Unmanned aerial vehicle fuselage clamping device

Abstract

The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle body clamping device which comprises a base. A supporting plate is arranged at the top end of the base; a pair of connecting plates is arranged on one side of each of the pair of supporting plates; a pair of sliding grooves is formed in one side of each connecting plate. The bottom ends of the interiors of the pair of sliding grooves are rotationally connected with two-way threaded rods. One end of each bidirectional threaded rod penetrates through the top end of the corresponding connecting plate and is fixedly connected with a rotating wheel; a pair of sliding blocks is in threaded connection with each of the two-way threaded rods; in order to make up for the defects in the prior art and solve the problems that when an existing unmanned aerial vehicle body fixing device fixes a vehicle body, the height of fixing equipment cannot be adjusted, the height of the fixing equipment cannot be adjusted, and the height of the fixing equipment cannot be adjusted. The problems that in the maintenance process, workers need to frequently stoop down or lift arms to adapt to the position of the unmanned aerial vehicle due to the fact that the workers need to maintain the unmanned aerial vehicle, the labor intensity of the workers is increased, and the maintenance quality cannot be improved easily are solved.

Description

Technical Field

[0001] The utility model belongs to the technical field of unmanned aerial vehicles, in particular to a clamping device for a fuselage of an unmanned aerial vehicle. Background Art

[0002] A drone, also known as a drone or unmanned aerial vehicle, is an aircraft that can fly without a pilot or by remote control. They can be used for various purposes, including military, commercial, scientific research, and entertainment. Due to environmental factors and mechanical wear and tear, drones need to be maintained, so a device is needed to fix the drone body.

[0003] In the prior art, when the existing UAV fuselage fixing device fixes the fuselage, since the fixing device itself cannot be adjusted in height, the staff needs to frequently bend over or raise their arms to adapt to the position of the UAV during the maintenance process. This not only increases the labor intensity of the staff, but also is not conducive to improving the maintenance quality.

[0004] To this end, the utility model provides a drone fuselage clamping device. Utility Model Content

[0005] In order to make up for the shortcomings of the existing technology and to solve the problem that when the existing UAV fuselage fixing device fixes the fuselage, the fixing device itself cannot be height adjusted, which results in the staff needing to frequently bend over or raise their arms to adapt to the position of the UAV during the maintenance process. This not only increases the labor intensity of the staff, but also is not conducive to improving the maintenance quality.

[0006] The technical solution adopted by the utility model to solve its technical problems is: the utility model describes a drone fuselage clamping device, comprising a base; a support plate is provided at the top of the base; a pair of connecting plates are provided on one side of a pair of the support plates; a pair of slide grooves are provided on one side of a pair of the connecting plates; a pair of two-way threaded rods are rotatably connected to the bottom ends of the inner parts of the pair of slide grooves; one end of a group of two-way threaded rods respectively penetrates the top of the connecting plate and is fixedly connected with a rotating wheel; a pair of sliders are threadedly connected to a group of two-way threaded rods; an arc-shaped clamping plate is fixedly connected to one side of a pair of sliders; a protective pad is provided on the clamping surface of the arc-shaped clamping plate; a lifting component is provided on one side of the base; the lifting component is used to drive the lifting and lowering of a pair of connecting plates.

[0007] Preferably, the lifting assembly includes a groove and a power unit; the groove is opened at the top of the base; a limit plate is fixed inside the groove; a U-shaped plate is provided at the top of the limit plate; a pair of support plates are respectively fixed to the top of the U-shaped plate; a pair of first rotating rods are rotatably connected to the bottom end of the limit plate, and one end of the pair of first rotating rods passes through the limit plate; the U-shaped plate is rotatably connected to a pair of first rotating rods.

[0008] Preferably, the power unit includes a motor; the motor is fixedly connected to one side of the base through a first fixed rod; a second rotating rod is provided at the output end of the motor; one end of the second rotating rod passes through the inside of the base and is rotatably connected to the inner wall of the base; a pair of first bevel gears are fixedly connected to the second rotating rod; a pair of second bevel gears are fixedly connected to the bottom ends of the first rotating rods; the first bevel gear and the second bevel gear transmit to each other.

[0009] Preferably, a pair of support plates are each provided with a through groove on one side; a turntable is rotatably connected in the pair of through grooves; a pair of turntables are each provided with a connecting column on one side, and one end of the pair of connecting columns passes through the turntable and is fixedly connected to one side of the connecting plate; the pair of connecting columns are respectively slidably connected in the turntable; and the other end of the pair of connecting columns is fixedly connected to a limiting block.

[0010] Preferably, a group of slots are provided on one side of a pair of turntables; an elastic telescopic rod is fixedly connected inside one side of a pair of support plates; one end of a pair of elastic telescopic rods is fixedly connected to a connecting block; one end of a pair of connecting blocks is fixedly connected to a second fixing rod; and a pair of second fixing rods are slidably connected in the slots.

