Adjustable unmanned aerial vehicle fuselage positioning tool

Abstract

The utility model discloses an adjustable unmanned aerial vehicle body positioning tool which comprises a mounting frame, a mounting plate is fixedly mounted at the upper end of the mounting frame, a first mounting table is fixedly mounted on the left side of the upper end of the mounting plate, a vertical frame is fixedly mounted on the right side of the upper end of the first mounting table, and a first positioning mechanism is arranged on the right side of the vertical frame. A brake mechanism is arranged on the left side of the vertical frame, and a slider is slidably mounted on the right side of the upper end of the mounting frame. The first motor drives the lead screw to rotate, so that the sliding block drives the second positioning mechanism to move left and right, the positioning tool can be adjusted and is suitable for unmanned aerial vehicle bodies with different lengths, and then the unmanned aerial vehicle bodies are fixedly installed between the first positioning disc and the second positioning disc; the unmanned aerial vehicle body is driven by the second motor to rotate by a specific angle for machining, the brake mechanism arranged at the leftmost end can rapidly complete braking, the unmanned aerial vehicle body can rotate to the specific angle, and machining of the unmanned aerial vehicle body is achieved.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle processing, in particular to an adjustable unmanned aerial vehicle fuselage positioning tool. Background Art

[0002] Unmanned aerial vehicle, also known as UAV, is an unmanned aerial vehicle controlled by radio remote control equipment and its own program control device. It has the advantages of easy positioning and excellent performance. It is widely used in aerial photography, agriculture, plant protection, micro selfie, express delivery and disaster relief.

[0003] The existing UAV fuselage needs to be punched during processing, and the punching positions are located at various angles of the fuselage. Utility Model Content

[0004] In order to overcome the above-mentioned defects existing in the prior art, the utility model provides an adjustable UAV fuselage positioning tool.

[0005] The technical solution adopted by the utility model to solve its technical problems is: an adjustable UAV fuselage positioning tooling, including a mounting frame, a mounting plate is fixedly installed on the upper end of the mounting frame, a first mounting platform is fixedly installed on the left side of the upper end of the mounting plate, a vertical frame is fixedly installed on the right side of the upper end of the first mounting platform, a first positioning mechanism is arranged on the right side of the vertical frame, a brake mechanism is arranged on the left side of the vertical frame, a slider is slidably installed on the right side of the upper end of the mounting frame, and a second positioning mechanism is arranged on the upper end of the slider.

[0006] Furthermore, the first positioning mechanism includes a first bearing seat, the first bearing seat is fixedly installed on the right side of the stand, a first transmission shaft is movably installed inside the first bearing seat, and a first positioning plate is fixedly installed on the right side of the first transmission shaft.

[0007] Furthermore, the brake mechanism includes a brake disc, which is fixedly mounted on the left end of the first transmission shaft. A brake pad is mounted on the outer side of the brake disc. The brake pad is fixedly mounted on a fixing frame, and the fixing frame is fixedly mounted on the upper end of the first mounting platform.

[0008] Furthermore, a first motor is fixedly installed on the right side of the upper end of the mounting plate, a lead screw is fixedly connected to the power output shaft of the first motor, the end of the lead screw is movably installed on a fixed block, the fixed block is fixedly installed on the upper end of the mounting plate, and a slider is movably installed on the lead screw.

[0009] Further, the second positioning mechanism includes a second mounting platform, the second mounting platform is fixedly mounted on the upper end of the slider, a motor mounting frame is fixedly mounted on the right side of the second mounting platform, a second motor is fixedly mounted on the motor mounting frame, a second motor is fixedly mounted on the power output shaft of the second motor, the second transmission shaft is fixedly connected to the second bearing seat, the second bearing seat is fixedly mounted on the left side of the second mounting platform, and a second positioning plate is fixedly mounted on the left side of the second transmission shaft.

