Wing assembly equipment for folding wing unmanned aerial vehicle

Abstract

The utility model discloses wing assembly equipment for a folding wing unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicle assembly. The folding wing unmanned aerial vehicle wing assembling equipment comprises an operation table, a direction adjusting mechanism and a positioning mechanism, the direction adjusting mechanism is arranged at the top of the operation table and comprises a rotating rod and a bearing block, the top of the operation table is rotationally connected with one end of the rotating rod, and the other end of the rotating rod is fixedly connected with the bottom of the bearing block; the positioning mechanism is arranged above the operation table, the positioning mechanism comprises a cavity, a bidirectional threaded rod, an auxiliary knob and an internal threaded block, the cavity is formed in the bearing block, the inner wall of one side of the cavity is rotationally connected with one end of the bidirectional threaded rod, and the other end of the bidirectional threaded rod extends out of the cavity and is fixedly connected with one side of the auxiliary knob. The unmanned aerial vehicle body is prevented from deviating and shaking during wing assembling, the operation difficulty of workers is lowered, the assembling efficiency of the unmanned aerial vehicle is improved, and the unmanned aerial vehicle assembling device can be suitable for assembling unmanned aerial vehicles of various sizes.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle assembly, in particular to a folding-wing unmanned aerial vehicle wing assembly device. Background Art

[0002] Chinese patent document CN218837680U discloses an unmanned aerial vehicle assembly platform, comprising: a workbench, a support plate is fixedly installed on the bottom surface of the workbench, an installation box is fixedly installed on the bottom surface of the workbench, a fixing frame is fixedly installed on the top surface of the workbench, and a mounting block is arranged below the fixing frame; a fill light component, the fill light component is arranged on the top surface of the workbench, and is used to increase the brightness of the surrounding environment when assembling the unmanned aerial vehicle, by arranging a positioning rod, the positioning rod can move laterally inside the accommodating groove, so that the movable block can be driven to move synchronously inside the accommodating groove, by arranging the movable block, the movable block can utilize the fixed installation with the mounting block to drive the mounting block to move synchronously when the movable block moves, and by arranging the mounting block, the mounting block can drive the fluorescent tube to move above the workbench when it moves, so that the lighting range of the fluorescent tube can be changed, so that the lighting range of the fluorescent tube can be adjusted according to the staff's own habits.

[0003] The above-mentioned UAV assembly platform is not convenient for fixing the UAV body when assembling the wings. The UAV body is prone to shifting and shaking during the assembly process, which increases the assembly difficulty for the staff and reduces the assembly efficiency of the UAV. Utility Model Content

[0004] The purpose of the utility model is to provide a folding-wing UAV wing assembly device, which can solve the problem that the above-mentioned UAV assembly platform is not convenient for fixing the UAV body when assembling the wing, and the UAV body is prone to deviation and shaking during the assembly process, which increases the assembly difficulty for the staff and reduces the assembly efficiency of the UAV.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a folding-wing UAV wing assembly device, including an operating table, an adjustment mechanism and a positioning mechanism, the adjustment mechanism is arranged on the top of the operating table, the adjustment mechanism includes a rotating rod and a supporting block, the top of the operating table is rotatably connected to one end of the rotating rod, and the other end of the rotating rod is fixedly connected to the bottom of the supporting block; the positioning mechanism is arranged above the operating table, the positioning mechanism includes a cavity, a bidirectional threaded rod, an auxiliary knob and an internal threaded block, a cavity is opened inside the supporting block, an inner wall of one side of the cavity is rotatably connected to one end of the bidirectional threaded rod, the other end of the bidirectional threaded rod extends to the outside of the cavity and is fixedly connected to one side of the auxiliary knob, and the outer wall of the bidirectional threaded rod is connected to the internal threads of two groups of internal threaded blocks.

[0006] Preferably, the direction adjusting mechanism further includes a brake motor. The brake motor is fixedly installed at the bottom of the operating table. The output shaft of the brake motor is fixedly connected to one end of the rotating rod. Without removing the UAV body, the direction of the UAV body can be directly adjusted, which is convenient for installing the wings at different positions of the UAV body, improving the flexibility and practicability of the device.

[0007] Preferably, the positioning mechanism further includes a sliding groove, a movable block and a positioning rod. A strip-shaped opening is obliquely arranged at the top of the supporting block. The inner wall of the cavity is slidably connected to the outer wall of the internally threaded block. Two groups of sliding grooves are respectively arranged at the top of the internally threaded block. The movable block is slidably installed on the inner wall of the sliding groove. The positioning rod is fixedly installed at the top of the movable block. The positioning rod passes through the strip-shaped opening and extends to the outside of the cavity to clamp the UAV body, avoiding the deviation and shaking of the UAV body during the assembly of the wings, ensuring the stability of the UAV body, reducing the operation difficulty of the staff, improving the assembly efficiency of the UAV, and being applicable to the assembly of UAVs of various sizes.