[0011] Preferably, a group of square boxes is fixedly connected to the top end of the U-shaped plate.

[0012] The beneficial effects of the utility model are as follows:

[0013] 1. The utility model describes a drone fuselage clamping device, which is provided with a base, a pair of support plates are provided on the top of the base, a pair of connecting plates are provided on the inner side of the support plates, a side slide groove is provided on the inner side of the connecting plate, a two-way threaded rod is provided in the slide groove, and a pair of sliders are provided on the two-way threaded rods, and an arc-shaped clamping plate is fixedly connected to one side of the slider, which can be used to adjust the width between the slide groove clamping plates, so as to facilitate the clamping of fuselages of different thicknesses. A lifting component is provided on the base, so that the staff can find a suitable height to repair the drone fuselage.

[0014] 2. The utility model describes a drone fuselage clamping device, which opens a through groove on one side of a pair of support plates, and sets a rotatable turntable in the through groove, and sets a connecting column on one side of the turntable, so that the connecting column passes through the turntable and is fixed to the connecting plate. In this way, not only the connecting plate can be supported, but also fuselages of different sizes can be clamped. The turntable is rotatable, so that the staff can flip the fuselage so that both sides can face up, which is convenient for the staff to observe and repair both sides. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] The utility model will be further described below in conjunction with the accompanying drawings.

[0016] Figure 1It is a three-dimensional diagram of the utility model;

[0017] Figure 2 It is the front view of the utility model;

[0018] Figure 3 It is a cross-sectional view in the utility model;

[0019] Figure 4 It is a schematic diagram of a local structure in the utility model;

[0020] Figure 5 yes Figure 1 A magnified view of middle;

[0021] In the figure: 1. base; 2. support plate; 3. connecting plate; 4. slide groove; 5. bidirectional threaded rod; 6. rotating wheel; 7. slider; 8. arc clamping plate; 9. groove; 10. limit plate; 11. U-shaped plate; 12. first rotating rod; 13. motor; 14. first fixed rod; 15. second rotating rod; 16. first bevel gear; 17. second bevel gear; 18. through groove; 19. turntable; 20. connecting column; 21. limiting block; 22. slot; 23. elastic telescopic rod; 24. connecting block; 25. second fixed rod; 26. square box. DETAILED DESCRIPTION

[0022] In order to make the technical means, creative features, objectives and effects achieved by the present invention easy to understand, the present invention is further described below in conjunction with specific implementation methods.

[0023] like Figures 1 to 5 As shown, a drone fuselage clamping device described in an embodiment of the utility model comprises a base 1; a support plate 2 is provided at the top of the base 1; a pair of connecting plates 3 are provided on one side of a pair of the supporting plates 2; a pair of slide grooves 4 are provided on one side of a pair of connecting plates 3; a pair of two-way threaded rods 5 are rotatably connected to the bottom ends of the inner parts of a pair of slide grooves 4; one end of a group of two-way threaded rods 5 respectively penetrates the top of the connecting plate 3 and is fixedly connected to a rotating wheel 6; a pair of two-way threaded rods 5 are threadedly connected to a pair of sliders 7; a pair of sliders 7 are fixedly connected to one side of an arc-shaped clamping plate 8; a protective pad is provided on the clamping surface of the arc-shaped clamping plate 8; the A lifting component is provided on one side of the base 1; the lifting component is used to drive the lifting of a pair of connecting plates 3. When working, by setting the base 1, a pair of support plates 2 are set on the top of the base 1, a pair of connecting plates 3 are set on the inner side of the support plate 2, and a side slide groove 4 is opened on the inner side of the connecting plate 3. A two-way threaded rod 5 is set in the slide groove 4, and a pair of sliders 7 are set on the two-way threaded rod 5. An arc-shaped clamping plate 8 is fixedly connected to one side of the slider 7. It can be used to adjust the width between the clamping plates of the slide groove 4, which is convenient for clamping fuselages of different thicknesses. The lifting component is set on the base 1, which is convenient for the staff to find a suitable height to repair the drone fuselage.

[0024] The lifting assembly includes a groove 9 and a power unit; the groove 9 is opened at the top of the base 1; a limit plate 10 is fixed inside the groove 9; a U-shaped plate 11 is provided at the top of the limit plate 10; a pair of support plates 2 are respectively fixed to the top of the U-shaped plate 11; a pair of first rotating rods 12 are rotatably connected to the bottom end of the limit plate 10, and one end of a pair of first rotating rods 12 passes through the limit plate 10; the U-shaped plate 11 is rotatably connected to a pair of first rotating rods 12. When working, by opening a groove 9 on the base 1, setting a limit plate 10 in the groove 9, and setting a pair of first rotating rods 12 at the bottom end of the limit plate 10, and by passing the rotating rod through the top of the limit plate 10, it is convenient for the power part to drive the U-shaped plate 11 to slide upward on the rotating rod, so as to drive the support plate 2 upward, so that the staff can adjust the height to repair the drone fuselage.

