CN220145316U - Aerospace metal part processingequipment - Google Patents
Aerospace metal part processingequipment Download PDFInfo
- Publication number
- CN220145316U CN220145316U CN202321640274.8U CN202321640274U CN220145316U CN 220145316 U CN220145316 U CN 220145316U CN 202321640274 U CN202321640274 U CN 202321640274U CN 220145316 U CN220145316 U CN 220145316U
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- positioning
- groove
- clamping
- jack catch
- screw
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- 239000002184 metal Substances 0.000 title claims abstract description 32
- 238000003754 machining Methods 0.000 claims description 16
- 210000000078 claw Anatomy 0.000 claims description 12
- 230000003044 adaptive effect Effects 0.000 claims 2
- 230000000694 effects Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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- Jigs For Machine Tools (AREA)
Abstract
The utility model provides an aerospace metal part processingequipment, includes processing platform, side brace table, rotation positioning disk, length location fixture block, location carrier block, location jack catch, angle location slider, jack catch drive piece, gangbar, jack catch driven platform, drive screw, the inside anti-rotation draw-in groove that has of location carrier block, anti-rotation draw-in groove suits with the jack catch drive piece, anti-rotation draw-in groove connects the jack catch drive piece, the jack catch drive piece is at the inside slip of anti-rotation draw-in groove, the location carrier block front portion has the jack catch connection pad, jack catch connection pad surface has the jack catch constant head tank, location jack catch rear portion has the jack catch positioning table, the jack catch positioning table suits with the jack catch constant head tank, jack catch positioning table slides in jack catch constant head tank inside, jack catch positioning table rear portion has the jack catch driven platform.
Description
Technical Field
The utility model relates to the field of aerospace component machining, in particular to an aerospace metal component machining device.
Background
The prior patent (publication number: CN 213352159U) proposes an aerospace metal part processing device, which comprises a fixed seat, bearings a are embedded and fixedly connected in the inner parts of the two sides, which are close to the fixed seat, two bearings a are connected with a rotating shaft in a common rotation mode, one end of the rotating shaft extends out of the fixed seat and is fixedly connected with a hand wheel, two worms are fixedly arranged on the outer side wall of the rotating shaft, the two worms are respectively meshed with two worm wheels, however, the device is used for clamping a workpiece by moving a clamping plate, the clamping plate is of a flat-plate design, the metal part is fixed by virtue of friction, and the types and the tightness of the processable part are limited.
Disclosure of Invention
The utility model aims at the defects in the prior art, and provides the aerospace metal part processing device which can clamp the metal part through the positioning claw when the aerospace metal part is required to be processed, adopts a V-shaped structure and has the surface of a multi-arc splicing design, so that the device can be clamped on the inner ring, the outer ring and the side surface according to the requirements when the device is used for processing the barrel-shaped metal, and has larger contact area when the inner ring, the outer ring and the side surface are clamped, the clamping and positioning effects of the device are ensured, the overall adaptability is strong, and the processing is stable.
The utility model aims at realizing the following technical scheme:
the utility model provides an aerospace metal part processingequipment, includes processing platform, side brace table, rotation positioning disk, length location fixture block, location carrier block, location jack catch, angle location slider, jack catch drive piece, gangbar, jack catch driven platform, drive screw, the inside anti-rotation draw-in groove that has of location carrier block, anti-rotation draw-in groove suits with the jack catch drive piece, anti-rotation draw-in groove connects the jack catch drive piece, the jack catch drive piece slides inside anti-rotation draw-in groove, the location carrier block front portion has the jack catch connection pad, jack catch connection pad surface has the jack catch constant head tank, location jack catch rear portion has the jack catch positioning platform, the jack catch positioning platform suits with the jack catch constant head tank, jack catch positioning platform connects the jack catch constant head tank, jack catch positioning platform slides in jack catch constant head tank inside, jack catch driven platform rear portion has the upper rotation connection platform, jack catch drive piece outside has the lower rotation connection platform, the gangbar bottom rotates with the lower rotation connection platform.
The linkage rod top rotates with last rotation connection platform to be connected, and the jack catch connection pad middle part has the screw rod spread groove, and the drive screw front portion has the screw rod spread groove, and the screw rod spread groove suits with the screw rod spread groove, and the screw rod spread groove is connected to the screw rod spread groove, and the screw rod spread groove is inside to rotate.
Advantageous effects
1. When the aerospace metal part is required to be processed, the metal part can be clamped by the positioning clamping jaws, the positioning clamping jaws are of a V-shaped structure, and the surfaces of the positioning clamping jaws are of a multi-arc splicing design, so that the device can be clamped on the inner ring, the outer ring and the side surfaces according to requirements when the device faces the barrel-shaped metal to be processed, and the inner ring, the outer ring and the side surfaces are clamped with larger contact areas, so that the clamping and positioning effects of the device are guaranteed, the overall adaptability is strong, and the processing is stable.
