A multi-wire erecting device for Beidou navigation and positioning UAV

Abstract

The present invention discloses a Beidou navigation and positioning UAV multiple-wire stringing device, including a flight bracket, a rope self-weight elastic card and device, a mounting plate, a mounting support, a cantilever, a UAV device and a mounting plate suspension, wherein one end of the cantilever is arranged at the upper end of the flight support, the UAV device is arranged on the other end of the cantilever, the mounting support is arranged on the UAV device, the mounting plate suspension is arranged on the bottom wall of the mounting support, the mounting plate is arranged on the mounting plate suspension, and the rope self-weight elastic card and device are arranged on the mounting plate. The present invention belongs to the field of UAV technology, and specifically refers to a Beidou navigation and positioning UAV multiple-wire stringing device, which not only solves the problems of danger and backwardness of wire stringing in the prior art, but also can fix various types of cables and perform secondary reinforcement on the cables to make the operation more accurate, and can use the Beidou navigation and positioning function according to work needs.

Description

Technical Field

[0001] The invention belongs to the technical field of unmanned aerial vehicles, and specifically refers to a Beidou navigation and positioning unmanned aerial vehicle multi-wire erecting device. Background Art

[0002] With the rapid development of Chinese society, power transmission is also required in many mountainous areas, and power from the west needs to be transmitted to the east through the power transmission system. The power transmission system needs to build transmission lines across mountains and ridges. Especially in the mountainous areas in the west, it is very difficult to build transmission lines to all directions through the mountains. However, the previous method of using people and horses to carry the power is obviously too backward. It not only makes the construction time longer and the construction efficiency low, but also prone to many dangerous accidents, and is greatly affected by the weather. The use of mortars to release the traction rope leads to inaccurate placement of the traction rope, large directional errors, and easy to make the traction rope not put in place, with a high risk factor, high construction difficulty, and correspondingly high construction costs. Summary of the invention

[0003] In order to solve the above problems, the present invention provides a Beidou navigation and positioning UAV multiple cable laying device, which not only solves the problems of dangerous and backward cable laying in the prior art, but also can fix various types of cables and perform secondary reinforcement on the cables to make the operation more accurate, and can use the Beidou navigation and positioning function according to work needs.

[0004] In order to achieve the above functions, the technical solution adopted by the present invention is as follows: a Beidou navigation and positioning UAV multi-wire device, comprising a flight support, a rope self-weight elastic clamping device, a mounting plate, a mounting support, a cantilever, a UAV device and a mounting plate suspension, wherein one end of the cantilever is arranged on the upper end of the flight support, the flight support supports the cantilever, the UAV device is arranged on the other end of the cantilever, and the cantilever supports and fixes the UAV device, the mounting support is arranged on the UAV device, the mounting plate suspension is arranged on the bottom wall of the mounting support, the mounting plate is arranged on the mounting plate suspension, and the rope self-weight elastic clamping device is arranged on the mounting plate; the rope self-weight elastic clamping device comprises a fixed mounting seat, a contraction clamping assembly, a folding sleeve, a rope clamping wheel, a clamping wheel bracket, a rocker arm, a spring and a fixed disk, the upper end of the fixed disk is arranged on the mounting plate through a fixed mounting seat, the mounting plate supports and fixes the fixed disk, and the contraction clamping assembly The assembly is arranged on the fixing plate, the swing arm is arranged on the contraction clamping assembly, one end of the spring is arranged on the fixed mounting seat, and the other end of the spring is arranged on the swing arm, the spring drives the swing arm to drive the contraction clamping assembly, and the contraction clamping assembly fixes the rope. One end of the card wheel bracket is arranged on the lower end of the fixing plate, the folded sleeve is arranged on the lower end of the fixing plate, the folded sleeve is arranged between the card wheel bracket, the rope card wheel is arranged on the other end of the card wheel bracket, the folded sleeve is arranged between the rope card wheel and the fixing plate, the rope first passes through the rope card wheel and then passes through the folded sleeve in the reverse direction and passes through the contraction clamping assembly in the reverse direction again and is arranged on the side of the fixing plate, the rope is folded multiple times and then formed into multiple S shapes and is arranged on the rope self-weight elastic clamping device. Because the rope is folded multiple times in the reverse direction, it is easier to fix. At the same time, the contraction clamping assembly fixes the rope at the end, and the rope is less likely to fall off from the rope self-weight elastic clamping device, so as to realize the fixation of the rope.