[0025] The power unit includes a motor 13; the motor 13 is fixedly connected to one side of the base 1 through a first fixed rod 14; a second rotating rod 15 is provided at the output end of the motor 13; one end of the second rotating rod 15 passes through the inside of the base 1 and is rotatably connected to the inner wall of the base 1; a pair of first bevel gears 16 are fixedly connected to the second rotating rod 15; a pair of second bevel gears 17 are fixedly connected to the bottom ends of the first rotating rods 12; the first bevel gears 16 and the second bevel gears 17 transmit to each other, and when working, by fixing the motor 13 on one side of the base 1, and by setting the second rotating rod 15 at the output end of the motor 13, when the second rotating rod 15 rotates, the first bevel gear 16 transmits a pair of second bevel gears 17, so that the first rotating rod 12 rotates, thereby driving the U-shaped plate 11 to move upward, so as to complete the height adjustment of the support plate 2.

[0026] A pair of the support plates 2 are provided with a through slot 18 on one side; a pair of the through slots 18 are rotatably connected with a turntable 19; a pair of the turntables 19 are provided with a connecting column 20 on one side, and one end of the pair of connecting columns 20 passes through the turntable 19 and is fixedly connected to one side of the connecting plate 3; a pair of the connecting columns 20 are respectively slidably connected in the turntable 19; the other end of the pair of connecting columns 20 is fixedly connected with a limiting block 21. During operation, a through slot 18 is provided on one side of a pair of support plates 2, and a rotatable turntable 19 is arranged in the through slot 18, and a connecting column 20 is arranged on one side of the turntable 19, so that the connecting column 20 passes through the turntable 19 and is fixedly connected to the connecting plate 3. In this way, not only the connecting plate 3 can be supported, but also fuselages of different sizes can be clamped. The turntable 19 is arranged to be rotatable, so that the staff can flip the fuselage so that both sides can be upward, which is convenient for the staff to observe and repair both sides.

[0027] A group of slots 22 are provided on one side of a pair of turntables 19; an elastic telescopic rod 23 is fixedly connected inside one side of a pair of support plates 2; one end of a pair of elastic telescopic rods 23 is fixedly connected to a connecting block 24; one end of a pair of connecting blocks 24 is fixedly connected to a second fixing rod 25; a pair of second fixing rods 25 are slidably connected in the slots 22. During operation, after the staff raises the support plate 2 to a suitable position and rotates the connecting plate 3 to adjust the fuselage to an angle convenient for maintenance, the staff can pull the elastic telescopic rod 23 to clamp the fixing rod in the slot 22 to fix the position of the turntable 19, which can effectively assist the staff in repairing the drone fuselage.

[0028] A group of square boxes 26 are fixedly connected to the top of the U-shaped plate 11. During operation, by setting a group of square boxes 26 inside the U-shaped plate 11, when the staff maintains or disassembles the fuselage, the parts can be placed in the square boxes 26 to prevent the parts from falling and affecting the assembly.

[0029] Working principle: by setting a base 1, a pair of support plates 2 are set on the top of the base 1, a pair of connecting plates 3 are set on the inner side of the support plate 2, a side slide groove 4 is opened on the inner side of the connecting plate 3, a two-way threaded rod 5 is set in the slide groove 4, a pair of sliders 7 are set on the two-way threaded rod 5, and an arc-shaped clamping plate 8 is fixed on one side of the slider 7, which can be used to adjust the width between the clamping plates of the slide groove 4, so as to facilitate the clamping of fuselages of different thicknesses. A lifting component is set on the base 1 to facilitate the staff to find a suitable height to repair the drone fuselage. By opening a lifting component on the base 1, a lifting component is set on the base 1 to facilitate the staff to find a suitable height to repair the drone fuselage. The groove 9 is provided with a limit plate 10 in the groove 9, and a pair of first rotating rods 12 are provided at the bottom of the limit plate 10. By passing the rotating rod through the top of the limit plate 10, it is convenient for the power part to drive the U-shaped plate 11 to slide upward on the rotating rod, so as to drive the support plate 2 upward, so that the staff can adjust the height to repair the drone body. By fixing the motor 13 on one side of the base 1, and by setting the second rotating rod 15 at the output end of the motor 13, when the second rotating rod 15 rotates, the first bevel gear 16 drives a pair of second bevel gears 17, so that the first rotating rod 12 rotates, thereby driving the U-shaped plate 11 to move upward to complete the height adjustment of the support plate 2. A through slot 18 is provided on one side of a pair of support plates 2, and a rotatable turntable 19 is provided in the through slot 18. A connecting column 20 is provided on one side of the turntable 19, so that the connecting column 20 passes through the turntable 19 and is fixed to the connecting plate 3. In this way, not only the connecting plate 3 can be supported, but also fuselages of different sizes can be clamped. The turntable 19 is arranged to be rotatable, so that the staff can flip the fuselage so that both sides can face up, which is convenient for the staff to adjust the two sides. The U-shaped plate 11 is provided with a group of square boxes 26, so that when the staff maintains or disassembles the fuselage, the parts can be placed in the square boxes 26 to prevent the parts from falling and affecting the assembly.

