CN215880864U - Aviation seat support adds clamping apparatus - Google Patents
Aviation seat support adds clamping apparatus Download PDFInfo
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- CN215880864U CN215880864U CN202122451524.0U CN202122451524U CN215880864U CN 215880864 U CN215880864 U CN 215880864U CN 202122451524 U CN202122451524 U CN 202122451524U CN 215880864 U CN215880864 U CN 215880864U
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- positioning groove
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- mounting plate
- hole
- positioning
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Abstract
The utility model belongs to the technical field of machining, and relates to an aviation seat support machining clamp which comprises a mounting plate, wherein a base is arranged on the upper surface of the mounting plate, a plurality of positioning holes are formed in the mounting plate, connecting holes are formed in the base, and the connecting holes in the base are aligned with the corresponding positioning holes in the mounting plate and then fixedly connected through a connecting assembly; the base is provided with a positioning groove, the positioning groove comprises a front positioning groove and a back positioning groove, and the front positioning groove and the back positioning groove are respectively arranged on two sides of the base corresponding to the connecting line of the two connecting holes; and after the front positioning groove and the back positioning groove are respectively matched with the workpieces, the workpieces are limited through the expansion blocks. The utility model can be suitable for multiple processes without re-clamping and debugging, thereby reducing debugging time, improving production efficiency and saving materials.
Description
Technical Field
The utility model belongs to the technical field of machining and relates to an aviation seat support machining clamp.
Background
Aiming at some parts processed in large batch, the traditional machine clamp can only complete a certain fixed process, needs great manpower and material resources to switch to the next process, and does not meet the production requirement of a factory.
Disclosure of Invention
Aiming at the problems, the utility model provides the machining clamp for the aviation seat support, which can effectively reduce manpower and material resources and improve the machining efficiency.
According to the technical scheme of the utility model: the utility model provides an aviation seat support adds clamping apparatus which characterized in that: the mounting plate comprises a mounting plate, wherein a base is arranged on the upper surface of the mounting plate, a plurality of positioning holes are formed in the mounting plate, connecting holes are formed in the base, and the connecting holes in the base are aligned with the corresponding positioning holes in the mounting plate and then fixedly connected through a connecting assembly;
the base is provided with a positioning groove, the positioning groove comprises a front positioning groove and a back positioning groove, and the front positioning groove and the back positioning groove are respectively arranged on two sides of the base corresponding to the connecting line of the two connecting holes;
and after the front positioning groove and the back positioning groove are respectively matched with the workpieces, the workpieces are limited through the expansion blocks.
As a further improvement of the utility model, the connecting hole and the positioning hole are both constructed as step counter bores, wherein the step surface of the positioning hole is provided with a threaded hole, and the step surface of the positioning hole is positioned and provided with a connecting sleeve which is fixedly connected with the mounting plate through a fastening bolt;
the shaft sleeve is arranged on the step surface of the connecting hole, and the connecting bolt penetrates through the shaft sleeve and then is in threaded connection with the connecting sleeve, so that the base is fixedly connected with the mounting plate.
As a further improvement of the utility model, the base is provided with two front positioning grooves and two back positioning grooves.
As a further improvement of the utility model, process spaces are arranged at the vertex angles of the bending parts of the front positioning groove and the back positioning groove.
The utility model has the technical effects that: the utility model can be suitable for multiple processes without re-clamping and debugging, thereby reducing debugging time, improving production efficiency and saving materials.
Drawings
Fig. 1 is an exploded view of the present invention.
Fig. 2 is an assembly view of the present invention.
Detailed Description
The following further describes embodiments of the present invention with reference to the drawings.
In the figures 1 and 2, the device comprises a workpiece 1, an expansion block 2, a connecting bolt 3, a shaft sleeve 4, a mounting plate 5, a positioning hole 5-1, a connecting sleeve 6, a fastening bolt 7, a positioning groove 8, a front positioning groove 8-1, a back positioning groove 8-2, a base 9 and the like.
As shown in fig. 1 and 2, the utility model relates to an aviation seat support machining clamp which comprises a mounting plate 5, wherein a base 9 is arranged on the upper surface of the mounting plate 5, a plurality of positioning holes 5-1 are formed in the mounting plate 5, a connecting hole 9-1 is formed in the base 9, and the connecting hole 9-1 in the base 9 is aligned with the corresponding positioning hole 5-1 in the mounting plate 5 and then fixedly connected through a connecting component.
