Unmanned aerial vehicle nest for electric power inspection

Abstract

The utility model relates to the technical field of unmanned aerial vehicle nests, and discloses an unmanned aerial vehicle nest for electric power inspection, which comprises a base, a fuselage fixedly mounted at the upper part of the base, an opening and closing cover plate arranged at the upper part of the fuselage, a rain baffle fixedly mounted at the upper part of the opening and closing cover plate, and a conical block fixedly connected to the upper part of the rain baffle, the rain shed is fixedly installed on the left side of the machine body, the connecting assembly is arranged on one side of the machine body and comprises a moving mechanism arranged on the lower portion of the machine body, a dismounting and mounting mechanism is arranged on the left side of the machine body, the bottom end of a supporting rod is rotationally connected with a first sliding block through a pin, and one end of a first spring is fixedly connected with the first sliding block; one end of the second spring is fixedly connected with the abutting block, and the abutting block and the abutting groove are arranged in a clamped mode. The problems that an existing device is inconvenient to move, so that the device is inconvenient to transfer manually, and when the device needs to be transferred outdoors, labor is wasted are solved.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle nests, in particular to an unmanned aerial vehicle nest for power inspection. Background Technique

[0002] An unmanned aerial vehicle nest is a platform that enables the automatic take-off and landing of unmanned aerial vehicles. The unmanned aerial vehicle nest can be placed in the wild for use. Staff can remotely control the unmanned aerial vehicle to fly out of and land on the nest automatically, and can also automatically charge and replace the battery of the unmanned aerial vehicle. The existing unmanned aerial vehicle nests usually include an automatically opening and closing cover plate and a main body. The automatically opening and closing cover plate can be automatically opened and closed to allow the unmanned aerial vehicle to fly out and seal and shield the main body. When the unmanned aerial vehicle returns, the automatically opening and closing cover plate automatically opens, and the unmanned aerial vehicle lands on the main body.

[0003] According to an unmanned aerial vehicle nest for power inspection disclosed in the patent publication number CN 220465833 U, the device uses the mutual cooperation of a first inclined plate, a side plate, a second inclined plate, a docking plate and a conical block. The side plate seals the two sides of the first inclined plate, the side plate and the second inclined plate. The docking plate and the conical block are docked and fitted. The first inclined plate, the second inclined plate and the conical block are inclined, which is beneficial to guide rain for the opening and closing cover plate, allowing the rainwater to flow away, and facilitating the prevention of rainwater remaining between the two opening and closing cover plates. However, the device is not easy to move, so it is not convenient for manual transportation operation of the device. When it is necessary to transport the device outdoors, it is more laborious.

[0004] Therefore, we propose an unmanned aerial vehicle nest for power inspection to solve the problem. Content of the Utility Model

[0005] The purpose of the utility model is to provide an unmanned aerial vehicle nest for power inspection, which solves the problems raised in the above background technique.

[0006] To achieve the above purpose, the utility model provides the following technical scheme: an unmanned aerial vehicle nest for power inspection, including a base;

[0007] A fuselage fixedly installed on the upper part of the base;

[0008] An opening and closing cover plate arranged on the upper part of the fuselage;

[0009] A rain shield fixedly installed on the upper part of the opening and closing cover plate;

[0010] A conical block fixedly connected to the upper part of the rain shield;

[0011] A rain shed fixedly installed on the left side of the fuselage;

[0012] and a connection component disposed on one side of the fuselage, the connection component including a moving mechanism disposed at the lower part of the fuselage, and a disassembly and assembly mechanism disposed on the left side of the fuselage.

[0013] Preferably, the moving mechanism includes a hydraulic cylinder fixedly installed on the inner wall of the base, the output end of the hydraulic cylinder is fixedly connected with a connecting plate, the bottom of the connecting plate is fixedly connected with a mounting block, the bottom of the mounting block is rotationally connected with a support rod through a pin, the bottom of the support rod is provided with a mounting plate, a first sliding groove is opened on the upper part of the mounting plate, a first sliding rod is fixedly connected to the inner wall of the first sliding groove, a first sliding block is slidably connected to the outer wall of the first sliding rod, a first spring is fixedly connected to the inner wall of the first sliding groove, a pressing groove is opened on the inner wall of the first sliding groove, an inner groove is opened inside the first sliding block, a pressing block is sleeved inside the inner groove, a second spring is fixedly connected to the inner wall of the inner groove, and a moving wheel is arranged at the bottom of the mounting plate.

