CN218556336U - Adjustable pressure testing device for aviation part machining - Google Patents
Adjustable pressure testing device for aviation part machining Download PDFInfo
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- CN218556336U CN218556336U CN202222999449.6U CN202222999449U CN218556336U CN 218556336 U CN218556336 U CN 218556336U CN 202222999449 U CN202222999449 U CN 202222999449U CN 218556336 U CN218556336 U CN 218556336U
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- adjusting box
- adjustable pressure
- rotating shaft
- gear
- pressure testing
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Abstract
The utility model discloses an adjustable pressure testing tight device of aviation spare part processing, comprising a base plate, be equipped with the cavity in the bottom plate, be equipped with the motor in the cavity, it is equipped with by motor drive's pivot one to peg graft on the bottom plate, the top of pivot one is equipped with gear one, the top of bottom plate is equipped with the regulating box, be equipped with pivot two between regulating box and the bottom plate, be equipped with in the pivot two with gear one meshing gear two, the both ends of two-way screw rod all are equipped with the movable block, the bottom of movable block is equipped with guide structure, the top of regulating box is equipped with the opening, the top of movable block is equipped with and passes open-ended connecting rod, the top of connecting rod all is equipped with fixed knot and constructs. Compared with the prior art, the utility model the advantage lie in: not only conveniently compress tightly fixedly to the spare part of size difference, the debuggability is strong, can accomplish the processing on all surfaces of spare part in a location compresses tightly moreover, and it is convenient to use, and the flexibility is strong.
Description
Technical Field
The utility model relates to a spare part processing technology field specifically indicates an adjustable pressure testing tight device of aviation spare part processing.
Background
In the aeronautical manufacturing field, a lot of aviation spare parts need compress tightly fixedly to it when production man-hour, and closing device commonly used is inconvenient compresses tightly fixedly to the spare part of size difference when using, influences result of use and application range, is adjusted the position of part when spare part is fixed back is inconvenient moreover, is not convenient for accomplish the processing to all surfaces of spare part, influences the convenience of using and the flexibility of device.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is overcome above technical defect, provide an adjustable pressure testing tight device of aviation spare part processing, not only conveniently compress tightly fixedly to the spare part of size difference, the debuggability is strong, can accomplish the processing on all surfaces of spare part in a location compresses tightly moreover, and it is convenient to use, and the flexibility is strong.
In order to solve the technical problem, the utility model provides a technical scheme does: the utility model provides an adjustable pressure testing tight device of aviation spare part processing, includes the bottom plate, be equipped with the cavity in the bottom plate, be equipped with the motor in the cavity, it is equipped with by motor drive's pivot one to peg graft on the bottom plate, the top of pivot one is equipped with gear one, the top of bottom plate is equipped with the regulating box, be equipped with pivot two between regulating box and the bottom plate, be equipped with gear two with gear one meshing on the pivot two, be equipped with two-way screw rod in the regulating box, the both ends of two-way screw rod all are equipped with the movable block, the bottom of movable block is equipped with guide structure, the top of regulating box is equipped with the opening, the top of movable block is equipped with passes open-ended connecting rod, the top of connecting rod all is equipped with fixed knot and constructs.
As the improvement, the bottom four corners of bottom plate all is equipped with the supporting leg, and the four corners is firm, guarantees whole device stability.
As an improvement, the top end of the second rotating shaft is fixedly connected with the adjusting box, the bottom end of the second rotating shaft is rotatably connected with the bottom plate through a bearing, a motor can conveniently drive the adjusting box to rotate through the first gear and the second gear, and all surfaces of the cold part can be machined in one-time positioning and pressing.
As an improvement, the guide structure comprises that sliding blocks are arranged at the bottom of the moving block, and sliding grooves matched with the sliding blocks for use are formed in the adjusting box, so that the moving block is guided conveniently and is ensured to move left and right.
As an improvement, the fixed knot constructs including the equal concave block in top of connecting rod, peg graft threaded connection's bolt on the concave block, the bottom of bolt is equipped with the clamp plate, the bottom of clamp plate and the bottom all are equipped with the rubber pad in the concave block, can compress tightly fixedly to spare part, and the outer wall of spare part can be protected to the rubber pad, avoids causing the outward appearance damage of spare part because excessively compress tightly.
