CN220093844U - Grinding fixture for engine cylinder cover of unmanned aerial vehicle - Google Patents

Grinding fixture for engine cylinder cover of unmanned aerial vehicle Download PDF

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Publication number
CN220093844U
CN220093844U CN202321587014.9U CN202321587014U CN220093844U CN 220093844 U CN220093844 U CN 220093844U CN 202321587014 U CN202321587014 U CN 202321587014U CN 220093844 U CN220093844 U CN 220093844U
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China
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fixedly connected
unmanned aerial
aerial vehicle
rod
screw rod
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CN202321587014.9U
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Chinese (zh)
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田晨
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Xi'an Topland Aviation Technology Co ltd
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Xi'an Topland Aviation Technology Co ltd
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Abstract

The utility model belongs to the technical field of unmanned aerial vehicles, in particular to a grinding clamp for an engine cylinder cover of an unmanned aerial vehicle, which aims at solving the problems that the conventional equipment is poor in general clamping effect and polishing and cutting are required to be carried out step by step. The utility model has simple operation and convenient use, can ensure better clamping effect, and can finish polishing and cutting in the box body.

Description

Grinding fixture for engine cylinder cover of unmanned aerial vehicle
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a grinding fixture for an engine cylinder cover of an unmanned aerial vehicle.
Background
Unmanned aerial vehicle's development is comparatively ripe to be applied to each field, like photographic, making a video recording etc. also be a part of its application with unmanned aerial vehicle is used for putting out a fire, and presents fine effect, uses manpower sparingly resource and less damage, and unmanned aerial vehicle engine cylinder cap is as unmanned aerial vehicle engine's important component, and its manufacturing process is very important. With the continuous improvement of the working strength, people also put forward higher requirements on the processing and manufacturing process of the engine cylinder cover.
The existing grinding clamp for the engine cylinder cover of the unmanned aerial vehicle is poor in clamping effect, and grinding and cutting are required to be carried out step by step, so that the grinding clamp for the engine cylinder cover of the unmanned aerial vehicle is provided.
Disclosure of Invention
The utility model aims to solve the defects that the conventional equipment is poor in clamping effect and polishing and cutting are required to be performed step by step, and provides a grinding clamp for an engine cylinder cover of an unmanned aerial vehicle.
In order to achieve the above purpose, the present utility model adopts the following technical scheme:
the utility model provides a grinding anchor clamps of unmanned aerial vehicle engine cylinder cap, includes the box, fixedly mounted has first motor on the side outer wall of box, fixedly connected with first transfer line on the output shaft of first motor, be connected with adjustment mechanism on the first transfer line, sliding connection has the brace table on the bottom inner wall of box, fixedly connected with second motor on the side of brace table, fixedly connected with second transfer line on the output shaft of second motor, be connected with fixture on the second transfer line, fixedly mounted has the cylinder on the top of box, be connected with first baffle on the piston of cylinder, sliding connection has the second baffle on the inner wall of first baffle and box, be connected with elevating system on first baffle and the second baffle, the rotation is connected with the bull stick on the inner wall of box.
Preferably, the adjusting mechanism comprises a first screw rod and a guide block, the first screw rod is fixedly sleeved on the first transmission rod, the guide block is in threaded connection with the first screw rod, and the guide block is fixedly connected with the supporting table.
Preferably, the clamping mechanism comprises a forward rotating screw rod, a reverse rotating screw rod and a guide rod, wherein the forward rotating screw rod and the reverse rotating screw rod are fixedly sleeved on the second transmission rod, the forward rotating screw rod and the reverse rotating screw rod are connected with sliding blocks in a threaded manner, and the guide rod is fixedly connected with the sliding blocks.
Preferably, the lifting mechanism comprises a first rack, a second rack and a gear, wherein the first rack is fixedly connected with the second guide plate, the second rack is fixedly connected with the first guide plate, the gear is in meshed connection with the first rack and the second rack, and the gear is sleeved on the rotating rod.
Preferably, the support platform is provided with a through hole, and the guide rod is matched with the through hole.
Preferably, the guide rod is fixedly connected with a push plate, the push plate is fixedly connected with a spring, the other end of the spring is fixedly connected with a clamping plate, and the clamping plate and the push plate are both in sliding connection with the supporting table.
Preferably, the bottom of the first guide plate is fixedly provided with a cutting knife, the top of the second guide plate is fixedly provided with a third motor, the output shaft of the third motor is fixedly provided with a third transmission rod, the third transmission rod is rotationally connected with the second guide plate, and the third transmission rod is fixedly connected with a polishing head.
Compared with the prior art, the utility model has the advantages that:
(1) This scheme is owing to set up corotation screw rod, reversal screw rod and guide arm, and the second transfer line rotates and drives corotation screw rod and reversal screw rod and rotate, and corotation screw rod and reversal screw rod drive the slider motion that corresponds through the threaded connection with corresponding slider, and the slider drives the guide arm motion, and the guide arm drives the push pedal motion, and the push pedal drives spring and splint motion to make unmanned aerial vehicle engine cylinder cap on the brace table obtain the centre gripping.