[0010] The beneficial effect of the utility model is as follows: the first motor drives the lead screw to rotate, so that the slider drives the second positioning mechanism to move left and right, so that the positioning tooling can be adjusted and suitable for UAV fuselages of different lengths, and then the UAV fuselage is fixedly installed between the first positioning plate and the second positioning plate, and the second motor drives the UAV fuselage to rotate a specific angle for processing, and the brake mechanism set at the leftmost end can quickly complete the braking, so that the UAV fuselage can be rotated to a specific angle, thereby realizing the processing of the UAV fuselage. BRIEF DESCRIPTION OF THE DRAWINGS

[0011] The utility model is further described below in conjunction with the accompanying drawings and embodiments.

[0012] Figure 1 It is the front view of the utility model;

[0013] Figure 2 It is an enlarged view of point A of the utility model;

[0014] Figure 3 It is an enlarged view of point B of the utility model;

[0015] Figure 4 It is a side view of the first mounting platform of the utility model;

[0016] Figure 5 It is a top view of the utility model;

[0017] Figure 6 It is an enlarged view of point C of the utility model;

[0018] Figure 7 It is an enlarged view of point D of the present utility model.

[0019] In the figure: 1. mounting frame, 2. mounting plate, 3. first mounting platform, 4. stand, 5. first bearing seat, 6. first transmission shaft, 7. first positioning plate, 8. brake disc, 9. brake pad, 10. fixing frame, 11. first motor, 12. fixing block, 13. lead screw, 14. slider, 15. second mounting platform, 16. motor fixing frame, 17. second motor, 18. second bearing seat, 19. second transmission shaft, 20. second positioning plate. DETAILED DESCRIPTION

[0020] In order to more clearly illustrate the technical solution of the utility model, the utility model is further described below in conjunction with the accompanying drawings. Obviously, the accompanying drawings described below are only one embodiment of the utility model. For ordinary technicians in this field, without paying any creative work, other embodiments can be obtained based on this drawing and embodiment, which all belong to the protection scope of the utility model.

[0021] like Figure 1 , Figure 2 , Figure 5 and Figure 6 As shown, the utility model includes a mounting frame 1, the upper end of the mounting frame 1 is fixedly installed with a mounting plate 2 by bolts, the upper left end of the mounting plate 2 is fixedly installed with a first mounting platform 3 by bolts, the upper right end of the first mounting platform 3 is fixedly installed with a vertical frame 4 by bolts, and the vertical frame 4 is provided with a first positioning mechanism on the right side, the first positioning mechanism includes a first bearing seat 5, the first bearing seat 5 is fixedly installed on the right side of the vertical frame 4 by bolts, a first transmission shaft 6 is movably installed inside the first bearing seat 5, and a first positioning plate 7 is fixedly installed on the right side of the first transmission shaft 6.

[0022] like Figures 1 to 6 As shown, a brake mechanism is arranged on the left side of the stand 4, and the brake mechanism includes a brake disc 8, and the brake disc 8 is fixedly mounted on the left end of the first transmission shaft 6, and a brake pad 9 is installed on the outer side of the brake disc 8, and the brake pad 9 is fixedly mounted on a fixing frame 10, and the fixing frame 10 is fixedly mounted on the upper end of the first mounting platform 3.

[0023] like Figure 3 and Figure 7 As shown, the first motor 11 is fixedly installed on the right side of the upper end of the mounting plate 2 by bolts, and a lead screw 13 is fixedly connected to the power output shaft of the first motor 11. The end of the lead screw 13 is movably installed on a fixed block 12, and the fixed block 12 is welded and installed on the upper end of the mounting plate 2. A slider 14 is movably installed on the lead screw 13, and the slider 14 is slidably installed on the upper end of the mounting frame 1, and a second positioning mechanism is provided on the upper end of the slider 14.