As an improvement, a rotating handle is arranged at one end of the bidirectional screw rod, which is positioned outside the adjusting box, so that the bidirectional screw rod can be driven to rotate conveniently.
Compared with the prior art, the utility model the advantage lie in: the handle is changeed in the rotation, drives two-way screw rod and does not stop the rotation, and the movable block that is located on two-way screw rod drives the spill piece through the connecting rod and removes, adjusts suitable distance, rotates the bolt and drives the clamp plate down, can conveniently compress tightly fixedly to the spare part of size difference, and the debugging nature is strong. The motor drives the adjusting box to rotate through the first rotating shaft, the first gear and the second gear, machining of all surfaces of parts can be completed in one-time positioning and pressing, and the device is convenient to use and high in flexibility.
Drawings
Fig. 1 is the utility model discloses a but aviation spare part processing debugging closing device's schematic structure diagram.
Fig. 2 is the utility model relates to a main view schematic diagram of the adjustable pressure testing device of aviation spare part processing.
Fig. 3 is the utility model discloses a but, a part A detail enlargements of tight device of aviation spare part processing adjustable pressure.
As shown in the figure: 1. a base plate; 2. supporting legs; 3. a cavity; 4. a motor; 5. a first rotating shaft; 6. a first gear; 7. an adjusting box; 8. a second rotating shaft; 9. a second gear; 10. a bidirectional screw; 11. a moving block; 12. a slider; 13. a chute; 14. an opening; 15. a connecting rod; 16. a concave block; 17. a bolt; 18. pressing a plate; 19. a rubber pad; 20. and (4) turning the handle.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
With reference to the accompanying drawing 1, an adjustable pressure testing device for aviation part processing comprises a bottom plate 1, a cavity 3 is arranged in the bottom plate 1, a motor 4 is arranged in the cavity 3, a first rotating shaft 5 driven by the motor 4 is inserted and connected onto the bottom plate 1, a first gear 6 is arranged at the top end of the first rotating shaft 5, an adjusting box 7 is arranged above the bottom plate 1, a second rotating shaft 8 is arranged between the adjusting box 7 and the bottom plate 1, a second gear 9 meshed with the first gear 6 is arranged on the second rotating shaft 8, a bidirectional screw 10 is arranged in the adjusting box 7, moving blocks 11 are arranged at two ends of the bidirectional screw 10, a guide structure is arranged at the bottom of each moving block 11, an opening 14 is arranged at the top of the adjusting box 7, a connecting rod 15 penetrating through the opening 14 is arranged at the top end of each moving block 11, and a fixing structure is arranged at the top end of each connecting rod 15.
With reference to fig. 2, in order to ensure the stability of the whole device, four corners of the bottom plate 1 are provided with support legs 2.
With reference to fig. 2, the top end of the second rotating shaft 8 is fixedly connected with the adjusting box 7, and the bottom end of the second rotating shaft 8 is rotatably connected with the bottom plate 1 through a bearing, so as to drive the adjusting box to rotate.
With reference to fig. 3, the guide structure includes that the bottom of the moving block 11 is provided with a sliding block 12, and the adjusting box 7 is provided with a sliding groove 13 used in cooperation with the sliding block 12 for guiding and limiting the moving block.
With reference to fig. 1, the fixing structure includes a top-end concave block 16 of the connecting rod 15, a bolt 17 in threaded connection is inserted into the concave block 16, a pressing plate 18 is arranged at the bottom end of the bolt 17, rubber pads 19 are arranged at the bottom of the pressing plate 18 and the bottom of the concave block 16 and used for pressing and fixing, and the rubber pads can protect the appearance of the parts and avoid damage caused by pressing.
Referring to fig. 1, in order to facilitate the rotation of the bidirectional screw, a rotating handle 20 is disposed at one end of the bidirectional screw 10 located outside the adjusting box 7.
The utility model discloses when concrete implementation, the user rotates and changes the handle, drives the incessant rotation of two-way screw rod, and the movable block that is located on the two-way screw rod can drive through the connecting rod and control about the spill piece under the spacing of slider and spout, and the size of the spare part that can process as required adjusts the distance between the movable block of both sides in a flexible way, places spare part in the middle of the spill piece of both sides. The bolt is rotated to drive the pressing plate to descend, and parts needing to be processed can be pressed and fixed.