[0014] Preferably, the disassembly and assembly mechanism includes a heat dissipation hole opened on the left side of the fuselage, a placement groove is opened outside the heat dissipation hole, a dust-proof plate is clamped on the inner wall of the placement groove, a clamping groove is opened on the outside of the dust-proof plate, a second sliding groove is opened on the left side of the fuselage, a second sliding rod is fixedly connected to the inner wall of the second sliding groove, a second sliding block is slidably connected to the outer wall of the second sliding rod, a third spring is fixedly connected to the inner wall of the second sliding groove, a connecting rod is fixedly connected to the outside of the second sliding block, one end of the connecting rod is movably connected with a clamping rod, a limiting block is fixedly connected to the outer end of the clamping rod, and a fourth spring is fixedly connected to the outside of the connecting rod.

[0015] Preferably, the bottom end of the support rod is rotationally connected with the first sliding block through a pin, one end of the first spring is fixedly connected with the first sliding block. Through the cooperation of the hydraulic cylinder, the connecting plate, the mounting block, the support rod, the first sliding rod, the first sliding block, and the first spring, relative movement can occur between the base and the ground. When the base is far from the ground, it is convenient for manual transfer operation of the device, thereby increasing the applicability of the device. At the same time, under the action of the elastic force of the first spring, when the device is jolted during movement, a buffering effect can be achieved, thereby preventing the device from being damaged due to jolts.

[0016] Preferably, one end of the second spring is fixedly connected with the pressing block, and the pressing block is clamped with the pressing groove. Through the cooperation of the pressing block, the pressing groove, and the second spring, when the first sliding block and the first sliding groove slide relative to each other, the pressing block and the pressing groove can slide relative to each other, thereby reducing the elastic potential energy generated by the first spring during the buffering process, and further achieving a shock absorption effect.

[0017] Preferably, one end of the fourth spring away from the connecting rod is fixedly connected to the limiting block. The clamping rod is adapted to the clamping groove. Through the cooperation of the heat dissipation holes and the dust-proof plate, it can prevent external dust from entering the fuselage through the heat dissipation holes. Through the cooperation of the fourth spring, the connecting rod, the second sliding rod, the second slider, the clamping rod and the clamping groove, it is convenient for manual disassembly of the dust-proof plate, so as to facilitate manual cleaning of the dust-proof plate, and further prevent the mesh holes of the dust-proof plate from being blocked, affecting the heat dissipation effect of the device.

[0018] Preferably, one end of the third spring is fixedly connected to the second slider. Through the cooperation of the second sliding rod, the second slider and the third spring, the connecting rod can stay at a position away from the dust-proof plate, so that the operator can free up his hands, and it is more convenient for the operator to disassemble and assemble the dust-proof plate.

[0019] The utility model provides a drone nest for power inspection. The drone nest for power inspection has the following beneficial effects:

[0020] (1) For this drone nest for power inspection, by setting the moving mechanism, under the action of the hydraulic cylinder, the connecting plate, the mounting block, the support rod, the first sliding rod, the first slider and the first spring, the base can move relative to the ground. When the base moves away from the ground, it is convenient for manual transportation of the device, thereby increasing the applicability of the device. At the same time, under the action of the first spring, when the device is jolted during movement, it can play a buffering effect, thus preventing the device from being damaged due to jolts. Under the action of the pressing block, the pressing groove and the second spring, when the first slider slides relative to the first sliding groove, the pressing block can slide relative to the pressing groove, thereby reducing the elastic potential energy generated by the first spring during buffering, and further playing a shock-absorbing effect;