[0005] The cam is connected with the fixed plate, and the cam is connected with the fixed plate, and the cam is connected with the fixed plate to the fixed plate, and the cam is connected with the fixed plate to the fixed plate, and the cam is connected with the fixed plate to the fixed plate, and the cam is connected with the fixed plate to the fixed plate.

[0006] Furthermore, the UAV device includes a UAV body, blades, a Beidou navigation and positioning device and a driving motor. The UAV body is arranged at the other end of the cantilever, the Beidou navigation and positioning device is arranged on the UAV body, the Beidou navigation and positioning device performs positioning and navigation, the driving motor is arranged at the upper end of the flight support, the blades are connected to the output shaft of the driving motor, and the driving motor drives the blades to rotate and drives the equipment to fly and move.

[0007] Furthermore, the flight support is made of aluminum alloy.

[0008] Furthermore, the middle of the rope clamping wheel is arranged in a concave structure to facilitate clamping of the rope.

[0009] Furthermore, the rope self-weight elastic locking device is provided with a plurality of groups.

[0010] The present invention adopts the above-mentioned structure to achieve the following beneficial effects: the present invention provides a Beidou navigation and positioning UAV multiple line-laying device, in which a contraction clamping assembly, a folding sleeve and a rope clamping wheel are arranged in sequence, so that the rope can first pass through the rope clamping wheel and then reversely pass through the folding sleeve and then reversely pass through the contraction clamping assembly arranged on the side of the fixed disk. The rope is folded multiple times and then formed into multiple S shapes and arranged on the rope's own weight elastic clamping device. Since the rope is folded multiple times in the reverse direction, it is easier to fix. At the same time, the contraction clamping assembly fixes the rope at the end, and the rope is less likely to fall off from the rope's own weight elastic clamping device, thereby achieving rope fixation. BRIEF DESCRIPTION OF THE DRAWINGS

[0011] Figure 1 This is a schematic diagram of the overall structure of a Beidou navigation and positioning UAV multi-wire erection device of the present invention;

[0012] Figure 2 It is a structural schematic diagram of a rope self-weight elastic clamping device of a Beidou navigation and positioning UAV multi-wire erecting device of the present invention;

[0013] Figure 3 It is a rear view of a rope self-weight elastic clamping device of a Beidou navigation and positioning UAV multiple wire-laying device of the present invention.

[0014] Among them, 1. flight support, 2. rope self-weight elastic clamping device, 3. mounting plate, 4. mounting support, 5. cantilever, 6. UAV device, 7. mounting plate suspension, 8. fixed mounting seat, 9. retractable clamping assembly, 10. folding sleeve, 11. rope clamping wheel, 12. clamping wheel bracket, 13. rocker arm, 14. spring, 15. fixed plate, 16. sliding plate, 17. slide groove, 18. positioning column, 19. claw, 20. crank connecting rod, 21. UAV body, 22. blades, 23. Beidou navigation positioning device, 24. driving motor. DETAILED DESCRIPTION

