CN210334919U - Clamp for auxiliary welding of aviation socket for intermediate frequency product - Google Patents
Clamp for auxiliary welding of aviation socket for intermediate frequency product Download PDFInfo
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- CN210334919U CN210334919U CN201920903704.8U CN201920903704U CN210334919U CN 210334919 U CN210334919 U CN 210334919U CN 201920903704 U CN201920903704 U CN 201920903704U CN 210334919 U CN210334919 U CN 210334919U
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- vertical plate
- intermediate frequency
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Abstract
The utility model discloses an anchor clamps that is used for supplementary welding aviation socket of intermediate frequency product, include: the mounting component is arranged on the supporting component; the cover plate is connected with one side of the mounting assembly through a connecting piece; the overturning assembly is used for fixing the mounting assembly and the cover plate on the supporting assembly and enabling the mounting assembly to overturn; the supporting assembly is composed of a bottom plate, a first vertical plate and a second vertical plate, the first vertical plate and the second vertical plate are vertically fixed on the bottom plate, and central axes of the first vertical plate and the second vertical plate are on the same straight line. The utility model discloses a set up supplementary anchor clamps, the convenience welds the aviation socket, overturns the installation component through control upset subassembly, and convenient operation improves welding efficiency, guarantees welding quality.
Description
Technical Field
The utility model relates to an aviation socket makes technical field, especially relates to an anchor clamps that is used for supplementary welding aviation socket of intermediate frequency product.
Background
In order to improve the health index and the happiness of the people; in order to meet the actual market requirements, various manufacturing enterprises have developed a plurality of intermediate frequency therapeutic apparatuses as medical equipment in the manufacturing industry for comprehensively promoting development and production of medical and health care industries.
At present, the middle-frequency therapeutic instrument product is manufactured, a clamp for processing an output accessory (an aviation socket) of the product is not provided, manual operation is adopted for welding the aviation socket, the aviation socket needs to be installed and welded one by one, and the operation is complex.
When the mill was making medium frequency therapy appearance instrument processing aviation socket, because the outward appearance structure particularity of this piece and actual operation's very big inconvenience, cause that the technical ability to the personnel when actual operation requires highly, welded technology and quality effect can't ensure stably simultaneously, are more difficult to promote the efficiency of production.
Disclosure of Invention
The utility model aims to solve the technical problem that to the not enough among the above-mentioned prior art, a anchor clamps that is used for supplementary welding aviation socket of intermediate frequency product is disclosed.
The utility model adopts the technical proposal that:
a fixture for auxiliary welding of an aviation socket for intermediate frequency products comprises:
a support component is arranged on the base plate,
the mounting assembly is arranged on the supporting assembly;
the cover plate is connected with one side of the mounting assembly through a connecting piece;
the overturning assembly is used for fixing the mounting assembly and the cover plate on the supporting assembly and enabling the mounting assembly to overturn;
the supporting assembly is composed of a bottom plate, a first vertical plate and a second vertical plate, the first vertical plate and the second vertical plate are vertically fixed on the bottom plate, and central axes of the first vertical plate and the second vertical plate are on the same straight line.
As a further technical solution of the utility model is: the installation component adopts a strip plate structure with a strip through hole in the middle, wherein two ends of the strip plate structure are fixed with the first vertical plate and the second vertical plate through the turnover component respectively.
As a further technical solution of the utility model is: the upset subassembly includes swivel bearing and automatic latch fitting, swivel bearing sets up in the both sides of supporting component and fixed with the supporting component, the last fixed installation component that sets up of swivel bearing, automatic latch fitting passes through the latch fitting fixed plate to be fixed on the supporting component.
As a further technical solution of the utility model is: and the supporting component is provided with a positioning sheet.
As a further technical solution of the utility model is: the connecting pieces are connected by hinges.
As a further technical solution of the utility model is: the cover plate is provided with a first mounting part, a second mounting part is arranged on the mounting component corresponding to the first mounting part in a buckled mode with the cover plate, and the cover plate and the mounting component are locked and fixed through the first mounting part and the second mounting part.
