CN217371403U - Automatic reloading jig for machining aviation parts - Google Patents
Automatic reloading jig for machining aviation parts Download PDFInfo
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- CN217371403U CN217371403U CN202122498234.1U CN202122498234U CN217371403U CN 217371403 U CN217371403 U CN 217371403U CN 202122498234 U CN202122498234 U CN 202122498234U CN 217371403 U CN217371403 U CN 217371403U
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P90/00—Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
- Y02P90/30—Computing systems specially adapted for manufacturing
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Abstract
The utility model discloses an automatic reloading jig for aviation part machining, which comprises a positioning seat and a plurality of positioning components, wherein the top end of the positioning seat is formed into a positioning surface, and the plurality of positioning components are arranged on the positioning surface; the positioning components are distributed at intervals in the width direction of the positioning surface; the positioning assembly comprises two adjusting rods and two positioning blocks, and the two adjusting rods are distributed at intervals in the length direction of the positioning surface; the adjusting rod can move along the height direction of the positioning seat; one end of each of the two positioning blocks is respectively arranged at the top ends of the two adjusting rods; the other ends of the two positioning blocks are both formed into positioning ends. The utility model discloses an automatic tool that reloads for aviation parts machining, it can the different part of clamping, and the clamping is efficient.
Description
Technical Field
The utility model relates to an aviation parts machining equipment technical field especially relates to an automatic tool that reloads for aviation parts machining.
Background
Along with the continuous development of aerospace technologies in China, the requirements on the quality and efficiency of aerospace part machining processes are continuously improved, and efficient machining becomes a key technology of part machining processes. If the traditional clamping is used in the processing, the processing efficiency is low, and the applicability is poor. In addition, the traditional clamping method can cause the machine tool to stop for too long time, so that the machine tool is insufficient in productivity, and the requirements of the parts are very huge.
SUMMERY OF THE UTILITY MODEL
In order to overcome the not enough of prior art, the utility model aims to provide an automatic tool that reloads for aviation parts machining, its part that can the clamping be different, and the clamping is efficient.
The purpose of the utility model is realized by adopting the following technical scheme:
an automatic reloading jig for machining aviation parts comprises a positioning seat and a plurality of positioning components, wherein the top end of the positioning seat is formed into a positioning surface, and the plurality of positioning components are arranged on the positioning surface; the positioning components are distributed at intervals in the width direction of the positioning surface; the positioning assembly comprises two adjusting rods and two positioning blocks, and the two adjusting rods are distributed at intervals in the length direction of the positioning surface; the adjusting rod can move along the height direction of the positioning seat; one end of each positioning block is respectively arranged at the top ends of the two adjusting rods; the other ends of the two positioning blocks are both formed into positioning ends.
Furthermore, the positioning block is provided with an adjusting hole, and the adjusting hole extends along the length direction of the positioning surface; the adjusting hole is internally provided with a positioning piece which can slide and is connected in a penetrating way.
Further, the positioning member is formed of a positioning bolt.
Furthermore, the heights of the adjusting rods of the positioning assemblies are sequentially reduced in the width direction of the positioning surface.
Furthermore, the automatic reloading jig for machining the aviation parts further comprises a base, wherein at least two positioning holes are formed in the base and are distributed at intervals around the circumference of the central axis of the base; the bottom end of the positioning seat is provided with at least two positioning pins; the at least two positioning pins are used for being correspondingly inserted into the at least two positioning holes one by one.
Further, this an automatic tool that reloads for aviation parts machining still includes the clamping board, be equipped with a plurality of clamping holes on the clamping board, the base is equipped with the connecting piece, the connecting piece is used for cartridge to downthehole to one of them clamping.
Compared with the prior art, the beneficial effects of the utility model reside in that: when the workpiece is clamped, the workpiece can be placed on the positioning surface, each section of the workpiece in the width direction can be correspondingly placed at each positioning assembly, two positioning blocks of each positioning assembly can be positioned in the length direction of the workpiece, when the clamping is fixed, the adjusting rod can move downwards, the positioning ends of the positioning blocks are tightly pressed on two sides of the corresponding position of the workpiece, the positioning clamping is realized, and the clamping efficiency is high.
The adjusting rod can move up and down, so that the clamping height of the positioning block can be adjusted according to different thicknesses of workpieces, the positioning block is suitable for clamping different workpieces, and the application range is wider.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic structural view of the base of the present invention;
fig. 3 is a schematic structural view of the clamping plate of the present invention.