2. The jaw driving block is adapted to the anti-rotation clamping groove, so that the jaw driving block can not rotate and only longitudinally slide when driven by the driving screw, and the jaw driving block can smoothly drive the linkage rod to change the angle, thereby adjusting the interval between the positioning jaws and ensuring the working stability of the device.
3. According to the utility model, when the angle positioning clamping groove is sleeved outside the angle positioning clamping rod, the part is clamped, so that the processing of the aerospace metal part is facilitated, when the lifting platform is driven to lift the angle positioning sliding block to enable the angle positioning clamping groove to be separated from the angle positioning clamping rod, the rotating positioning disc can freely rotate, and the angle change of the aerospace metal part is facilitated, so that the processing of the device is more convenient.
4. The sliding support table slides on the processing table, so that the device can adapt to clamping and positioning of parts with different lengths, and the adaptability of the device is further improved.
Drawings
FIG. 1 is a schematic structural view of an aerospace metal part processing apparatus according to the present utility model.
FIG. 2 is a side view of an aerospace metal part tooling assembly according to the present utility model.
Fig. 3 is a front view, partially in cross section, of an aerospace metal part tooling device according to the present utility model.
Fig. 4 is a schematic structural view of a clamping mechanism of an aerospace metal part machining device according to the utility model.
Fig. 5 is a partial exploded view of an aerospace metal part tooling assembly according to the present utility model.
Fig. 6 is a schematic diagram of the structure of the jaw driving block according to the present utility model.
Fig. 7 is a schematic structural diagram of a positioning carrier block according to the present utility model.
Fig. 8 is a schematic view of a positioning claw structure according to the present utility model.
Fig. 9 is a schematic view of an angular positioning slider according to the present utility model.
Description of the embodiments
The utility model is described in further detail below with reference to the drawings and examples:
examples
The aerospace metal part machining device comprises a machining table 1, a side supporting table 4, a rotary positioning disk 6, a length positioning clamping block 7, a positioning bearing block 8, a positioning clamping jaw 10, an angle positioning sliding block 16, a clamping jaw driving block 19, a linkage rod 21, a clamping jaw driven table 22 and a driving screw 26, wherein an anti-rotation clamping groove 25 is formed in the positioning bearing block 8, the anti-rotation clamping groove 25 is adapted to the clamping jaw driving block 19, the anti-rotation clamping groove 25 is connected with the clamping jaw driving block 19, the clamping jaw driving block 19 slides in the anti-rotation clamping groove 25, the clamping jaw driving block 19 is adapted to the anti-rotation clamping groove 25, the clamping jaw driving block 19 can not rotate by itself when driven by the driving screw 26 and only can slide longitudinally, the clamping jaw driving block 19 can smoothly drive the linkage rod 21 to change the angle, the distance between the positioning clamping jaws 10 is adjusted, and the working stability of the device is ensured, the front part of the positioning bearing block 8 is provided with a jaw connecting disc 9, the surface of the jaw connecting disc 9 is provided with a jaw positioning groove 23, the rear part of the positioning jaw 10 is provided with a jaw positioning table 29, when the aerospace metal part is required to be processed, the metal part can be clamped by the positioning jaw 10, the positioning jaw 10 adopts a V-shaped structure, and the surface is in multi-arc splicing design, so that the device can be clamped on an inner ring, an outer ring and a side surface according to the requirement when processing the barrel-shaped metal, and the inner ring, the outer ring and the side surface are clamped with larger contact areas, thereby ensuring the clamping positioning effect of the device, having strong overall adaptability and stable processing, the jaw positioning table 29 is suitable for the jaw positioning groove 23, the jaw positioning table 29 is connected with the jaw positioning groove 23, the jaw positioning table 29 slides in the jaw positioning groove 23, the rear part of the jaw positioning table 29 is provided with a jaw driven table 22, the side of the jaw driven table 22 is provided with an upper rotating connecting table 20, the outer side of the jaw driving block 19 is provided with a lower rotating connecting table 28, and the bottom of the linkage rod 21 is rotationally connected with the lower rotating connecting table 28.
