Unmanned aerial vehicle part multi-angle clamping and docking simulation device

Abstract

The utility model relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle part multi-angle clamping and butting simulation device. According to the multi-angle clamping and butt-joint simulation device for the unmanned aerial vehicle parts, different unmanned aerial vehicle parts can be clamped and fixed, the clamped unmanned aerial vehicle parts can be rotated, the states of the parts at different installation angles can be simulated conveniently, and the flexibility of using the device is improved. An unmanned aerial vehicle part multi-angle clamping and docking simulation device comprises a base, sliding seats and the like, and the left and right parts of the base are slidably connected with the sliding seats. According to the unmanned aerial vehicle part clamping device, different unmanned aerial vehicle parts are clamped through the fixing piece, then the supporting base is rotated, the sliding piece is driven to rotate, the unmanned aerial vehicle parts are made to rotate, the different unmanned aerial vehicle parts can be clamped and fixed, and the clamped unmanned aerial vehicle parts can be rotated; the simulation of the states of the part at different installation angles is facilitated, and the flexibility of using the device is improved.

Description

Technical Field

[0001] The utility model relates to the field of unmanned aerial vehicles, in particular to a multi-angle clamping and docking simulation device for unmanned aerial vehicle parts. Background Art

[0002] With the rapid development of UAV technology, the manufacturing, assembly and maintenance of UAV parts have become increasingly important. Multi-angle clamping and docking simulation of UAV parts refers to the use of a combination of computer simulation and physical experiments to pre-evaluate and optimize the clamping and docking behaviors of various UAV components at different angles and postures during the design and verification of UAV component assembly.

[0003] The existing multi-angle clamping and docking of UAV parts usually involves clamping the UAV parts with special fixtures and then docking the UAV parts with mobile fixtures. However, the current device can only clamp different UAV parts with special fixtures, and different fixtures are needed to clamp the UAV parts. It has a single function, low flexibility of use, and is relatively inconvenient.

[0004] Therefore, it is necessary to design a drone parts multi-angle clamping and docking simulation device that can clamp and fix different drone parts and rotate the clamped drone parts, so as to simulate the states of the parts at different installation angles and improve the flexibility of using the device. Utility Model Content

[0005] In order to overcome the shortcomings of the existing multi-angle clamping and docking of drone parts, which can only be clamped by special clamps, and different drone parts need to be clamped by different clamps, with single function and low flexibility of use, the utility model provides a drone parts multi-angle clamping and docking simulation device that can clamp and fix different drone parts and can rotate the clamped drone parts, thereby simulating the states of parts at different installation angles and improving the flexibility of using the device.

[0006] The technical solution of the utility model is: a multi-angle clamping and docking simulation device for unmanned aerial vehicle parts, including a base, a sliding seat, a first screw rod, a support frame, a support seat, a sliding part, a second screw rod, a fixing part and a spring, the left and right parts of the base are slidably connected with the sliding seat, the middle and upper part of the base is rotatably connected with the first screw rod, the sliding seats are threadedly connected with the first screw rod, the upper side of the sliding seat is connected with the support frame, the upper part of the support frame is rotatably connected with the support seat, the front and rear parts of the support seat are slidably connected with the sliding part, the middle part of the support seat is rotatably connected with the second screw rod, the sliding parts are threadedly connected with a plurality of fixing parts, and springs are connected between the fixing parts and adjacent sliding parts.

[0007] In one embodiment, a first knob is further included, and the first knob is connected to both the left and right sides of the first screw rod.

[0008] In one of the embodiments, screws are further included. The front upper part of the support frame is threadedly connected with the screws, and the screws are in contact with the adjacent support seats.

[0009] In one embodiment, a second knob is further included, and the front side of the second screw rod is connected to the second knob.

[0010] In one embodiment, the interior of the fixing member is arc-shaped.

[0011] In one embodiment, it also includes a telescopic rod and a laser scanner. The upper rear side of the base is connected to the telescopic rod, and the telescopic end of the telescopic rod is connected to the laser scanner.

[0012] The beneficial effect is: the utility model clamps different drone parts through the fixing parts, and then rotates the support seat to drive the sliding parts to rotate, so that the drone parts rotate, thereby achieving the effect of being able to clamp and fix different drone parts, and being able to rotate the clamped drone parts, thereby simulating the states of the parts at different installation angles and improving the flexibility of using the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a three-dimensional structural schematic diagram of the utility model.

[0014] Figure 2 It is a partial three-dimensional structural schematic diagram of the utility model.

[0015] Figure 3 It is a partial three-dimensional structural sectional view of the utility model.

[0016] Markings in the figure are: 1-base, 2-sliding seat, 3-first screw rod, 4-first knob, 5-support frame, 6-screw, 7-support seat, 8-sliding member, 9-second screw rod, 10-second knob, 11-fixing member, 12-spring, 13-telescopic rod, 14-laser scanner. DETAILED DESCRIPTION

[0017] The utility model is further described below in conjunction with the embodiments shown in the accompanying drawings.