[0015] The technical solution of the present invention will be described clearly and completely below in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0016] like Figure 1-Figure 3 The present invention discloses a Beidou navigation and positioning UAV multi-wire erecting device, comprising a flight support 1, a rope self-weight elastic clamping device 2, a mounting plate 3, a mounting support 4, a cantilever 5, a UAV device 6 and a mounting plate suspension 7, wherein one end of the cantilever 5 is arranged at the upper end of the flight support 1, the UAV device 6 is arranged on the other end of the cantilever 5, the mounting support 4 is arranged on the UAV device 6, the mounting plate suspension 7 is arranged on the bottom wall of the mounting support 4, the mounting plate 3 is arranged on the mounting plate suspension 7, and the rope self-weight elastic clamping device 2 is arranged on the mounting plate 3; the rope self-weight elastic clamping device 2 comprises a fixed mounting seat 8, a contraction clamping assembly 9, a folded sleeve 10, a rope clamp The wheel 11, the card wheel bracket 12, the rocker arm 13, the spring 14 and the fixed plate 15, the upper end of the fixed plate 15 is arranged on the mounting plate 3 through the fixed mounting seat 8, the contraction clamping assembly 9 is arranged on the fixed plate 15, the rocker arm 13 is arranged on the contraction clamping assembly 9, one end of the spring 14 is arranged on the fixed mounting seat 8, the other end of the spring 14 is arranged on the rocker arm 13, one end of the card wheel bracket 12 is arranged on the lower end of the fixed plate 15, the inflected sleeve 10 is arranged at the lower end of the fixed plate 15, the inflected sleeve 10 is arranged between the card wheel bracket 12, the rope card wheel 11 is arranged on the other end of the card wheel bracket 12, and the inflected sleeve 10 is arranged between the rope card wheel 11 and the fixed plate 15.

[0017] The retractable clamping assembly 9 includes a sliding disk 16, a sliding groove 17, a positioning column 18, a claw 19 and a crank connecting rod 20. The sliding groove 17 is arranged on the sliding disk 16, the positioning column 18 passes through the sliding groove 17 and is arranged on the fixed disk 15, the sliding disk 16 is slidably arranged on the side wall of the fixed disk 15 through the positioning column 18, the rocker arm 13 is arranged on the sliding disk 16, one end of the crank connecting rod 20 is rotatably hinged on the sliding disk 16, one end of the claw 19 is rotatably arranged on the fixed disk 15, and the other end of the claw 19 is rotatably hinged on the other end of the crank connecting rod 20.

[0018] The UAV device 6 includes a UAV body 21, blades 22, a Beidou navigation and positioning device 23 and a drive motor 24. The UAV body 21 is arranged at the other end of the cantilever 5, the Beidou navigation and positioning device 23 is arranged on the UAV body 21, the drive motor 24 is arranged at the upper end of the flight support 1, and the blades 22 are connected to the output shaft of the drive motor 24.

[0019] The flying support 1 is made of aluminum alloy.

[0020] The rope clamping wheel 11 is arranged in a concave structure in the middle.

[0021] The rope self-weight elastic clamping device 2 is provided with several groups.

[0022] When in use, the operator pushes the swing rod 13 to move the swing rod 13 away from the fixed mounting seat 8, and the swing rod 13 applies tension to the spring 14, which elastically deforms and stretches, and the swing rod 13 drives the sliding plate 16 to slide, and the slide groove 17 and the positioning column 18 in the sliding plate 16 slide relative to each other to achieve displacement, and the sliding plate 16 slides and pushes the crank connecting rod 20 to rotate, and the crank connecting rod 20 pushes the claw 19 to rotate and open with the hinged part with the fixed plate 15 as the rotation axis, and the rope first passes through the rope clamping wheel 11, then passes through the reverse folding sleeve 10, and then passes through the contraction clamping assembly 9 arranged on the side of the fixed plate 15 in the reverse direction, and the rope is folded multiple times and then formed into a A plurality of S-shaped clamps are arranged between the claws 19. After the rope passes through the claws 19, the operator releases the rocker arm 13, and the spring 14 can apply a driving force to the rocker arm 13, driving the rocker arm 13 to move to a position close to the fixed mounting seat 8. The rocker arm 13 drives the sliding disk 16 to slide, and the slide groove 17 and the positioning column 18 in the sliding disk 16 slide relative to each other to achieve displacement. The sliding disk 16 slides and drives the crank connecting rod 20 to rotate. The crank connecting rod 20 drives the claw 19 to rotate and close with the hinged part with the fixed disk 15 as the rotation axis to fix the rope. The drive motor 24 works to drive the blades 22 to rotate, and drives the equipment to fly and move according to the positioning of the Beidou navigation positioning device 23.