When other parts of the part need to be processed, the motor is started, the motor drives the first rotating shaft to rotate ceaselessly, the first gear rotates ceaselessly, the first gear is rotated ceaselessly, the second gear meshed with the first gear is rotated ceaselessly, the second rotating shaft is driven to rotate ceaselessly, and the bottom end and the bottom plate of the second rotating shaft are fixedly connected through the bearing, so that the adjusting box can be driven to rotate, the processing of all surfaces of the part is guaranteed to be completed in one-time positioning and pressing, and the device is convenient to use and high in flexibility.
Because the bottom of clamp plate and the bottom all has the rubber pad in the spill piece, can play the guard action to the spare part, avoid causing spare part outward appearance damage because excessively compress tightly.
The present invention and the embodiments thereof have been described above, but the description is not limited thereto, and the embodiment shown in the drawings is only one of the embodiments of the present invention, and the actual structure is not limited thereto. In summary, those skilled in the art should understand that they should not be limited to the embodiments described above, and that they can design the similar structure and embodiments without departing from the spirit of the invention.
Claims (6)
1. The utility model provides an adjustable pressure tight device of aviation spare part processing which characterized in that: the novel adjustable type motor is characterized by comprising a base plate (1), a cavity (3) is formed in the base plate (1), a motor (4) is arranged in the cavity (3), a first rotating shaft (5) driven by the motor (4) is arranged on the base plate (1) in an inserted mode, a first gear (6) is arranged on the top end of the first rotating shaft (5), an adjusting box (7) is arranged above the base plate (1), a second rotating shaft (8) is arranged between the adjusting box (7) and the base plate (1), a second gear (9) meshed with the first gear (6) is arranged on the second rotating shaft (8), a bidirectional screw rod (10) is arranged in the adjusting box (7), moving blocks (11) are arranged at two ends of the bidirectional screw rod (10), a guide structure is arranged at the bottom of each moving block (11), an opening (14) is formed in the top of the adjusting box (7), a connecting rod (15) penetrating through the opening (14) is arranged at the top end of each moving block (11), and a fixing structure is arranged at the top end of each connecting rod (15).
2. The aviation part machining adjustable pressure testing device of claim 1, characterized in that: the bottom four corners of the bottom plate (1) are provided with supporting legs (2).
3. The aviation part machining adjustable pressure testing device of claim 1, characterized in that: the top end of the second rotating shaft (8) is fixedly connected with the adjusting box (7), and the bottom end of the second rotating shaft (8) is rotatably connected with the bottom plate (1) through a bearing.
4. The adjustable pressure testing device for aviation part processing according to claim 1, characterized in that: the guide structure comprises sliding blocks (12) arranged at the bottoms of the moving blocks (11), and sliding grooves (13) matched with the sliding blocks (12) for use are formed in the adjusting box (7).
5. The aviation part machining adjustable pressure testing device of claim 1, characterized in that: the fixing structure comprises a top end uniform concave block (16) of the connecting rod (15), a bolt (17) in threaded connection is inserted in the concave block (16), a pressing plate (18) is arranged at the bottom end of the bolt (17), and rubber pads (19) are arranged at the bottom of the pressing plate (18) and the inner bottom of the concave block (16).
6. The adjustable pressure testing device for aviation part processing according to claim 1, characterized in that: and a rotating handle (20) is arranged at one end of the bidirectional screw (10) outside the adjusting box (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222999449.6U CN218556336U (en) | 2022-11-11 | 2022-11-11 | Adjustable pressure testing device for aviation part machining |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222999449.6U CN218556336U (en) | 2022-11-11 | 2022-11-11 | Adjustable pressure testing device for aviation part machining |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218556336U true CN218556336U (en) | 2023-03-03 |
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ID=85324342
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222999449.6U Active CN218556336U (en) | 2022-11-11 | 2022-11-11 | Adjustable pressure testing device for aviation part machining |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218556336U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116494170A (en) * | 2023-06-29 | 2023-07-28 | 四川省嘉绮瑞航空装备有限公司 | Positioning and clamping device for assembling front flap in airplane |
-
2022
- 2022-11-11 CN CN202222999449.6U patent/CN218556336U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116494170A (en) * | 2023-06-29 | 2023-07-28 | 四川省嘉绮瑞航空装备有限公司 | Positioning and clamping device for assembling front flap in airplane |
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