Examples
The top of the linkage rod 21 is rotationally connected with the upper rotating connecting table 20, the middle part of the claw connecting disc 9 is provided with a screw connecting groove 27, the front part of the driving screw 26 is provided with a screw connecting table 24, the screw connecting table 24 is matched with the screw connecting groove 27, the screw connecting table 24 is connected with the screw connecting groove 27, the screw connecting table 24 rotates in the screw connecting groove 27, the inside of the claw driving block 19 is in threaded connection with the driving screw 26, the rear part of the driving screw 26 is provided with a driving knob 12, the rear part of the positioning bearing block 8 is fixedly connected with the rotating positioning disc 6, the inside of the side supporting table 4 is provided with a rotating connecting groove 5, the rotating connecting groove 5 is matched with the rotating positioning disc 6, the rotating positioning disc 6 is connected with the rotating connecting groove 5, and the rotating positioning disc 6 rotates in the rotating connecting groove 5.
Examples
The upper part of the rotary connecting groove 5 is provided with a clamping rod connecting groove 15, the side surface of the clamping rod connecting groove 15 is provided with a lifting sliding groove 13, the clamping rod connecting groove 15 is matched with an angle positioning sliding block 16, the clamping rod connecting groove 15 is connected with the angle positioning sliding block 16, the angle positioning sliding block 16 slides in the clamping rod connecting groove 15, the side surface of the angle positioning sliding block 16 is provided with a lifting table 14, the lifting sliding groove 13 is matched with the lifting table 14, the lifting table 14 is connected with the lifting sliding groove 13, the lifting table 14 slides in the lifting sliding groove 13, and the outer side of the rotary positioning disc 6 is provided with an angle positioning clamping rod 18.
Examples
According to the utility model, the lower side of the angle positioning slide block 16 is provided with the angle positioning clamping groove 17, the angle positioning clamping groove 17 is matched with the angle positioning clamping rod 18, the angle positioning clamping groove 17 is connected with the angle positioning clamping rod 18, the angle positioning clamping groove 17 is sleeved outside the angle positioning clamping rod 18, when the angle positioning clamping groove 17 is sleeved outside the angle positioning clamping rod 18, a part is clamped, so that the processing of an aerospace metal part is facilitated, when the lifting table 14 is driven to lift the angle positioning slide block 16 to enable the angle positioning clamping groove 17 to be separated from the angle positioning clamping rod 18, the rotating positioning disk 6 can freely rotate, the angle change of the aerospace metal part is facilitated, the processing of the device is more convenient, the lower side of the side supporting table 4 is provided with the sliding supporting table 3, the bottom of the processing table 1 is provided with the supporting leg 2, and the processing table 1 is matched with the sliding supporting table 3.
Examples
According to the utility model, the processing table 1 is connected with the sliding support table 3, the sliding support table 3 slides outside the processing table 1, and the sliding support table 3 slides on the processing table 1, so that the device can adapt to clamping and positioning of parts with different lengths, the adaptability of the device is further improved, the front part of the sliding support table 3 is provided with the screw positioning table 30, the rear part of the length positioning clamping block 7 is provided with the threaded clamping rod 11, the threaded clamping rod 11 is in threaded connection with the screw positioning table 30, and the threaded clamping rod 11 is tightly pressed on the side surface of the processing table 1.
Examples
The utility model comprises the following steps: the method comprises the steps of inserting a claw positioning table 29 of a positioning claw 10 into a claw positioning groove 23 of a positioning bearing block 8, inserting a claw driving block 19 into an anti-rotation clamping groove 25 of the positioning bearing block 8, inserting an angle positioning slide block 16 into a clamping rod connecting groove 15 of the side supporting table 4, enabling an angle positioning slide block 16 to be provided with an angle positioning clamping rod 18 outside the rotating positioning clamping rod 18 of the side supporting table 4, enabling a screw rod connecting table 24 of a driving screw rod 26 to be rotatably connected with a screw rod connecting groove 27 of the positioning bearing block 8, enabling the driving screw rod 26 to be in threaded connection with the inside of the claw driving block 19, fixedly connecting the rear of the positioning bearing block 8 with the rotating positioning disk 6, inserting the rotating positioning disk 6 into the rotating connecting groove 5 of the side supporting table 4, inserting the angle positioning slide block 16 into a lifting slide groove 13 of the side supporting table 4, enabling the angle positioning slide block 16 to be provided with the angle positioning clamping groove 17 to be sleeved outside the lifting slide groove 13 of the side supporting table 4, enabling the sliding support table 3 to be provided with the clamping rod 11 to be provided with a clamping rod 3, and installing the clamping rod 11 to be provided with a clamping groove 30, and completing the threaded connection device.
The above description is only of the preferred embodiments of the present utility model and is not intended to limit the present utility model, and it should be noted that it is possible for those skilled in the art to make several improvements and modifications without departing from the technical principle of the present utility model, and these improvements and modifications should also be regarded as the protection scope of the present utility model.
