components of a whole that can function independently leg wire main part, the mounting means of bolt has been replaced, the work efficiency of installation has been improved, and the adapter sleeve block is in electron detonator and components of a whole that can function independently leg wire main part junction, it is more stable when the detonator main part inserts the blasting thing.
The utility model discloses further set up to, the one end of adapter sleeve is provided with first connector, and the other end of adapter sleeve is provided with the second connector to the adapter sleeve is close to the outer wall of first connector one end and has seted up the second draw-in groove.
Through adopting above-mentioned technical scheme, the adapter sleeve can block at the outer wall of circular connector and socket to protect electron detonator and components of a whole that can function independently leg wire main part junction.
The utility model discloses further set up to, the outer wall of detonator main part is provided with waterproof circle.
Through adopting above-mentioned technical scheme, waterproof circle through setting up increases the waterproof leakproofness of adapter sleeve when the adapter sleeve block is at detonator main part outer wall.
The utility model discloses further set up to, aviation plug's one end is provided with the terminal, and the terminal laminates mutually with the terminal mounting hole.
Through adopting above-mentioned technical scheme, can realize the current conduction with the cooperation of terminal mounting hole through the terminal that sets up.
The utility model discloses further set up to, second draw-in groove inner wall and the laminating of first buckle outer wall for the adapter sleeve block is at socket's outer wall.
Through adopting above-mentioned technical scheme, through the cooperation of second draw-in groove and first fixture block to realize that adapter sleeve and socket carry out the purpose fixed.
The utility model discloses further set up to, state the guide way of having seted up of circular connector, and the inner wall of guide way is laminated with the outer wall of guide post mutually.
Through adopting above-mentioned technical scheme, can cooperate with the guide post through the metallic channel that sets up, carry on spacingly to aviation plug's removal for aviation plug installs more fast.
To sum up, the utility model discloses mainly have following beneficial effect:
the utility model discloses a detonator main part, first draw-in groove, the adapter sleeve, the setting of aviation plug and socket, the problem that electronic detonator and components of a whole that can function independently foot line main part junction stability are not enough has been solved, adapter sleeve through setting up can the block at the outer wall of aviation plug and socket, thereby protect electronic detonator and components of a whole that can function independently foot line main part junction, first buckle through the socket outer wall cooperates with first interface, be convenient for fix socket and adapter sleeve, the inside second block of socket cooperates with the first draw-in groove of detonator main part outer wall, the realization is connected the purpose to detonator main part and components of a whole that can function independently foot line main part, threaded mounting means has been replaced, the work efficiency of installation has been improved, and the adapter sleeve block is in electronic detonator and components of a whole that can function independently foot line main part junction, it is more stable when the detonator main part inserts the explosive substance.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the present invention;
fig. 3 is a schematic structural diagram of the socket of the present invention;
fig. 4 is a side view of the socket of the present invention.
In the figure: 1. a split leg wire main body; 2. a detonator body; 21. a waterproof ring; 22. a first card slot; 3. connecting sleeves; 31. a first connection port; 32. a second connection port; 33. a second card slot; 4. an aviation plug; 41. a terminal; 42. a guide groove; 5. a socket; 51. a first buckle; 52. a guide post; 53. a second buckle; 54. and a terminal mounting hole.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present invention, and should not be construed as limiting the present invention.
The following describes an embodiment of the present invention according to its overall structure.
A buckle type split foot line with an aviation connector electronic digital detonator is disclosed, as shown in figures 1-4, and comprises a split foot line main body 1, wherein one end of the split foot line main body 1 is provided with a socket 5, one end of the socket 5 is connected with an aviation plug 4, one end of the aviation plug 4 far away from the socket 5 is connected with a detonator main body 2, the outer walls of the aviation plug 4 and the socket 5 are sleeved with a connecting sleeve 3, the connecting sleeve 3 is pushed to enable the connecting sleeve 3 to move on the outer wall of the socket 5, then a first buckle 51 is matched with a second clamping groove 33 to complete the fixing of the connecting sleeve 3, one end of the connecting sleeve 3 is provided with a first connecting port 31, the other end of the connecting sleeve 3 is provided with a second connecting port 32, the outer wall of the connecting sleeve 3 close to one end of the first connecting port 31 is provided with a second clamping groove 33, the outer wall of the detonator main body 2 is provided with a first clamping groove 22, and the outer wall of the socket 5 is fixed with a first buckle 51, and a guide post 52 and a second buckle 53 are fixed inside the socket 5, the guide post 52 is matched with the guide groove 42, then the terminal 41 is inserted into the terminal mounting hole 54, the second buckle 53 is matched with the first clamping groove 22, the fixing of the connecting sleeve 3 and the detonator main body 2 is completed, and the terminal mounting hole 54 is arranged inside the socket 5.