[0008] Preferably, an anti-slip rubber sleeve is arranged on the outer wall of the positioning rod.

[0009] Preferably, a mounting bracket is fixedly installed at the top of the operating table, and a supplementary light is fixedly installed at the inner top of the mounting bracket.

[0010] Preferably, a group of placement boxes are respectively fixedly installed on both sides of the operating table.

[0011] Preferably, a plurality of support legs distributed in a rectangular shape are fixedly installed at the bottom of the operating table.

[0012] Compared with the prior art, the beneficial effects of the present utility model are as follows:

[0013] (1) For the wing assembly device of the folding-wing UAV, through the combined use of the brake motor, the rotating rod and the supporting block, without removing the UAV body, the direction of the UAV body can be directly adjusted, which is convenient for installing the wings at different positions of the UAV body, improving the flexibility and practicability of the device.

[0014] (2) For the wing assembly device of the folding-wing UAV, through the combined use of the cavity, the bidirectional threaded rod, the auxiliary knob, the internally threaded block, the sliding groove, the movable block and the positioning rod, the UAV body is clamped, avoiding the deviation and shaking of the UAV body during the assembly of the wings, ensuring the stability of the UAV body, reducing the operation difficulty of the staff, improving the assembly efficiency of the UAV, and being applicable to the assembly of UAVs of various sizes. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] The following further describes the present utility model in conjunction with the drawings and embodiments:

[0016] Figure 1 Schematic three - dimensional structure diagram of the present utility model;

[0017] Figure 2 Schematic bottom three - dimensional structure diagram of the present utility model;

[0018] Figure 3 Bottom three - dimensional view of the supporting block of the present utility model;

[0019] Figure 4 Schematic three - dimensional structure diagram of the supporting block of the present utility model.

[0020] Reference numerals: 1, operating table; 2, orientation adjusting mechanism; 201, brake motor; 202, rotating rod; 203, supporting block; 3, positioning mechanism; 301, cavity; 302, bidirectional threaded rod; 303, auxiliary knob; 304, internally threaded block; 305, sliding groove; 306, movable block; 307, positioning rod; 4, mounting bracket; 5, fill light; 6, placement box; 7, support leg. Specific embodiments

[0021] This part will describe in detail the specific embodiments of the present utility model. The preferred embodiments of the present utility model are shown in the drawings. The function of the drawings is to supplement the description in the text part of the specification, enabling people to intuitively and vividly understand each technical feature and the overall technical solution of the present utility model, but it cannot be construed as a limitation on the protection scope of the present utility model.

[0022] Please refer to Figures 1-4 , the present utility model provides a technical solution: a folding - wing UAV wing assembly device, including an operating table 1, an orientation adjusting mechanism 2 and a positioning mechanism 3. The orientation adjusting mechanism 2 is arranged on the top of the operating table 1. The orientation adjusting mechanism 2 includes a rotating rod 202 and a supporting block 203. One end of the rotating rod 202 is rotatably connected to the top of the operating table 1, and the other end of the rotating rod 202 is fixedly connected to the bottom of the supporting block 203. The positioning mechanism 3 is arranged above the operating table 1. The positioning mechanism 3 includes a cavity 301, a bidirectional threaded rod 302, an auxiliary knob 303 and an internally threaded block 304. A cavity 301 is opened inside the supporting block 203. One inner wall of the cavity 301 is rotatably connected to one end of the bidirectional threaded rod 302. The other end of the bidirectional threaded rod 302 extends outside the cavity 301 and is fixedly connected to one side of the auxiliary knob 303. The outer wall of the bidirectional threaded rod 302 is threadedly connected to the inside of two groups of internally threaded blocks 304. A mounting bracket 4 is fixedly installed on the top of the operating table 1, and a fill light 5 is fixedly installed on the inner top of the mounting bracket 4. A group of placement boxes 6 are respectively fixedly installed on both sides of the operating table 1. A plurality of support legs 7 distributed in a rectangular shape are fixedly installed at the bottom of the operating table 1.

[0023] Secondly, the steering mechanism 2 further includes a brake motor 201. The brake motor 201 is fixedly installed at the bottom of the operating table 1. The output shaft of the brake motor 201 is fixedly connected to one end of the rotating rod 202. Without removing the UAV body, the direction of the UAV body can be directly adjusted, which is convenient for installing the wings on different positions of the UAV body, improving the flexibility and practicability of the device.