[0023] The present invention and its embodiments are described above, and such description is not restrictive. The drawings show only one embodiment of the present invention, and the actual structure is not limited thereto. In short, if ordinary technicians in the field are inspired by it, without departing from the purpose of the invention, they can design a structure and embodiment similar to the technical solution without creativity, which should belong to the protection scope of the present invention.

Claims

1. A Beidou navigation and positioning UAV multi-wire device, characterized by: The invention comprises a flight support, a rope self-weight elastic clamping device, a mounting plate, a mounting support, a cantilever, a UAV device and a mounting plate suspension, wherein one end of the cantilever is arranged at the upper end of the flight support, the UAV device is arranged on the other end of the cantilever, the mounting support is arranged on the UAV device, the mounting plate suspension is arranged on the bottom wall of the mounting support, the mounting plate is arranged on the mounting plate suspension, and the rope self-weight elastic clamping device is arranged on the mounting plate; the rope self-weight elastic clamping device comprises a fixed mounting seat, a contraction clamping assembly, a folded sleeve, a rope clamp A wheel, a card wheel bracket, a swing rod, a spring and a fixed plate, wherein the upper end of the fixed plate is arranged on the mounting plate through a fixed mounting seat, the contraction clamping assembly is arranged on the fixed plate, the swing rod is arranged on the contraction clamping assembly, one end of the spring is arranged on the fixed mounting seat, the other end of the spring is arranged on the swing rod, one end of the card wheel bracket is arranged on the lower end of the fixed plate, the folded sleeve is arranged on the lower end of the fixed plate, the folded sleeve is arranged between the card wheel brackets, the rope card wheel is arranged on the other end of the card wheel bracket, and the folded sleeve is arranged between the rope card wheel and the fixed plate; The contraction clamping assembly includes a sliding plate, a sliding groove, a positioning column, a claw and a crank connecting rod, wherein the sliding groove is arranged on the sliding plate, the positioning column penetrates the sliding groove and is arranged on the fixed plate, the sliding plate is slidably arranged on the side wall of the fixed plate through the positioning column, the swing rod is arranged on the sliding plate, one end of the crank connecting rod is rotatably hinged on the sliding plate, one end of the claw is rotatably arranged on the fixed plate, and the other end of the claw is rotatably hinged on the other end of the crank connecting rod; The spring applies a pushing force to the swing rod, driving the swing rod to move to a position close to the fixed mounting seat, and the swing rod drives the sliding plate to slide, and the sliding groove and the positioning column in the sliding plate slide relative to each other; The sliding disk slides to push the crank connecting rod to rotate, and the crank connecting rod pushes the clamping claw to rotate and close with the hinged position with the fixed disk as the rotation axis.

2. A Beidou navigation and positioning UAV multi-wire device according to claim 1, characterized in that: The UAV device includes a UAV body, blades, a Beidou navigation and positioning device and a drive motor. The UAV body is arranged at the other end of the cantilever, the Beidou navigation and positioning device is arranged on the UAV body, the drive motor is arranged at the upper end of the flight support, and the blades are connected to the output shaft of the drive motor.

3. The Beidou navigation and positioning UAV multi-wire erecting device according to claim 1, characterized in that: The flight support is made of aluminum alloy.

4. The Beidou navigation and positioning UAV multi-wire erecting device according to claim 1, characterized in that: The middle of the rope clamping wheel is arranged in a concave structure.

5. The Beidou navigation and positioning UAV multi-wire erecting device according to claim 1, characterized in that: The rope self-weight elastic clamping device is provided with a plurality of groups.

Images