In the figure: 10. positioning seats; 21. positioning blocks; 211. an adjustment hole; 22. adjusting a rod; 23. a positioning member; 30. a base; 31. positioning holes; 40. installing a clamping plate; 41. and (4) clamping holes.
Detailed Description
The invention will be further described with reference to the following drawings and detailed description:
as shown in fig. 1, fig. 2 and fig. 3, the automatic reloading jig for machining aviation parts comprises a positioning seat 10 and a plurality of positioning assemblies, wherein the top end of the positioning seat 10 forms a positioning surface, and the positioning assemblies are mounted on the positioning surface.
The positioning assemblies are distributed at intervals in the width direction of the positioning surface and comprise two adjusting rods 22 and two positioning blocks 21, and the two adjusting rods 22 are distributed at intervals in the length direction of the positioning surface. In addition, the adjusting rods 22 can move along the height direction of the positioning base 10, and one end of the two positioning blocks 21 are respectively installed at the top ends of the two adjusting rods 22; the other ends of the two positioning blocks 21 are formed as positioning ends.
On the basis of the structure, use the utility model discloses an automatic tool that changes outfit for aviation parts machining, when carrying out the work piece clamping, the work piece can be placed at the locating surface, and each section of work piece width direction can correspond and place in each locating component department, and two locating pieces 21 of each locating component can fix a position in work piece length direction, and the clamping is fixed time, adjusts pole 22 and can downstream, compresses tightly the both sides that correspond the position at the work piece with the location end of locating piece 21, realizes the location clamping, and the clamping is efficient.
The adjusting rod 22 can move up and down, so that the clamping height of the positioning block 21 can be adjusted according to different thicknesses of workpieces, the adjustable clamping device is suitable for clamping different workpieces, and the application range is wider.
It should be noted that the adjusting rod 22 may be an adjusting screw rod in the prior art, a threaded hole is correspondingly formed on the positioning surface, the adjusting screw rod may be screwed into the threaded hole, and the adjusting screw rod may move up and down relative to the positioning seat 1O by rotating, so as to adjust the positioning block 21 up and down.
Specifically, when adjusting pole 22 upward movement, can drive the locating end upward movement of locating piece 21, the work piece clamping interval that forms between locating end and the locating surface can grow, and when adjusting pole 22 downward movement, can drive the locating end downward movement of locating piece 21, the work piece clamping interval that forms between locating end and the locating surface alright diminishes, when the work piece carries out the clamping promptly, the work piece can be arranged in each section on the width direction in the locating end of each group's locating component and the work piece clamping interval that the locating surface formed in correspondingly, the height of adjusting pole 22 is adjusted, alright realize the compressing tightly of locating piece 21 to the work piece or loosen the action, the clamping is convenient.
Furthermore, can also be equipped with regulation hole 211 on locating piece 21, this regulation hole 211 extends along the length direction of locating surface, can be equipped with slidable cross-under in regulation hole 211 and have setting element 23, that is to say, when carrying out the work piece clamping, the work piece is arranged in behind locating end and the locating surface of locating piece 21, can drive the setting end through adjusting pole 22 downstream on the one hand and compress tightly the work piece downwards, on the other hand, can further through setting element 23 fastening connection of regulation hole 211 on the work piece, the clamping structure is more stable.
Of course, since the positioning element 23 can slide in the adjusting hole 211, the position of the positioning element 23 in the length direction of the positioning surface can be adjusted, and thus, when pressing, the position of the positioning element 23 can be adjusted according to the length of the workpiece, so that the size of the workpiece is more suitable.
Furthermore, the positioning part 23 is formed by a positioning bolt, so that after the positioning block 21 is driven by the adjusting rod 22 to be pressed down on the workpiece, the positioning bolt can be in threaded fit with the adjusting hole 211, and the workpiece is further pressed by rotation, so that the clamping structure is more stable.
Furthermore, the heights of the adjusting rods 22 of the positioning assemblies are sequentially reduced in the width direction of the positioning surface, that is, the heights of the workpiece clamping intervals between the positioning blocks 21 and the positioning surface at corresponding positions are determined by the heights of the corresponding adjusting rods 22, so that the positioning device is suitable for clamping workpieces with multiple steps, and is wider in application range.
Further, the automatic reloading jig for machining aviation parts further comprises a base 30, at least two positioning holes 31 are formed in the base 30, the at least two positioning holes 31 are distributed around the circumference of the central axis of the base 30 at intervals, at least two positioning pins are correspondingly arranged at the bottom end of the positioning seat 10, and the at least two positioning pins are used for being correspondingly inserted into the at least two positioning holes 31 one by one.