[0021] (2) For this drone nest for power inspection, by setting the disassembly and assembly mechanism, under the action of the heat dissipation holes and the dust-proof plate, it can prevent external dust from entering the fuselage through the heat dissipation holes. Under the action of the fourth spring, the connecting rod, the second sliding rod, the second slider, the clamping rod and the clamping groove, it is convenient for manual disassembly of the dust-proof plate, so as to facilitate manual cleaning of the dust-proof plate, and further prevent the mesh holes of the dust-proof plate from being blocked, affecting the heat dissipation effect of the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] Figure 1 is a schematic diagram of the overall structure of the utility model;

[0023] Figure 2 is a schematic diagram of the overall sectional structure of the utility model;

[0024] Figure 3 is a schematic diagram of the moving mechanism structure of the utility model;

[0025] Figure 4This is a schematic diagram of the partial structure of the moving mechanism of the present utility model;

[0026] Figure 5 This is a schematic diagram of the disassembly and assembly mechanism of the present utility model;

[0027] In the figure: 1, base; 2, fuselage; 3, connection component; 31, moving mechanism; 311, hydraulic cylinder; 312, connecting plate; 313, mounting block; 314, support rod; 315, first chute; 316, first slide bar; 317, first slider; 318, first spring; 319, pressing groove; 3110, inner groove; 3111, pressing block; 3112, second spring; 3113, mounting plate; 32, disassembly and assembly mechanism; 321, heat dissipation hole; 322, placement groove; 323, dust-proof plate; 324, clamping groove; 325, second chute; 326, second slide bar; 327, second slider; 328, third spring; 329, connecting rod; 3210, clamping rod; 3211, fourth spring; 4, opening and closing cover plate; 5, rain shield; 6, conical block; 7, canopy. Specific embodiments

[0028] In order to have a clearer understanding of the technical features, objectives, and effects of the present utility model, the specific embodiments of the present utility model will now be described with reference to the accompanying drawings.

[0029] Embodiment 1

[0030] As Figures 1-5 shown, the present utility model provides a technical solution: an unmanned aerial vehicle nest for power inspection, including a base 1, a fuselage 2 fixedly installed on the upper part of the base 1, an opening and closing cover plate 4 arranged on the upper part of the fuselage 2, a rain shield 5 fixedly installed on the upper part of the opening and closing cover plate 4, a conical block 6 fixedly connected to the upper part of the rain shield 5, a canopy 7 fixedly installed on the left side of the fuselage 2, and a connection component 3 arranged on one side of the fuselage 2. The connection component 3 includes a moving mechanism 31 arranged at the lower part of the fuselage 2, and a disassembly and assembly mechanism 32 arranged on the left side of the fuselage 2. The moving mechanism 31 includes a hydraulic cylinder 311 fixedly installed on the inner wall of the base 1. The output end of the hydraulic cylinder 311 is fixedly connected to a connecting plate 312. The bottom of the connecting plate 312 is fixedly connected to a mounting block 313. The bottom of the mounting block 313 is rotatably connected to a support rod 314 through a pin. The bottom of the support rod 314 is provided with a mounting plate 3113. The upper part of the mounting plate 3113 is provided with a first chute 315. The inner wall of the first chute 315 is fixedly connected to a first slide bar 316. The outer wall of the first slide bar 316 is slidably connected to a first slider 317. The inner wall of the first chute 315 is fixedly connected to a first spring 318. The inner wall of the first chute 315 is provided with a pressing groove 319. The inside of the first slider 317 is provided with an inner groove 3110. The inside of the inner groove 3110 is sleeved with a pressing block 3111. The inner wall of the inner groove 3110 is fixedly connected to a second spring 3112. The bottom of the mounting plate 3113 is provided with moving wheels.

[0031] In this embodiment, the bottom end of the support rod 314 is rotatably connected to the first slider 317 through a pin. One end of the first spring 318 is fixedly connected to the first slider 317. Through the cooperation of the hydraulic cylinder 311, the connecting plate 312, the mounting block 313, the support rod 314, the first slide bar 316, the first slider 317, and the first spring 318, relative movement can occur between the base 1 and the ground. When the base 1 moves away from the ground, it is convenient for manual transfer operation of the device, thereby increasing the applicability of the device. At the same time, under the action of the elastic force of the first spring 318, when the device is jolted during movement, a buffering effect can be achieved, thereby preventing damage to the device caused by jolts.