Further: the first installation part adopts a lock catch, and the second installation part adopts a spring lock piece.
Further: the overturning angle of the overturning assembly is 180 degrees.
The utility model has the advantages that:
the utility model discloses a set up supplementary anchor clamps, can conveniently weld the aviation socket, play the fixed stay effect to the installation component through the supporting component, place the aviation socket and put into perpendicularly in the installation component, it is fixed to utilize the apron to carry out the pressfitting, will install the subassembly upset through control upset subassembly, the bottom of aviation socket up this moment, then can be to the welding of aviation socket. Convenient operation, improved welding efficiency and ensured welding quality.
Drawings
Fig. 1 is a perspective view of a fixture for assisting in welding an aviation socket to an intermediate frequency product according to the present invention;
fig. 2 is a structural diagram of the mounting assembly and the cover plate according to the present invention;
fig. 3 is a top view of the cover plate and the mounting assembly.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, 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, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Example one
Referring to fig. 1 to fig. 3, fig. 1 is a perspective view of a fixture for assisting welding an aviation socket of an intermediate frequency product according to the present invention; fig. 2 is a structural diagram of the mounting assembly and the cover plate according to the present invention; fig. 3 is a top view of the cover plate and the mounting assembly.
As shown in fig. 1 to 3, a fixture for auxiliary welding of an aviation socket for intermediate frequency products includes:
a support assembly (10) for supporting the workpiece,
a mounting assembly 20, the mounting assembly 20 being disposed on the support assembly 10;
a cover plate 30, wherein the cover plate 30 is connected with one side of the mounting assembly 20 through a connecting piece 50;
a turnover assembly 40 for fixing the mounting assembly 20 and the cover plate 30 on the support assembly 10 and turning over the mounting assembly 20;
the supporting assembly 10 is composed of a bottom plate 101, a first vertical plate 102 and a second vertical plate 103, wherein the first vertical plate 102 and the second vertical plate 103 are vertically fixed on the bottom plate 101, and central axes of the first vertical plate 102 and the second vertical plate 103 are on the same straight line.
The embodiment of the utility model provides an in, through setting up supplementary anchor clamps, can conveniently weld the aviation socket, play the fixed stay effect to the installation component through the supporting component, place the aviation socket and put into perpendicularly in the installation component, it is fixed to utilize the apron to carry out the pressfitting, overturns the installation component through control upset subassembly, and the bottom of aviation socket up this moment then can be to the welding of aviation socket. Convenient operation, improved welding efficiency and ensured welding quality.
Example two
The embodiment further defines the mounting assembly on the basis of the first embodiment, specifically, the mounting assembly 20 adopts a strip plate structure with a strip through hole 201 in the middle, wherein two ends of the strip plate structure are respectively fixed with the first vertical plate 102 and the second vertical plate 103 through the turning assembly 40. The installation component adopts the strip through hole, can operate a plurality of aviation spares simultaneously, improves production efficiency.
EXAMPLE III
The present embodiment is to limit the structure of the turnover assembly, specifically, the turnover assembly 40 includes a rotary bearing 401 and an automatic locking piece 402, the rotary bearing 401 is disposed on two sides of the supporting assembly 10 and fixed with the supporting assembly, the mounting assembly 20 is fixedly disposed on the rotary bearing 401, and the automatic locking piece 402 is fixed on the supporting assembly through a locking piece fixing plate 403. Fix the installation component through automatic latch fitting, prevent to rotate at installation aviation socket or welded in-process swivel bearing, improve welding operation convenience and welding product quality.
Example four
In order to fix the installation component conveniently, prevent that the installation component from rotating at will, still set up spacer 104 on the supporting component, wherein the spacer is fixed on the first riser of supporting component for "L" type structure, and after the installation component upset, carry on spacingly through the spacer, then lock through automatic latch fitting, automatic latch fitting adopts the spring lock, convenient operation.
The embodiment of the utility model provides an in, the connecting piece can adopt hinge connection, also can adopt the pivot to connect to but realize that the lid is rotatory around one side of installation component and lock can, preferred, the connecting piece adopts hinge connection.