[0024] like Figure 3 and Figure 7 As shown, the second positioning mechanism includes a second mounting platform 15, the second mounting platform 15 is fixedly mounted on the upper end of the slider 14, a motor mounting bracket 16 is fixedly mounted on the right side of the second mounting platform 15, a second motor 17 is fixedly mounted on the motor mounting bracket 16, the second motor 17 is fixedly connected to a second transmission shaft 19 at the power output shaft, the second transmission shaft 19 is movably mounted on a second bearing seat 18, the second bearing seat 18 is fixedly mounted on the left side of the second mounting platform 15, and a second positioning plate 20 is fixedly mounted on the left side of the second transmission shaft 19.

[0025] When the utility model is in use, the first motor 11 drives the lead screw 13 to rotate, so that the slider 14 drives the second positioning mechanism to move left and right, so that the positioning tooling can be adjusted and suitable for UAV fuselages of different lengths, and then the UAV fuselage is fixedly installed between the first positioning plate 7 and the second positioning plate 20, and the second motor 17 is used to drive the UAV fuselage to rotate a specific angle for processing. The brake mechanism set at the leftmost end can quickly complete the braking, so that the UAV fuselage can be rotated to a specific angle, thereby realizing the processing of the UAV fuselage.

[0026] The above embodiments are only exemplary embodiments of the present invention and are not intended to limit the present invention. The protection scope of the present invention is defined by the claims. Those skilled in the art may make various modifications or equivalent substitutions to the present invention within the essence and protection scope of the present invention, and such modifications or equivalent substitutions shall also be deemed to fall within the protection scope of the present invention.

Claims

1. An adjustable UAV fuselage positioning tool, comprising a mounting frame (1), characterized in that: The upper end of the mounting frame (1) is fixedly mounted with a mounting plate (2), the upper left end of the mounting plate (2) is fixedly mounted with a first mounting platform (3), the upper right end of the first mounting platform (3) is fixedly mounted with a vertical frame (4), the upper right end of the vertical frame (4) is provided with a first positioning mechanism, the left end of the vertical frame (4) is provided with a brake mechanism, the upper right end of the mounting frame (1) is slidably mounted with a slider (14), and the upper end of the slider (14) is provided with a second positioning mechanism.

2. The adjustable UAV fuselage positioning tool according to claim 1, characterized in that: The first positioning mechanism comprises a first bearing seat (5), the first bearing seat (5) is fixedly mounted on the right side of the stand (4), a first transmission shaft (6) is movably mounted inside the first bearing seat (5), and a first positioning plate (7) is fixedly mounted on the right side of the first transmission shaft (6).

3. The adjustable UAV fuselage positioning tool according to claim 2, characterized in that: The brake mechanism comprises a brake disc (8), the brake disc (8) is fixedly mounted on the left end of the first transmission shaft (6), a brake pad (9) is mounted on the outer side of the brake disc (8), the brake pad (9) is fixedly mounted on a fixing frame (10), and the fixing frame (10) is fixedly mounted on the upper end of the first mounting platform (3).

4. The adjustable UAV fuselage positioning tool according to claim 1, characterized in that: A first motor (11) is fixedly mounted on the right side of the upper end of the mounting plate (2); a lead screw (13) is fixedly connected to the power output shaft of the first motor (11); the end of the lead screw (13) is movably mounted on a fixed block (12); the fixed block (12) is fixedly mounted on the upper end of the mounting plate (2); and a sliding block (14) is movably mounted on the lead screw (13).

5. The adjustable UAV fuselage positioning tool according to claim 4, characterized in that: The second positioning mechanism comprises a second mounting platform (15), the second mounting platform (15) is fixedly mounted on the upper end of the slider (14), a motor mounting bracket (16) is fixedly mounted on the right side of the second mounting platform (15), a second motor (17) is fixedly mounted on the motor mounting bracket (16), a power output shaft of the second motor (17) is fixedly connected to a second transmission shaft (19), the second transmission shaft (19) is movably mounted on a second bearing seat (18), the second bearing seat (18) is fixedly mounted on the left side of the second mounting platform (15), and a second positioning plate (20) is fixedly mounted on the left side of the second transmission shaft (19).

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