Referring to fig. 2, the outer wall of the detonator main body 2 is provided with a waterproof ring 21, and when the connecting sleeve 3 is clamped on the outer wall of the detonator main body 2 through the waterproof ring 21, the waterproof sealing performance of the connecting sleeve 3 is improved.
Referring to fig. 2, a terminal 41 is disposed at one end of the aviation plug 4, and the terminal 41 is attached to an inner wall of the terminal mounting hole 54, and the terminal 41 can be matched with the terminal mounting hole 54 to achieve current conduction.
Referring to fig. 1, the inner wall of the second engaging groove 33 is attached to the outer wall of the first buckle 51, so that the connecting sleeve 3 is engaged with the outer wall of the socket 5, and the connecting sleeve 3 is fixed to the socket 5 by the engagement of the second engaging groove 33 and the first buckle 51.
Referring to fig. 2, the aviation plug 4 is provided with a guide groove 42, an inner wall of the guide groove 42 is attached to an outer wall of the guide column 52, and the guide groove 42 is matched with the guide column 52 to limit the movement of the aviation plug 4, so that the aviation plug 4 is mounted more quickly.
The utility model discloses a theory of operation does: when the detonator is installed, the first connecting port 31 at one end of the connecting sleeve 3 is sleeved on the outer wall of the socket 5, then the connecting sleeve 3 is pushed, so that the connecting sleeve 3 moves on the outer wall of the socket 5, then the first buckle 51 is matched with the second clamping groove 33, the fixing of the connecting sleeve 3 is completed, then the aviation plug 4 at one end of the detonator main body 2 is inserted into the connecting sleeve 3, the guide post 52 is matched with the guide groove 42, then the terminal 41 is inserted into the terminal installing hole 54, the second buckle 53 is matched with the first clamping groove 22, the fixing of the connecting sleeve 3 and the detonator main body 2 is completed, and the second connecting port 32 is matched with the waterproof ring 21, so that water is prevented from entering the inside.
Although embodiments of the present invention have been shown and described, it is intended that the present embodiments be illustrative only and not limiting to the invention, and that the particular features, structures, materials, or characteristics described may be combined in any suitable manner in one or more embodiments or examples, and that modifications, substitutions, variations, and the like, which are not inventive in light of the above teachings, may be made to the embodiments by those skilled in the art without departing from the principles and spirit of the present invention, but are to be construed as broadly as the following claims.
Claims (5)
1. The utility model provides a take aviation joint electron digital detonator buckle formula components of a whole that can function independently leg wire, includes components of a whole that can function independently leg wire main part (1), its characterized in that: one end of the split leg wire main body (1) is provided with a socket (5), one end of the socket (5) is connected with an aviation plug (4), and one end of the aviation plug (4) far away from the socket (5) is connected with a detonator main body (2), the outer walls of the aviation plug (4) and the socket (5) are sleeved with a connecting sleeve (3), a first clamping groove (22) is formed in the outer wall of the detonator main body (2), a first buckle (51) is fixed on the outer wall of the socket (5), and a guide post (52) and a second buckle (53) are fixed inside the socket (5), and a terminal mounting hole (54) is arranged in the socket (5), one end of the connecting sleeve (3) is provided with a first connecting port (31), the other end of the connecting sleeve (3) is provided with a second connecting port (32), and a second clamping groove (33) is formed in the outer wall of one end, close to the first connecting port (31), of the connecting sleeve (3).
2. The snap-in type split pin line with the aviation connector electronic digital detonator according to claim 1, characterized in that: the outer wall of the detonator main body (2) is provided with a waterproof ring (21).
3. The snap-in type split pin line with the aviation connector electronic digital detonator according to claim 1, characterized in that: and one end of the aviation plug (4) is provided with a terminal (41), and the terminal (41) is attached to the inner wall of the terminal mounting hole (54).
4. The snap-in type split pin line with the aviation connector electronic digital detonator according to claim 2, characterized in that: the inner wall of the second clamping groove (33) is attached to the outer wall of the first buckle (51), so that the connecting sleeve (3) is clamped on the outer wall of the socket (5).
5. The snap-in type split pin line with the aviation connector electronic digital detonator according to claim 1, characterized in that: the aviation plug (4) is provided with a guide groove (42), and the inner wall of the guide groove (42) is attached to the outer wall of the guide column (52).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221292858.6U CN217442411U (en) | 2022-05-27 | 2022-05-27 | Buckle type split pin wire with aviation connector and electronic digital detonator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221292858.6U CN217442411U (en) | 2022-05-27 | 2022-05-27 | Buckle type split pin wire with aviation connector and electronic digital detonator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217442411U true CN217442411U (en) | 2022-09-16 |
Family
ID=83222647
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221292858.6U Active CN217442411U (en) | 2022-05-27 | 2022-05-27 | Buckle type split pin wire with aviation connector and electronic digital detonator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217442411U (en) |
-
2022
- 2022-05-27 CN CN202221292858.6U patent/CN217442411U/en active Active
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