(2) According to the scheme, as the first rack, the gear and the second rack are arranged, the piston of the air cylinder drives the first guide plate to move, the first guide plate drives the second rack to move, the second rack drives the gear to rotate through being connected with the meshing of the gear, the gear drives the first rack to move through being connected with the meshing of the first rack, and the first rack drives the second guide plate to move, so that the box body can be subjected to polishing and cutting conversion.
The utility model has simple operation and convenient use, can ensure better clamping effect, and can finish polishing and cutting in the box body.
Drawings
Fig. 1 is a schematic structural view of a grinding fixture for an engine cylinder cover of an unmanned aerial vehicle;
fig. 2 is a schematic structural view of a support table of a grinding fixture for an engine cylinder cover of an unmanned aerial vehicle;
fig. 3 is a schematic top view of a support table of a grinding fixture for an engine cylinder cover of an unmanned aerial vehicle.
In the figure: 1. a case; 2. a first motor; 3. a second motor; 4. a third motor; 5. a cylinder; 6. a first transmission rod; 7. a first screw; 8. a second transmission rod; 9. a third transmission rod; 10. a cutting knife; 11. a first guide plate; 12. a second guide plate; 13. polishing head; 14. a guide block; 15. a support table; 16. a first rack; 17. a second rack; 18. a gear; 19. a forward rotating screw; 20. reversing the screw; 21. a slide block; 22. a guide rod; 23. a push plate; 24. a spring; 25. a clamping plate; 26. a through hole; 27. and (5) rotating the rod.
Detailed Description
The technical solutions of the present embodiment will be clearly and completely described below with reference to the drawings in the present embodiment, and it is apparent that the described embodiments are only some embodiments of the present embodiment, not all embodiments.
Example 1
Referring to fig. 1-3, a grinding fixture for an engine cylinder cover of an unmanned aerial vehicle comprises a box body 1, wherein a first motor 2 is fixedly installed on the outer wall of the side face of the box body 1, a first transmission rod 6 is fixedly connected to an output shaft of the first motor 2, an adjusting mechanism is connected to the first transmission rod 6, a supporting table 15 is slidingly connected to the inner wall of the bottom of the box body 1, a second motor 3 is fixedly connected to the side face of the supporting table 15, a second transmission rod 8 is fixedly connected to the output shaft of the second motor 3, a clamping mechanism is connected to the second transmission rod 8, a cylinder 5 is fixedly installed on the top of the box body 1, a first guide plate 11 is connected to a piston of the cylinder 5, the first guide plate 11 is slidingly connected with the inner wall of the box body 1, a second guide plate 12 is slidingly connected to the inner wall of the box body 1, a lifting mechanism is connected to the first guide plate 11 and the second guide plate 12, and a rotating rod 27 is rotationally connected to the inner wall of the box body 1.
In this embodiment, adjustment mechanism includes first screw rod 7 and guide block 14, and first screw rod 7 fixed cover is established on first transfer line 6, and guide block 14 and first screw rod 7 threaded connection, and guide block 14 and brace table 15 fixed connection, and fixture includes corotation screw rod 19, reverse screw rod 20 and guide arm 22, and corotation screw rod 19 and reverse screw rod 20 are all fixed the cover and are established on second transfer line 8, and equal threaded connection has slider 21 on corotation screw rod 19 and the reverse screw rod 20, guide arm 22 and slider 21 fixed connection.
In this embodiment, the lifting mechanism includes a first rack 16, a second rack 17 and a gear 18, the first rack 16 is fixedly connected with the second guide plate 12, the second rack 17 is fixedly connected with the first guide plate 11, the gear 18 is engaged with and connected with the first rack 16 and the second rack 17, the gear 18 is sleeved on a rotating rod 27, a through hole 26 is formed in the supporting table 15, and the guide rod 22 is matched with the through hole 26.
In this embodiment, a push plate 23 is fixedly connected to the guide rod 22, a spring 24 is fixedly connected to the push plate 23, a clamping plate 25 is fixedly connected to the other end of the spring 24, and the clamping plate 25 and the push plate 23 are both slidably connected to the support table 15.
In this embodiment, a cutting knife 10 is fixedly installed on the bottom of the first guide plate 11, a third motor 4 is fixedly installed on the top of the second guide plate 12, a third transmission rod 9 is fixedly installed on the output shaft of the third motor 4, the third transmission rod 9 is rotationally connected with the second guide plate 12, and a polishing head 13 is fixedly connected to the third transmission rod 9.
The working principle, the during operation is put unmanned aerial vehicle engine cylinder cap on supporting bench 15 earlier, start the switch of second motor 3, second motor 3 drives second transfer line 8 and rotates, second transfer line 8 drives corotation screw 19 and reverse screw 20 and rotates, corotation screw 19 and reverse screw 20 drive corresponding slider 21 through the threaded connection with corresponding slider 21 and move, slider 21 drives guide arm 22 and moves, guide arm 22 drives push pedal 23 and moves, push pedal 23 drives spring 24 and splint 25 and moves, thereby make unmanned aerial vehicle engine cylinder cap put and obtain the centre gripping, when the conversion that needs to cut and polish, the switch of start cylinder 5, the piston of cylinder 5 drives first baffle 11 and moves, first baffle 11 drives cutting knife 10 and moves, simultaneously first baffle 11 drives second rack 17 and moves, second rack 17 drives gear 18 through the meshing connection with gear 18 and drives first rack 16 and move, first rack 16 drives second baffle 12 and moves, thereby make box 1 can polish and cut the conversion, first motor 2 drives first drive rod 6, first rack 6 drives first rack 7 and drives first rack 14 and moves through the screw 14, the screw 14 is connected with the screw 14 and is connected to the screw 14 and is processed the screw rod is moved, the guide block 14 is convenient for carrying out the conversion of cutting.
Example two
The second embodiment is different from the first embodiment in that a waste collection mechanism is provided inside the case 1, so that waste generated during grinding and cutting can be collected.
The foregoing is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art will be able to apply equally to the technical solution of the present utility model and the inventive concept thereof, within the scope of the present utility model.