In order to ensure that the cover and the mounting assembly are not separated from each other after being fastened and turned over, in this embodiment, a first mounting part 301 is further disposed on the cover, a second mounting part 202 is disposed at a mounting assembly position corresponding to the first mounting part 301 fastened to the cover, and the cover 30 and the mounting assembly 20 are locked and fixed by the first mounting part 301 and the second mounting part 202. Preferably, the first mounting member is a latch and the second mounting member is a spring lock. Wherein, the turnover angle of the turnover assembly is 180 degrees.
The embodiment of the utility model provides an in, supporting component, installation component adopt the bakelite material preparation, and the size of installation component specifically uses actual design as the standard according to aviation socket's structure size setting.
The basic principles and main features of the invention and the advantages of the invention have been shown and described above. It should be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that various changes and modifications may be made without departing from the spirit and scope of the invention, and such changes and modifications fall within the scope of the claimed invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (8)
1. The utility model provides a anchor clamps that is used for supplementary welding aviation socket of intermediate frequency product which characterized in that includes:
a support component is arranged on the base plate,
the mounting assembly is arranged on the supporting assembly;
the cover plate is connected with one side of the mounting assembly through a connecting piece;
the overturning assembly is used for fixing the mounting assembly and the cover plate on the supporting assembly and enabling the mounting assembly to overturn;
the supporting assembly is composed of a bottom plate, a first vertical plate and a second vertical plate, the first vertical plate and the second vertical plate are vertically fixed on the bottom plate, and central axes of the first vertical plate and the second vertical plate are on the same straight line.
2. The fixture for the aviation socket for assisting in welding of the intermediate frequency product as claimed in claim 1, wherein the mounting assembly is a bar plate structure with a bar-shaped through hole in the middle, and two ends of the bar plate structure are fixed to the first vertical plate and the second vertical plate through the turnover assembly respectively.
3. The fixture for the aviation socket for the auxiliary welding of the intermediate frequency products as claimed in claim 1, wherein the flip assembly comprises a rotary bearing and an automatic locking member, the rotary bearing is disposed at two sides of the supporting assembly and fixed to the supporting assembly, a mounting assembly is fixedly disposed on the rotary bearing, and the automatic locking member is fixed to the supporting assembly through a locking member fixing plate.
4. The fixture for auxiliary welding of aviation sockets for intermediate frequency products as claimed in claim 1, wherein the support assembly is provided with a positioning plate.
5. The fixture for auxiliary welding of aviation sockets for intermediate frequency products according to claim 1, wherein the connecting pieces are connected by hinges.
6. The fixture for assisting in welding the aviation socket of the intermediate frequency product as claimed in claim 1, wherein the cover plate is provided with a first mounting member, and a second mounting member is provided at a position corresponding to a mounting component of the first mounting member, which is engaged with the cover plate, and the cover plate and the mounting component are locked and fixed by the first mounting member and the second mounting member.
7. The fixture for auxiliary welding of aviation sockets for intermediate frequency products as claimed in claim 6, wherein the first mounting member is a lock catch, and the second mounting member is a spring lock.
8. The fixture for the auxiliary welding aviation socket of the intermediate frequency products as claimed in claim 1, wherein the turning angle of the turning assembly is 180 degrees.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920903704.8U CN210334919U (en) | 2019-06-17 | 2019-06-17 | Clamp for auxiliary welding of aviation socket for intermediate frequency product |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920903704.8U CN210334919U (en) | 2019-06-17 | 2019-06-17 | Clamp for auxiliary welding of aviation socket for intermediate frequency product |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210334919U true CN210334919U (en) | 2020-04-17 |
Family
ID=70186034
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920903704.8U Active CN210334919U (en) | 2019-06-17 | 2019-06-17 | Clamp for auxiliary welding of aviation socket for intermediate frequency product |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210334919U (en) |
-
2019
- 2019-06-17 CN CN201920903704.8U patent/CN210334919U/en active Active
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