[0024] Furthermore, the positioning mechanism 3 further includes a sliding groove 305, a movable block 306 and a positioning rod 307. An inclined strip-shaped opening is formed at the top of the supporting block 203. The inner wall of the cavity 301 is slidably connected to the outer wall of the internally threaded block 304. Two groups of sliding grooves 305 are respectively formed at the top of the internally threaded block 304. The movable block 306 is slidably installed on the inner wall of the sliding groove 305. The positioning rod 307 is fixedly installed at the top of the movable block 306. The positioning rod 307 passes through the strip-shaped opening and extends to the outside of the cavity 301. The outer wall of the positioning rod 307 is provided with an anti-slip rubber sleeve, which clamps the UAV body, avoids the UAV body from shifting and shaking during the wing assembly, ensures the stability of the UAV body, reduces the operation difficulty of the staff, improves the assembly efficiency of the UAV, and can be applied to the assembly of UAVs of various sizes.

[0025] Working principle: When in use, place the UAV body to be installed with wings on the supporting block 203, put the parts needed in the installation process in the placement box 6, rotate the bidirectional threaded rod 302 by the auxiliary knob 303. Under the limitation of the cavity 301, drive the two internally threaded blocks 304 to slide in the cavity 301 in opposite directions. During the sliding of the cavity 301, drive the movable block 306 to slide in the sliding groove 305 through the guidance of the inclined strip-shaped opening, and then drive the multi-group positioning rods 307 to move towards the center of the supporting block 203 to clamp the UAV body. Turn on the fill light 5 for filling light, and install the wings on the UAV body. After installing a set of wings, turn on the brake motor 201 to drive the rotating rod 202 to rotate, drive the supporting block 203 to rotate, and then the orientation of the UAV can be adjusted and the installation can continue.

[0026] The above has described the embodiments of the present invention in detail with reference to the drawings. However, the present invention is not limited to the above embodiments. Within the scope of knowledge possessed by those of ordinary skill in the art in the technical field, various changes can be made without departing from the purpose of the present invention.

Claims

1. A folding wing UAV wing assembly device, characterized in that: include: Operating table (1); The direction adjustment mechanism (2) is arranged on the top of the operating platform (1), and comprises a rotating rod (202) and a supporting block (203). The top of the operating platform (1) is rotatably connected to one end of the rotating rod (202), and the other end of the rotating rod (202) is fixedly connected to the bottom of the supporting block (203); The positioning mechanism (3) is arranged above the operating table (1), and comprises a cavity (301), a bidirectional threaded rod (302), an auxiliary knob (303) and an internal thread block (304). The cavity (301) is provided inside the supporting block (203), an inner wall of one side of the cavity (301) is rotatably connected to one end of the bidirectional threaded rod (302), the other end of the bidirectional threaded rod (302) extends to the outside of the cavity (301) and is fixedly connected to one side of the auxiliary knob (303), and the outer wall of the bidirectional threaded rod (302) is connected to the internal threads of the two sets of internal thread blocks (304).

2. The folding-wing UAV wing assembly equipment according to claim 1, characterized in that: The direction adjustment mechanism (2) also includes a brake motor (201), the brake motor (201) is fixedly mounted on the bottom of the operating platform (1), and the output shaft of the brake motor (201) is fixedly connected to one end of the rotating rod (202).

3. The folding-wing UAV wing assembly equipment according to claim 2, characterized in that: The positioning mechanism (3) further comprises a sliding groove (305), a movable block (306) and a positioning rod (307); the top of the supporting block (203) is provided with an inclined strip opening; the inner wall of the cavity (301) is slidably connected to the outer wall of the internal thread block (304); the top of the internal thread block (304) is provided with two groups of sliding grooves (305); the inner wall of the sliding groove (305) is slidably mounted with a movable block (306); the top of the movable block (306) is fixedly mounted with a positioning rod (307); the positioning rod (307) passes through the strip opening and extends to the outside of the cavity (301).

4. The folding-wing UAV wing assembly equipment according to claim 3, characterized in that: The outer wall of the positioning rod (307) is provided with an anti-slip rubber sleeve.

5. The folding-wing UAV wing assembly equipment according to claim 4, characterized in that: A mounting frame (4) is fixedly mounted on the top of the operating table (1), and a fill light (5) is fixedly mounted on the inner top of the mounting frame (4).

6. The folding-wing UAV wing assembly equipment according to claim 5, characterized in that: A group of placement boxes (6) are respectively fixedly mounted on both sides of the operating table (1).

7. The folding-wing UAV wing assembly equipment according to claim 6, characterized in that: A plurality of groups of rectangularly distributed support legs (7) are fixedly mounted on the bottom of the operating table (1).

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