Claims (5)
1. The aerospace metal part machining device is characterized by comprising a machining table (1), a side supporting table (4), a rotary positioning disc (6), a length positioning clamping block (7), a positioning bearing block (8), a positioning clamping jaw (10), an angle positioning sliding block (16), a clamping jaw driving block (19), a linkage rod (21), a clamping jaw driven table (22) and a driving screw (26), wherein an anti-rotation clamping groove (25) is formed in the positioning bearing block (8), the anti-rotation clamping groove (25) is adaptive to the clamping jaw driving block (19), the anti-rotation clamping groove (25) is connected with the clamping jaw driving block (19), the clamping jaw driving block (19) slides in the anti-rotation clamping groove (25), a clamping jaw connecting disc (9) is arranged at the front part of the positioning bearing block (8), a clamping jaw positioning groove (23) is formed in the surface of the clamping jaw connecting disc (9), a clamping jaw positioning clamping jaw (10) is provided with a clamping jaw positioning table (29), the positioning table (29) is adaptive to the clamping jaw positioning groove (23), the clamping jaw (29) is connected with the clamping jaw positioning groove (23), the positioning table (29) slides in the positioning table (23), the clamping jaw (29) slides in the positioning table (23), the side surface of the clamping jaw (22) is provided with the driven table (22), the outer side of the claw driving block (19) is provided with a lower rotating connecting table (28), and the bottom of the linkage rod (21) is rotationally connected with the lower rotating connecting table (28).
2. The aerospace metal part machining device is characterized in that the top of the linkage rod (21) is rotationally connected with the upper rotating connecting table (20), a screw connecting groove (27) is formed in the middle of the claw connecting table (9), a screw connecting table (24) is arranged at the front of the driving screw (26), the screw connecting table (24) is matched with the screw connecting groove (27), the screw connecting table (24) is connected with the screw connecting groove (27), the screw connecting table (24) rotates in the screw connecting groove (27), the claw driving block (19) is internally connected with the driving screw (26) in a threaded mode, a driving knob (12) is arranged at the rear of the driving screw (26), the rear of the positioning bearing block (8) is fixedly connected with the rotating positioning disc (6), a rotating connecting groove (5) is formed in the side supporting table (4), the rotating connecting groove (5) is matched with the rotating positioning disc (6), the rotating positioning disc (6) is connected with the rotating positioning disc (6), and the rotating positioning disc (6) rotates in the rotating position inside the rotating connecting groove (5).
3. The aerospace metal part machining device according to claim 2, wherein the upper portion of the rotating connecting groove (5) is provided with a clamping rod connecting groove (15), the side face of the clamping rod connecting groove (15) is provided with a lifting sliding groove (13), the clamping rod connecting groove (15) is matched with an angle positioning sliding block (16), the clamping rod connecting groove (15) is connected with the angle positioning sliding block (16), the angle positioning sliding block (16) slides in the clamping rod connecting groove (15), the side face of the angle positioning sliding block (16) is provided with a lifting table (14), the lifting sliding groove (13) is matched with the lifting table (14), the lifting table (14) slides in the lifting sliding groove (13), and the outer side of the rotating positioning disc (6) is provided with an angle positioning clamping rod (18).
4. The aerospace metal part machining device according to claim 3, wherein the angle positioning sliding block (16) is provided with an angle positioning clamping groove (17) at the lower side, the angle positioning clamping groove (17) is matched with an angle positioning clamping rod (18), the angle positioning clamping groove (17) is connected with the angle positioning clamping rod (18), the angle positioning clamping groove (17) is sleeved on the outer side of the angle positioning clamping rod (18), the sliding supporting table (3) is arranged at the lower side of the side supporting table (4), the supporting leg (2) is arranged at the bottom of the machining table (1), and the machining table (1) is matched with the sliding supporting table (3).
5. The aerospace metal part machining device according to claim 1, wherein the machining table (1) is connected with a sliding support table (3), the sliding support table (3) slides outside the machining table (1), a screw positioning table (30) is arranged at the front part of the sliding support table (3), a threaded clamping rod (11) is arranged at the rear part of the length positioning clamping block (7), the threaded clamping rod (11) is in threaded connection with the screw positioning table (30), and the threaded clamping rod (11) is pressed on the side face of the machining table (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321640274.8U CN220145316U (en) | 2023-06-27 | 2023-06-27 | Aerospace metal part processingequipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321640274.8U CN220145316U (en) | 2023-06-27 | 2023-06-27 | Aerospace metal part processingequipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220145316U true CN220145316U (en) | 2023-12-08 |
Family
ID=89015973
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321640274.8U Active CN220145316U (en) | 2023-06-27 | 2023-06-27 | Aerospace metal part processingequipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220145316U (en) |
-
2023
- 2023-06-27 CN CN202321640274.8U patent/CN220145316U/en active Active
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