[0030] The above-mentioned front, back, left, right, top and bottom are all based on the figures in the specification. Figure 1 As a benchmark, according to the person's observation perspective, the side of the device facing the observer is defined as the front, the left side of the observer is defined as the left, and so on.

[0031] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", etc., indicating orientations or positional relationships, are based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as limiting the scope of protection of the present invention.

[0032] The above shows and describes the basic principles, main features and advantages of the utility model. Those skilled in the art should understand that the utility model is not limited by the above embodiments. The above embodiments and descriptions are only for explaining the principles of the utility model. Without departing from the spirit and scope of the utility model, the utility model may have various changes and improvements, which fall within the scope of the utility model to be protected. The scope of protection claimed by the utility model is defined by the attached claims and their equivalents.

Claims

1. A UAV fuselage clamping device, characterized in that: The invention comprises a base (1); a support plate (2) is provided at the top of the base (1); a pair of connecting plates (3) are provided on one side of a pair of the support plates (2); a pair of slide grooves (4) are provided on one side of a pair of the connecting plates (3); a pair of bidirectional threaded rods (5) are rotatably connected to the bottom ends of the inner parts of the pair of slide grooves (4); one end of a group of bidirectional threaded rods (5) respectively penetrates the top of the connecting plate (3) and is fixedly connected to a rotating wheel (6); a pair of sliders (7) are threadedly connected to a group of bidirectional threaded rods (5); an arc-shaped clamping plate (8) is fixedly connected to one side of the pair of sliders (7); a protective pad is provided on the clamping surface of the arc-shaped clamping plate (8); a lifting assembly is provided on one side of the base (1); the lifting assembly is used to drive the lifting of the pair of connecting plates (3).

2. The UAV fuselage clamping device according to claim 1, characterized in that: The lifting assembly comprises a groove (9) and a power unit; the groove (9) is opened at the top of the base (1); a limit plate (10) is fixedly connected inside the groove (9); a U-shaped plate (11) is provided at the top of the limit plate (10); a pair of support plates (2) are respectively fixedly connected to the top of the U-shaped plate (11); a pair of first rotating rods (12) are rotatably connected to the bottom end of the limit plate (10), and one end of the pair of first rotating rods (12) passes through the limit plate (10); the U-shaped plate (11) is rotatably connected to the pair of first rotating rods (12).

3. The UAV fuselage clamping device according to claim 2, characterized in that: The power unit comprises a motor (13); the motor (13) is fixedly connected to one side of the base (1) via a first fixing rod (14); a second rotating rod (15) is provided at the output end of the motor (13); one end of the second rotating rod (15) passes through the inside of the base (1) and is rotatably connected to the inner wall of the base (1); a pair of first bevel gears (16) are fixedly connected to the second rotating rod (15); the bottom ends of the pair of first rotating rods (12) are both fixedly connected to a second bevel gear (17); the first bevel gear (16) and the second bevel gear (17) are mutually driven.

4. The UAV fuselage clamping device according to claim 3 is characterized in that: A pair of support plates (2) are each provided with a through slot (18) on one side; a turntable (19) is rotatably connected in the pair of through slots (18); a pair of turntables (19) are each provided with a connecting column (20) on one side, and one end of the pair of connecting columns (20) passes through the turntable (19) and is fixedly connected to one side of the connecting plate (3); the pair of connecting columns (20) are respectively slidably connected in the turntable (19); and a limiting block (21) is fixedly connected to the other end of the pair of connecting columns (20).

5. The UAV fuselage clamping device according to claim 4, characterized in that: A group of slots (22) are provided on one side of the pair of rotating disks (19); an elastic telescopic rod (23) is fixedly connected inside one side of the pair of supporting plates (2); one end of the pair of elastic telescopic rods (23) is fixedly connected to a connecting block (24); one end of the pair of connecting blocks (24) is fixedly connected to a second fixing rod (25); and the pair of second fixing rods (25) are slidably connected in the slots (22).

6. The UAV fuselage clamping device according to claim 5, characterized in that: A group of square boxes (26) is fixedly connected to the top end of the U-shaped plate (11).

Images