The base 9 is provided with a positioning groove 8, the positioning groove 8 comprises a front positioning groove 8-1 and a back positioning groove 8-2, and the front positioning groove 8-1 and the back positioning groove 8-2 are respectively arranged on two sides of the base 9 corresponding to the line of the two connecting holes 9-1.
After the workpieces are respectively arranged in the front positioning groove 8-1 and the back positioning groove 8-2 in a matching manner, the expansion block 2 is used for limiting. The vertex angles of the bending parts of the front positioning groove 8-1 and the back positioning groove 8-2 are provided with process spaces 8-3.
The connecting hole 9-1 and the positioning hole 5-1 are both constructed as a step counter bore, wherein a step surface of the positioning hole 5-1 is provided with a threaded hole, the step surface of the positioning hole 5-1 is positioned and provided with a connecting sleeve 6, and the connecting sleeve 6 is fixedly connected with the mounting plate 5 through a fastening bolt 7.
The shaft sleeve 4 is arranged on the step surface of the connecting hole 9-1, and the connecting bolt 3 penetrates through the shaft sleeve 4 and then is in threaded connection with the connecting sleeve 6, so that the base 9 is fixedly connected with the mounting plate 5.
The base 9 is provided with two front positioning grooves 8-1 and two back positioning grooves 8-2.
As shown in figures 1 and 2, when in use, a workpiece 1 is respectively arranged in a front positioning groove 8-1 and a back positioning groove 8-2, and after the workpiece 1 is arranged, the workpiece 1 is reliably positioned by an expansion block 2. A plurality of inflation pieces 2 set gradually in constant head tank 8, fix a position work piece 1 reliably steadily, utilize the fixed point atress of inflation piece 2, guarantee that the work piece is indeformable to reach disposable quick processing twice process.
Claims (4)
1. The utility model provides an aviation seat support adds clamping apparatus which characterized in that: the device comprises a mounting plate (5), wherein a base (9) is arranged on the upper surface of the mounting plate (5), a plurality of positioning holes (5-1) are formed in the mounting plate (5), a connecting hole (9-1) is formed in the base (9), and the connecting hole (9-1) in the base (9) is aligned with the corresponding positioning hole (5-1) in the mounting plate (5) and then fixedly connected through a connecting component;
the base (9) is provided with a positioning groove (8), the positioning groove (8) comprises a front positioning groove (8-1) and a back positioning groove (8-2), and the front positioning groove (8-1) and the back positioning groove (8-2) are respectively arranged on the two sides of the base (9) corresponding to the connecting line of the two connecting holes (9-1);
and after the workpieces are respectively matched and arranged in the front positioning groove (8-1) and the back positioning groove (8-2), the workpieces are limited through the expansion block (2).
2. The aircraft seat support machining jig of claim 1, characterized in that: the connecting hole (9-1) and the positioning hole (5-1) are both constructed as step counter bores, wherein the step surface of the positioning hole (5-1) is provided with a threaded hole, the step surface of the positioning hole (5-1) is positioned and provided with a connecting sleeve (6), and the connecting sleeve (6) is fixedly connected with the mounting plate (5) through a fastening bolt (7);
the shaft sleeve (4) is arranged on the step surface of the connecting hole (9-1), and the connecting bolt (3) penetrates through the shaft sleeve (4) and then is in threaded connection with the connecting sleeve (6), so that the base (9) is fixedly connected with the mounting plate (5).
3. The aircraft seat support machining jig of claim 1, characterized in that: the base (9) is provided with two front positioning grooves (8-1) and two back positioning grooves (8-2).
4. An airline seat bracket machining jig as claimed in claim 3, wherein: and process spaces (8-3) are arranged at the vertex angles of the bending parts of the front positioning groove (8-1) and the back positioning groove (8-2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122451524.0U CN215880864U (en) | 2021-10-11 | 2021-10-11 | Aviation seat support adds clamping apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122451524.0U CN215880864U (en) | 2021-10-11 | 2021-10-11 | Aviation seat support adds clamping apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215880864U true CN215880864U (en) | 2022-02-22 |
Family
ID=80250055
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122451524.0U Active CN215880864U (en) | 2021-10-11 | 2021-10-11 | Aviation seat support adds clamping apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215880864U (en) |
-
2021
- 2021-10-11 CN CN202122451524.0U patent/CN215880864U/en active Active
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