CN219026009U

CN219026009U - Unmanned aerial vehicle screw perforating device

Info

Publication number: CN219026009U
Application number: CN202223524672.1U
Authority: CN
Inventors: 吴曼
Original assignee: Suqian Shuangying Intelligent Electronic Technology Co ltd
Current assignee: Suqian Shuangying Intelligent Electronic Technology Co ltd
Priority date: 2022-12-28
Filing date: 2022-12-28
Publication date: 2023-05-16
Anticipated expiration: 2032-12-28

Abstract

The utility model relates to the technical field of drilling, in particular to an unmanned aerial vehicle propeller punching device, which comprises an operation table and a propeller body, wherein a chute is formed in the upper surface of the operation table, a circular groove is formed in the upper surface of the operation table, a circular ring support member is fixedly arranged in the circular groove, the propeller body is placed on the circular ring support member, and a clamping structure is arranged on the operation table and comprises a clamping plate and a threaded rod. According to the unmanned aerial vehicle screw punching device, the two slide bars are driven to move close to each other or away from each other through rotation of the threaded rods, the two clamping plates are driven to move close to each other through the mutual close movement of the two slide bars, so that the gap between the two clamping plates is gradually reduced, the screw body can be fastened, and the punching operation can be directly performed at the moment.

Description

Unmanned aerial vehicle screw perforating device

Technical Field

The utility model relates to the technical field of drilling, in particular to a propeller punching device of an unmanned aerial vehicle.

Background

Drilling refers to the operation of drilling holes in solid materials with a drill bit. Drilling work in exploration work is taught herein, as well as auxiliary tools required for drilling and part of emergency measures.

Unmanned aerial vehicle screw is in the course of working, need use perforating device, and at present, unmanned aerial vehicle screw perforating device on the market is in the in-service use, and is comparatively troublesome to the fixed of screw, leads to punching comparatively inconvenient to the screw, and current unmanned aerial vehicle screw perforating device is inconvenient to collect the piece that the in-process produced that punches, still need the manual work to clear up, uses comparatively inconvenient, for this reason, we propose an unmanned aerial vehicle screw perforating device to solve above-mentioned problem.

Disclosure of Invention

In order to overcome the defects in the prior art, the utility model provides a unmanned aerial vehicle propeller punching device.

In order to solve the technical problems, the utility model provides the following technical scheme: the utility model provides an unmanned aerial vehicle screw perforating device, includes operation panel and screw body, the spout has been seted up to the upper surface of operation panel, the circular slot has been seted up to the upper surface of operation panel, circular slot internal fixation has ring support spare, the screw body is placed on ring support spare, be provided with the clamping structure on the operation panel, the clamping structure includes grip block and threaded rod, the quantity of grip block is two, two the grip block all sets up the top at the operation panel, the middle part of screw body is in between two grip blocks, two the equal fixed mounting of tip of grip block has the slide bar, two the slide bar all slides and sets up in the spout, the threaded rod rotates to install in the operation panel to the activity runs through the spout, the below of operation panel is provided with collection structure, collection structure includes box and collection box, be provided with dust catcher in the box slip setting in the box, four angles of operation panel bottom all fixed mounting have the supporting leg, tip fixed mounting have the hand wheel.

As a preferable technical scheme of the utility model, the bottom surface of the inner wall of the circular groove is provided with a leak hole communicated with the inner cavity of the box body, and both ends of the two clamping plates, which are opposite, are fixedly provided with limiting rods.

As a preferable technical scheme of the utility model, two sides of the upper end of the operating platform are fixedly provided with the baffle plates, and the two limit rods respectively penetrate through the two baffle plates.

As a preferable technical scheme of the utility model, the surfaces of the two sliding rods are provided with threaded holes, the threaded directions of the two threaded holes are opposite, and the threaded rods penetrate through the two threaded holes.

As a preferable technical scheme of the utility model, the box body is fixedly arranged at the bottom end of the operation table, the filter screen is embedded in the inner cavity of the collecting box, and the handle is fixedly arranged at the end part of the collecting box.

Compared with the prior art, the utility model has the following beneficial effects:

1. the rotation through the threaded rod can drive two slide bars and be close to each other or keep away from each other and remove, can mobilize two grip blocks and be close to each other and remove through two slide bars are close to each other for clearance between two grip blocks reduces gradually, thereby can fasten the screw body, can directly punch the operation this moment, and this unmanned aerial vehicle screw perforating device is fixed through fixing the screw body, conveniently punches the screw body.