Claims (7)

1. The utility model provides a grinding anchor clamps of unmanned aerial vehicle engine cylinder cap, includes box (1), a serial communication port, fixedly mounted has first motor (2) on the side outer wall of box (1), fixedly connected with first transfer line (6) on the output shaft of first motor (2), be connected with adjustment mechanism on first transfer line (6), sliding connection has brace table (15) on the bottom inner wall of box (1), fixedly connected with second motor (3) on the side of brace table (15), fixedly connected with second transfer line (8) on the output shaft of second motor (3), be connected with fixture on second transfer line (8), fixedly mounted has cylinder (5) on the top of box (1), be connected with first baffle (11) on the piston of cylinder (5), sliding connection has second baffle (12) on the inner wall of box (1), be connected with bull stick (27) on first baffle (11) and second elevating system (12).
2. The grinding fixture of the engine cylinder cover of the unmanned aerial vehicle according to claim 1, wherein the adjusting mechanism comprises a first screw rod (7) and a guide block (14), the first screw rod (7) is fixedly sleeved on the first transmission rod (6), the guide block (14) is in threaded connection with the first screw rod (7), and the guide block (14) is fixedly connected with the supporting table (15).
3. The grinding fixture for the engine cylinder cover of the unmanned aerial vehicle according to claim 1, wherein the clamping mechanism comprises a forward rotating screw rod (19), a reverse rotating screw rod (20) and a guide rod (22), the forward rotating screw rod (19) and the reverse rotating screw rod (20) are fixedly sleeved on the second transmission rod (8), sliding blocks (21) are connected to the forward rotating screw rod (19) and the reverse rotating screw rod (20) in a threaded mode, and the guide rod (22) is fixedly connected with the sliding blocks (21).
4. The grinding fixture of the engine cylinder cover of the unmanned aerial vehicle according to claim 1, wherein the lifting mechanism comprises a first rack (16), a second rack (17) and a gear (18), the first rack (16) is fixedly connected with the second guide plate (12), the second rack (17) is fixedly connected with the first guide plate (11), the gear (18) is in meshed connection with both the first rack (16) and the second rack (17), and the gear (18) is fixedly sleeved on the rotating rod (27).
5. A grinding jig for engine cylinder heads of unmanned aerial vehicle according to claim 3, wherein the support base (15) is provided with a through hole (26), and the guide rod (22) is matched with the through hole (26).
6. The grinding fixture for the engine cylinder cover of the unmanned aerial vehicle according to claim 5, wherein the guide rod (22) is fixedly connected with a push plate (23), the push plate (23) is fixedly connected with a spring (24), the other end of the spring (24) is fixedly connected with a clamping plate (25), and the clamping plate (25) and the push plate (23) are both in sliding connection with the supporting table (15).
7. The grinding fixture of the engine cylinder cover of the unmanned aerial vehicle according to claim 1, wherein a cutting knife (10) is fixedly installed on the bottom of the first guide plate (11), a third motor (4) is fixedly installed on the top of the second guide plate (12), a third transmission rod (9) is fixedly installed on an output shaft of the third motor (4), the third transmission rod (9) is rotationally connected with the second guide plate (12), and a grinding head (13) is fixedly connected on the third transmission rod (9).
CN202321587014.9U 2023-06-21 2023-06-21 Grinding fixture for engine cylinder cover of unmanned aerial vehicle Active CN220093844U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202321587014.9U CN220093844U (en) 2023-06-21 2023-06-21 Grinding fixture for engine cylinder cover of unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202321587014.9U CN220093844U (en) 2023-06-21 2023-06-21 Grinding fixture for engine cylinder cover of unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN220093844U true CN220093844U (en) 2023-11-28

Family

ID=88864631

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202321587014.9U Active CN220093844U (en) 2023-06-21 2023-06-21 Grinding fixture for engine cylinder cover of unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN220093844U (en)

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