[0032] Further, one end of the second spring 3112 is fixedly connected to the pressing block 3111. The pressing block 3111 is snap - connected to the pressing groove 319. Through the cooperation of the pressing block 3111, the pressing groove 319, and the second spring 3112, when the first slider 317 and the first sliding groove 315 slide relative to each other, the pressing block 3111 and the pressing groove 319 can slide relative to each other, thereby reducing the elastic potential energy generated by the first spring 318 during the buffering process, and further achieving a shock - absorbing effect.

[0033] When the device needs to be moved, first, the hydraulic cylinder 311 drives the connecting plate 312 to move downward, thereby enabling the mounting plate 3113 provided below the connecting plate 312 to move downward, and further enabling the moving wheels provided at the bottom of the mounting plate 3113 to move downward. When the moving wheels contact the ground, under the action of the interaction of forces, the base 1 can be moved away from the ground, and then the device can be transferred. Further, when the device is jolted during movement, under the action of gravity, relative movement can occur between the mounting plate 3113 and the connecting plate 312. Under the action of the mounting block 313, the support rod 314, and the first slider 317, the first slider 317 can slide in the first sliding groove 315 through the first slide bar 316, thereby deforming the first spring 318. Under the action of the elastic force of the first spring 318, a buffering effect can be achieved. And when the first slider 317 moves, under the action of the elastic force of the second spring 3112, the pressing block 3111 and the pressing groove 319 can slide relative to each other, so that under the action of the pressing force, the elastic potential energy generated by the first spring 318 during the buffering process can be reduced, and further a shock - absorbing effect can be achieved, thereby preventing damage to the device caused by jolts.

[0034] Embodiment 2

[0035] Based on Embodiment 1, a preferred embodiment of the UAV nest for power inspection provided by the present utility model is as Figures 1 to 5As shown: The disassembly and assembly mechanism 32 includes a heat dissipation hole 321 opened on the left side of the fuselage 2. A placement groove 322 is opened outside the heat dissipation hole 321. A dust-proof plate 323 is clamped on the inner wall of the placement groove 322. A clamping groove 324 is opened on the outer side of the dust-proof plate 323. A second sliding groove 325 is opened on the left side of the fuselage 2. A second sliding rod 326 is fixedly connected to the inner wall of the second sliding groove 325. A second slider 327 is slidably connected to the outer wall of the second sliding rod 326. A third spring 328 is fixedly connected to the inner wall of the second sliding groove 325. A connecting rod 329 is fixedly connected to the outer side of the second slider 327. One end of the connecting rod 329 is movably connected to a clamping rod 3210. A limiting block is fixedly connected to the outer end of the clamping rod 3210. A fourth spring 3211 is fixedly connected to the outer side of the connecting rod 329.

[0036] In this embodiment, one end of the fourth spring 3211 away from the connecting rod 329 is fixedly connected to the limiting block. The clamping rod 3210 is adapted to the clamping groove 324. Through the cooperation of the heat dissipation hole 321 and the dust-proof plate 323, it can prevent external dust from entering the fuselage 2 through the heat dissipation hole 321. Through the cooperation of the fourth spring 3211, the connecting rod 329, the second sliding rod 326, the second slider 327, the clamping rod 3210, and the clamping groove 324, it is convenient for manual disassembly of the dust-proof plate 323, so as to facilitate manual cleaning of the dust-proof plate 323, and further prevent the mesh holes of the dust-proof plate 323 from being blocked, affecting the heat dissipation effect of the device.

[0037] Furthermore, one end of the third spring 328 is fixedly connected to the second slider 327. Through the cooperation of the second sliding rod 326, the second slider 327, and the third spring 328, the connecting rod 329 can be kept at a position away from the dust-proof plate 323, so that the operator can free up his hands, and it is more convenient for the operator to disassemble and assemble the dust-proof plate 323.