The positioning seat 10 and the machine tool can be clamped through the base 30 each time, namely, after a workpiece is clamped to the positioning seat 10, the positioning pin at the bottom end of the positioning seat 10 can be correspondingly inserted into the positioning hole 31 in the base 30 to realize one-time positioning, and then the base 30 is directly clamped on the machine tool, so that the workpiece can be clamped through the positioning and clamping of the positioning seat 10 and the base 30 each time and then clamped with the machine tool, the workpiece is clamped on the machine tool at the same position each time, and the processing precision of the workpiece is higher.
Furthermore, the automatic reloading jig for machining aviation parts further comprises a clamping plate 40, a plurality of clamping holes 41 can be arranged on the clamping plate 40, in addition, the base 30 is provided with a connecting piece, so that when the positioning seat 10 and the base 30 are positioned and clamped, the base 30 can be connected with the clamping plate 40 by inserting the connecting piece at the bottom end of the base 30 into the clamping hole 41 corresponding to the clamping plate 40, specifically, the other clamping holes 41 on the clamping plate 40 can also be connected with a machine tool by the connecting piece, that is, the clamping plate 40 can be firstly clamped on the machine tool through the connecting piece, then the positioning seat 10 with the workpiece clamped thereon and the base 30 are clamped outside the machine tool, the base 30 is clamped on the clamping plate 40 through a connecting piece, the assembling position of the base 30 and the machine tool can be positioned and clamped every time, the positioning is more accurate, and the machining precision is further improved.
It should be noted that the specific connecting member may be one of the existing connecting members such as a bolt, or a screw, which is convenient for disassembly and assembly.
Various other modifications and changes can be made by those skilled in the art based on the above-described technical solutions and concepts, and all such modifications and changes should fall within the scope of the claims.
Claims (6)
1. An automatic reloading jig for machining aviation parts is characterized by comprising a positioning seat and a plurality of positioning components, wherein the top end of the positioning seat is formed into a positioning surface, and the positioning components are arranged on the positioning surface; the positioning components are distributed at intervals in the width direction of the positioning surface; the positioning assembly comprises two adjusting rods and two positioning blocks, and the two adjusting rods are distributed at intervals in the length direction of the positioning surface; the adjusting rod can move along the height direction of the positioning seat; one end of each of the two positioning blocks is respectively arranged at the top ends of the two adjusting rods; the other ends of the two positioning blocks are formed into positioning ends.
2. The automatic changing jig for the aviation component processing as claimed in claim 1, wherein the positioning block is provided with an adjusting hole, and the adjusting hole extends along a length direction of the positioning surface; the adjusting hole is internally provided with a positioning piece which can slide and is connected in a penetrating way.
3. The automatic reloading tool for machining aviation parts as claimed in claim 2, wherein said positioning member is formed by a positioning bolt.
4. The automatic reloading tool for machining aviation parts as claimed in claim 1, wherein the heights of the adjusting rods of the respective positioning assemblies are sequentially reduced in the width direction of the positioning surface.
5. The automatic reloading jig for aviation component processing as claimed in any one of claims 1 to 4, further comprising a base, wherein the base is provided with at least two positioning holes, and the at least two positioning holes are circumferentially distributed at intervals around a central axis of the base; the bottom end of the positioning seat is provided with at least two positioning pins; the at least two positioning pins are used for being correspondingly inserted into the at least two positioning holes one by one.
6. The automatic reloading jig for aviation part machining according to claim 5, wherein the automatic reloading jig for aviation part machining further comprises a clamping plate, a plurality of clamping holes are formed in the clamping plate, and the base is provided with a connecting piece which is used for being inserted into one of the clamping holes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122498234.1U CN217371403U (en) | 2021-10-15 | 2021-10-15 | Automatic reloading jig for machining aviation parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122498234.1U CN217371403U (en) | 2021-10-15 | 2021-10-15 | Automatic reloading jig for machining aviation parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217371403U true CN217371403U (en) | 2022-09-06 |
Family
ID=83083038
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122498234.1U Active CN217371403U (en) | 2021-10-15 | 2021-10-15 | Automatic reloading jig for machining aviation parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217371403U (en) |
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2021
- 2021-10-15 CN CN202122498234.1U patent/CN217371403U/en active Active
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