2. Starting the dust catcher for the piece that produces the screw body in the process of punching falls into the circular slot, and in discharging to collecting the box from the leak, the piece that the user outwards removes the handle and collect in can collecting the box is taken out, need not the piece that manual clearance punching in-process produced, the operation is more convenient, the equal fixed mounting in both ends that deviate from mutually through two grip blocks has the gag lever post, two gag lever posts activity respectively run through the baffle, have played limiting displacement to the grip block removal in-process, make two grip blocks remove more stably, guaranteed this clamp structure's steady operation, improved this unmanned aerial vehicle screw perforating device's practicality.

Drawings

Fig. 1 is a schematic structural view of a propeller punching device of an unmanned aerial vehicle;

FIG. 2 is a schematic view of the structure of the ring support of the present utility model;

FIG. 3 is a schematic view of the structure of the case of the present utility model;

fig. 4 is an enlarged schematic view of the structure of fig. 1 a according to the present utility model.

Wherein: 1. an operation table; 11. a chute; 12. a circular groove; 13. a baffle; 14. support legs; 2. a propeller body; 3. a circular ring support; 4. a clamping plate; 41. a slide bar; 42. a limit rod; 5. a threaded rod; 51. a hand wheel; 6. a case; 61. a dust collector; 7. a collection box; 71. a filter screen; 72. a handle.

Detailed Description

In order that the manner in which the above recited features, objects and advantages of the present utility model are obtained will become readily apparent, a more particular description of the utility model will be rendered by reference to specific embodiments thereof which are illustrated in the appended drawings. Based on the examples in the embodiments, those skilled in the art can obtain other examples without making any inventive effort, which fall within the scope of the utility model. The experimental methods in the following examples are conventional methods unless otherwise specified, and materials, reagents, etc. used in the following examples are commercially available unless otherwise specified.

As shown in fig. 1, fig. 2, fig. 3 and fig. 4, an unmanned aerial vehicle screw punching device comprises an operation table 1 and a screw body 2, wherein a chute 11 is formed in the upper surface of the operation table 1, a circular groove 12 is formed in the upper surface of the operation table 1, a circular ring support 3 is fixedly installed in the circular groove 12, the screw body 2 is placed on the circular ring support 3, a clamping structure is arranged on the operation table 1, the clamping structure comprises two clamping plates 4 and threaded rods 5, the number of the clamping plates 4 is two, the two clamping plates 4 are all arranged above the operation table 1, the middle part of the screw body 2 is positioned between the two clamping plates 4, sliding rods 41 are fixedly installed at the end parts of the two clamping plates 4, the two sliding rods 41 are all arranged in the chute 11 in a sliding manner, the threaded rods 5 are rotatably installed in the operation table 1 and movably penetrate through the chute 11, a collecting structure is arranged below the operation table 1, the collecting structure comprises a box body 6 and a collecting box 7, a dust collector 61 is arranged in the box body 6, the collecting box 7 is arranged in the box body 6 in a sliding way, supporting legs 14 are fixedly arranged at four corners of the bottom end of an operation table 1, a hand wheel 51 is fixedly arranged at the end part of a threaded rod 5, a leak hole communicated with the inner cavity of the box body 6 is formed in the bottom surface of the inner wall of a circular groove 12, limiting rods 42 are fixedly arranged at the two opposite ends of two clamping plates 4, baffle plates 13 are fixedly arranged at the two opposite sides of the upper end of the operation table 1, the two limiting rods 42 respectively penetrate through the two baffle plates 13 in a movable way, a screw body 2 is placed on a circular ring supporting piece 3, then the hand wheel 51 is twisted to enable the threaded rod 5 to rotate, two sliding rods 41 are driven to move close to each other or move away from each other through the rotation of the threaded rod 5, the two clamping plates 4 are driven to move close to each other through the mutual approaching movement of the two sliding rods 41, make the clearance between two grip blocks 4 dwindle gradually to can fasten screw body 2, can directly punch the operation this moment, this unmanned aerial vehicle screw perforating device is fixed through being fixed to screw body 2, conveniently punch to screw body 2, in the process of punching to screw body 2, start dust catcher 61, make the piece that produces the in-process of punching to screw body 2 fall into circular slot 12, and discharge from the leak hole to collecting box 7 in, the piece that can collect box 7 in-process collection can be taken out to the outside removal handle 72 of user, need not the piece that manual cleaning produced in-process of punching, the operation is more convenient, both ends that deviate from through two grip blocks 4 are all fixed mounting gag lever post 42, two gag lever post 42 are movable respectively runs through baffle 13, play spacing effect to grip block 4 removal in-process, make two grip blocks 4 remove more stably, the steady operation of this clamp structure has been guaranteed, the practicality of this unmanned aerial vehicle screw perforating device has been improved, threaded hole has all been seted up on the surface of two screw holes, the screw thread direction is opposite, 5 the threaded rod is installed at the bottom of the fixed mounting of filter screen 7, the inner chamber 71 is collected to the box 7, the bottom of the fixed mounting of filter screen 7 has 72.