[0018] A multi-angle clamping and docking simulation device for UAV parts, such as Figure 1-Figure 3As shown, it includes a base 1, a sliding seat 2, a first screw rod 3, a first knob 4, a support frame 5, a screw 6, a support seat 7, a sliding member 8, a second screw rod 9, a second knob 10, a fixing member 11, a spring 12, a telescopic rod 13 and a laser scanner 14. The left and right parts of the base 1 are both slidably connected to the sliding seat 2, the upper middle part of the base 1 is rotatably connected to the first screw rod 3, the left and right sides of the first screw rod 3 are connected to the first knob 4, the sliding seat 2 is threadedly connected to the first screw rod 3, the upper side of the sliding seat 2 is connected to the support frame 5, the upper part of the support frame 5 is rotatably connected to the support seat 7, and the front upper part of the support frame 5 The parts are all threadedly connected with screws 6, and the screws 6 are in contact with adjacent support seats 7. The front and rear parts of the support seats 7 are slidably connected with sliding members 8. The middle part of the support seat 7 is rotatably connected with a second screw rod 9, and the sliding members 8 are all threadedly connected to the second screw rod 9. The front side of the second screw rod 9 is connected to a second knob 10. Twenty-four fixing members 11 are slidably connected to the sliding members 8. The inside of the fixing members 11 is arc-shaped. Springs 12 are connected between the fixing members 11 and the adjacent sliding members 8. A telescopic rod 13 is connected to the upper side of the rear part of the base 1, and a laser scanner 14 is connected to the telescopic end of the telescopic rod 13.

[0019] When using the device, first place the base 1 in the multi-angle clamping and docking simulation area of ​​the drone parts, then turn the second knob 10 as needed to drive the second screw rod 9 to rotate, so that the sliding member 8 moves under the action of the thread, so that the sliding members 8 are close to or away from each other, and then place the drone parts between the fixing members 11 respectively, so that the fixing member 11 moves outward on the sliding member 8, and the spring 12 rebounds after being squeezed and contracted, and different drone parts are clamped by the fixing member 11, and then the support seat 7 is rotated as needed to drive the sliding member 8 to rotate, so that the drone parts rotate, and then the screw is The screw 6 is docked with the support frame 5, and then the screw 6 is turned and tightened to fix the support seat 7, so that different drone parts can be clamped and fixed, and the clamped drone parts can be rotated, which is convenient for simulating the state of the parts at different installation angles and improving the flexibility of using the device. After the fixation is completed, the first knob 4 is turned to drive the sliding seat 2 to move under the action of the thread, so that the support frame 5 moves, so that the drone parts are close to each other for docking. After the docking is completed, the drone parts are detected by the laser scanner 14 on the telescopic rod 13 to monitor the docking position of the drone parts in real time.

[0020] It should be understood that this embodiment is only used to illustrate the present invention and is not used to limit the scope of the present invention. In addition, it should be understood that after reading the content taught by the present invention, those skilled in the art can make various changes or modifications to the present invention, and these equivalent forms also fall within the scope defined by the claims attached to this application.

Claims

1. A multi-angle clamping and docking simulation device for drone parts, characterized in that: The invention comprises a base (1), a sliding seat (2), a first screw rod (3), a support frame (5), a support seat (7), a sliding member (8), a second screw rod (9), a fixing member (11) and a spring (12); the left and right parts of the base (1) are both slidably connected to the sliding seat (2); the middle and upper part of the base (1) is rotatably connected to the first screw rod (3); the sliding seats (2) are both threadedly connected to the first screw rod (3); the upper side of the sliding seat (2) is connected to the support frame (5); the upper part of the support frame (5) is rotatably connected to the support seat (7); the front and rear parts of the support seat (7) are both slidably connected to the sliding member (8); the middle part of the support seat (7) is rotatably connected to the second screw rod (9); the sliding members (8) are all threadedly connected to the second screw rod (9); a plurality of fixing members (11) are slidably connected to the sliding members (8); and springs (12) are connected between the fixing members (11) and adjacent sliding members (8).

2. A multi-angle clamping and docking simulation device for drone parts as claimed in claim 1, characterized in that: It also includes a first knob (4), and the left and right sides of the first screw rod (3) are both connected to the first knob (4).

3. A multi-angle clamping and docking simulation device for drone parts as claimed in claim 2, characterized in that: It also includes screws (6), and the upper front part of the support frame (5) is threadedly connected with the screws (6), and the screws (6) are in contact with the adjacent support seats (7).

4. A multi-angle clamping and docking simulation device for drone parts as claimed in claim 3, characterized in that: It also includes a second knob (10), and the front side of the second screw rod (9) is connected to the second knob (10).

5. The multi-angle clamping and docking simulation device for drone parts as claimed in claim 4, characterized in that: The interior of the fixing member (11) is arc-shaped.

6. A multi-angle clamping and docking simulation device for drone parts as claimed in claim 5, characterized in that: It also comprises a telescopic rod (13) and a laser scanner (14); the upper rear side of the base (1) is connected to the telescopic rod (13), and the telescopic end of the telescopic rod (13) is connected to the laser scanner (14).

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