[0038] When it is necessary to disassemble the dust-proof plate 323, first manually pull the clamping rod 3210 outwards to separate the clamping rod 3210 from the clamping groove 324. Then, under the action of the elastic force of the third spring 328, the second slider 327 can move outwards, so that the connecting rod 329 fixedly connected to the outer side of the second slider 327 can move synchronously, and the connecting rod 329 can be kept at a position away from the dust-proof plate 323, so that the operator can free up his hands. Then, the operator can manually take out the dust-proof plate 323 outwards, so as to facilitate manual cleaning of the dust-proof plate 323, and further prevent the mesh holes of the dust-proof plate 323 from being blocked, affecting the heat dissipation effect of the device.

[0039] Although the embodiments of the present invention have been shown and described, for those of ordinary skill in the art, it can be understood that various changes, modifications, substitutions, and variations can be made to these embodiments without departing from the principles and spirits of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An unmanned aerial vehicle (UAV) nest for power inspection, comprising a base (1); a fuselage (2) fixedly installed on the upper part of the base (1); an opening and closing cover plate (4) arranged on the upper part of the fuselage (2); a rain shield (5) fixedly installed on the upper part of the opening and closing cover plate (4); a conical block (6) fixedly connected to the upper part of the rain shield (5); a rain shed (7) fixedly installed on the left side of the fuselage (2); and a connection component (3) provided on one side of the fuselage (2), characterized in that: The connection assembly (3) includes a moving mechanism (31) arranged at the lower part of the fuselage (2), and a disassembly and assembly mechanism (32) is arranged on the left side of the fuselage (2).

2. The drone nest for power inspection according to claim 1, characterized in that: The moving mechanism (31) includes a hydraulic cylinder (311) fixedly installed on the inner wall of the base (1), the output end of the hydraulic cylinder (311) is fixedly connected with a connecting plate (312), the bottom of the connecting plate (312) is fixedly connected with a mounting block (313), the bottom of the mounting block (313) is rotatably connected with a support rod (314) through a pin, the bottom of the support rod (314) is provided with a mounting plate (3113), a first chute (315) is opened on the upper part of the mounting plate (3113), a first sliding rod (316) is fixedly connected to the inner wall of the first chute (315), a first slider (317) is slidably connected to the outer wall of the first sliding rod (316), a first spring (318) is fixedly connected to the inner wall of the first chute (315), a pressing groove (319) is opened on the inner wall of the first chute (315), an inner groove (3110) is opened inside the first slider (317), a pressing block (3111) is sleeved inside the inner groove (3110), a second spring (3112) is fixedly connected to the inner wall of the inner groove (3110), and a moving wheel is arranged at the bottom of the mounting plate (3113).

3. The drone nest for power inspection according to claim 1, characterized in that: The disassembly and assembly mechanism (32) includes a heat dissipation hole (321) opened on the left side of the fuselage (2), a placement groove (322) is opened outside the heat dissipation hole (321), a dust-proof plate (323) is clamped on the inner wall of the placement groove (322), a clamping groove (324) is opened on the outside of the dust-proof plate (323), a second chute (325) is opened on the left side of the fuselage (2), a second sliding rod (326) is fixedly connected to the inner wall of the second chute (325), a second slider (327) is slidably connected to the outer wall of the second sliding rod (326), a third spring (328) is fixedly connected to the inner wall of the second chute (325), a connecting rod (329) is fixedly connected to the outside of the second slider (327), one end of the connecting rod (329) is movably connected with a clamping rod (3210), a limiting block is fixedly connected to the outer end of the clamping rod (3210), and a fourth spring (3211) is fixedly connected to the outside of the connecting rod (329).

4. The drone nest for power inspection according to claim 2, wherein: The bottom end of the support rod (314) is rotatably connected to the first slider (317) through a pin, and one end of the first spring (318) is fixedly connected to the first slider (317).

5. The drone nest for power inspection according to claim 2, characterized in that: One end of the second spring (3112) is fixedly connected to the pressing block (3111), and the pressing block (3111) is arranged in a clamping connection with the pressing groove (319).

6. The drone nest for power inspection according to claim 3, characterized in that: One end of the fourth spring (3211) away from the connecting rod (329) is fixedly connected to the limit block, and the clamping rod (3210) is adapted to the clamping groove (324).

7. The drone nest for power inspection according to claim 3, characterized in that: One end of the third spring (328) is fixedly connected to the second slider (327).

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