During the use, place the screw body 2 on ring support 3, twist the hand wheel 51 and make threaded rod 5 rotate afterwards, the rotation through threaded rod 5 can drive two slide bars 41 and be close to each other or keep away from each other and remove, can transfer two grip blocks 4 to be close to each other and remove through two slide bars 41 are close to each other, make the clearance between two grip blocks 4 dwindle gradually, thereby can fasten screw body 2, can directly punch the operation this moment, this unmanned aerial vehicle screw perforating device is fixed through to screw body 2, conveniently punch screw body 2, in punching the in-process to screw body 2, start dust catcher 61, make the piece that produces in the punching process to screw body 2 fall into circular slot 12, and discharge to collect in the box 7 from the leak source, the piece that can collect in the box 7 is taken out to the outside removal handle 72 of user, need not the piece that manual cleaning produced in the punching process, the operation is more convenient, the equal fixed mounting in both ends that deviate from mutually has gag lever 42 through two grip blocks 4, two gag lever post 42 are movable baffle 13 respectively, the effect has been played to two stable holding device in the punching operation, this unmanned aerial vehicle has guaranteed to have improved the practicality and have been moved the grip device, the stable holding structure has been guaranteed.

The embodiments of the present utility model have been described in detail with reference to the drawings, but the present utility model is not limited thereto, and various changes can be made within the knowledge of those skilled in the art without departing from the spirit of the present utility model.

Claims

1. The utility model provides an unmanned aerial vehicle screw perforating device, includes operation panel (1) and screw body (2), its characterized in that, spout (11) have been seted up to the upper surface of operation panel (1), circular slot (12) internal fixation has ring support (3), screw body (2) are placed on ring support (3), be provided with clamping structure on operation panel (1), clamping structure includes grip block (4) and threaded rod (5), the quantity of grip block (4) is two, two grip block (4) all set up in the top of operation panel (1), the middle part of screw body (2) is in between two grip block (4), two the tip of grip block (4) all fixed mounting has slide bar (41), two slide bar (41) all set up in spout (11), threaded rod (5) rotate and install in operation panel (1) to be provided with clamping structure on the box (6) under the movable box (6), collection box (6) are located in collection box (6), the collecting box (7) is arranged in the box body (6) in a sliding mode.

2. The unmanned aerial vehicle propeller punching device according to claim 1, wherein supporting legs (14) are fixedly arranged at four corners of the bottom end of the operating table (1), and a hand wheel (51) is fixedly arranged at the end part of the threaded rod (5).

3. The unmanned aerial vehicle propeller punching device according to claim 1, wherein the inner wall bottom surface of the circular groove (12) is provided with a leak hole communicated with the inner cavity of the box body (6), and two ends of the two clamping plates (4) which are away from each other are fixedly provided with limiting rods (42).

4. A propeller punching device for an unmanned aerial vehicle according to claim 3, wherein two sides of the upper end of the operating table (1) are fixedly provided with baffle plates (13), and two limit rods (42) respectively penetrate through the two baffle plates (13) in an active manner.

5. An unmanned aerial vehicle propeller punching device according to claim 1, wherein the surfaces of the two slide bars (41) are provided with threaded holes, the threaded directions of the two threaded holes are opposite, and the threaded rod (5) penetrates through the two threaded holes.

6. The unmanned aerial vehicle propeller punching device according to claim 1, wherein the box body (6) is fixedly arranged at the bottom end of the operating platform (1), the filter screen (71) is embedded in the inner cavity of the collecting box (7), and the handle (72) is fixedly arranged at the end part of the collecting box (7).