Unmanned aerial vehicle device for electrical equipment detection

Abstract

The utility model relates to the related technical field of electrical equipment, in particular to an unmanned aerial vehicle device for electrical equipment detection, which comprises an unmanned aerial vehicle shell and a buffer mechanism, one side of the surface of the unmanned aerial vehicle shell is connected with a fixing frame, and one side of the surface of the unmanned aerial vehicle shell is fixedly provided with a storage battery. An electricity storage mechanism is arranged on one side of the surface of the unmanned aerial vehicle shell, and a buffering mechanism is arranged on one side of the bottom of the unmanned aerial vehicle shell. According to the unmanned aerial vehicle device for power equipment detection, through arrangement of the supporting columns, the sliding grooves, the first springs, the first soft cushions, the sliding block rings, supporting legs, second soft cushions, second springs and buffer cushions, when an unmanned aerial vehicle needs to land after working, the buffer cushions make contact with the ground preferentially; and a second spring on a buffer cushion impacts to a second soft cushion under the action of force, so that supporting legs drive a sliding block ring under the action of landing force, and the sliding block ring slides to a first soft cushion to extrude a first spring, so that the unmanned aerial vehicle is buffered during landing.

Description

Technical Field

[0001] The utility model relates to the technical field related to power equipment, and in particular to an unmanned aerial vehicle device for detecting power equipment. Background Art

[0002] With the continuous development of economy and science and technology, various power systems have also been improved. In recent years, the application scope of drones in power systems has become more and more extensive, and the effective application of drones has promoted the sustainable development of the power industry. The application scope of the power system is relatively wide, so the traditional power management system gradually cannot meet the development needs of the current power industry. The application of drones solves related problems, reduces the difficulty of power construction, and solves the problem of regional inspection. Therefore, there is a special need for a drone device for power equipment detection.

[0003] However, the existing UAV devices based on power equipment detection need to take off and land multiple times during use. The landing gear is a rigid structure. The UAV makes a hard landing through the landing gear below. The lack of a buffer structure can easily cause damage to the UAV, resulting in poor reliability and shortening the life of the UAV device. In addition, a long high-altitude flight time is required, and a continuous power supply must be available to drive the motor, flight control and other equipment to complete the flight mission. The current UAV devices have a weak endurance and require multiple charges to complete the flight mission. Utility Model Content

[0004] The purpose of the utility model is to provide a UAV device for power equipment detection, so as to solve the problems raised in the above background technology that the existing UAV device based on power equipment detection needs to take off and land multiple times during use, the landing gear makes a hard landing after work, lacks a buffer structure, and is easy to cause damage to the UAV, resulting in poor reliability and shortening the life of the UAV device.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a drone device for power equipment detection, comprising a drone shell and a buffer mechanism, a fixed frame is connected to one side of the surface of the drone shell, a storage battery is fixed to one side of the surface of the drone shell, a power storage mechanism is arranged on one side of the surface of the drone shell, and a buffer mechanism is arranged on one side of the bottom of the drone shell;

[0006] The buffer mechanism includes a support column, a slide groove, a first spring, a first soft pad, a slider ring, a support leg, a second soft pad, a second spring and a buffer pad. The support column is fixedly connected to one side of the surface of the drone shell, a slide groove is provided inside the support column, a first spring is fixedly installed at one end of the slide groove, a first soft pad is fixed to one side of the surface of the first spring, a slider ring is provided at one end of the slide groove, a support leg is sleeved at one end of the slider ring, a second soft pad is provided on one side of the surface of the support leg, a second spring is fixedly installed on the surface of the second soft pad, and a buffer pad is provided on one side of the surface of the second spring.

[0007] Preferably, three groups of the slide grooves are provided, and the slide grooves and the slider ring form a sliding structure.

[0008] Preferably, three groups of the first springs are provided, and the first springs form a buffer structure through support columns and slider rings.

[0009] Preferably, the power storage mechanism comprises a fixing frame, a bracket and a solar panel, the fixing frame is fixedly connected to one side of the surface of the fixing frame, brackets are provided at both ends of the fixing frame, and the solar panel is fixedly mounted on one end of the bracket.

[0010] Preferably, the solar panels are provided in three groups, and the solar panels are electrically connected to the batteries.

[0011] Compared with the prior art, the beneficial effects of the utility model are as follows: the UAV device for detecting electric equipment, through the arrangement of the support column, the slide groove, the first spring, the first cushion, the slider ring, the support leg, the second cushion, the second spring and the buffer pad, can provide a buffering effect when the UAV needs to land, takes off and lands multiple times, and the landing gear makes a hard landing after work, which lacks a buffer structure and easily causes damage to the UAV, thereby reducing the loss problem caused by landing during use and increasing the service life of the UAV; through the arrangement of the fixed frame, the bracket and the solar panel, when the UAV needs to fly for a long time, the solar panel can absorb sunlight and then store it in the battery, thereby increasing the flight time of the UAV. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] Figure 1 This is a schematic diagram of the external appearance structure of the UAV device for detecting power equipment of the utility model;

[0013] Figure 2 This is a schematic diagram of the structure of the buffer mechanism of the utility model;

[0014] Figure 3 This is a schematic diagram of the structure of the power storage mechanism of the utility model;

[0015] Figure 4 For this utility model Figure 1 Enlarged structural diagram at A in the middle.

[0016] In the figure: 1, UAV shell; 2, fixing frame; 3, battery; 4, power storage mechanism; 401, fixing frame; 402, bracket; 403, solar panel; 5, buffer mechanism; 501, support column; 502, slide groove; 503, first spring; 504, first cushion; 505, slider ring; 506, support leg; 507, second cushion; 508, second spring; 509, cushion; DETAILED DESCRIPTION

[0017] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0018] See also Figure 1-4 The utility model provides a technical solution: a drone device for power equipment detection, comprising a drone shell 1 and a buffer mechanism 5, a fixed frame 2 is connected to one side of the surface of the drone shell 1, a storage battery 3 is fixed to one side of the surface of the drone shell 1, a power storage mechanism 4 is arranged on one side of the surface of the drone shell 1, and a buffer mechanism 5 is arranged on one side of the bottom of the drone shell 1;

[0019] The buffer mechanism 5 includes a support column 501, a slide groove 502, a first spring 503, a first cushion 504, a slider ring 505, a support leg 506, a second cushion 507, a second spring 508 and a buffer pad 509. The support column 501 is fixedly connected to one side of the surface of the drone shell 1. The slide groove 502 is provided inside the support column 501. The first spring 503 is fixedly installed at one end of the slide groove 502. The first cushion 504 is fixedly installed on one side of the surface of the first spring 503. The slider ring 505 is provided at one end of the slide groove 502. The support leg 506 is sleeved on one end of the slider ring 505. The second cushion 507 is provided on one side of the surface of the support leg 506. The second spring 507 is fixedly installed on the surface of the second cushion 507. 8. A buffer pad 509 is arranged on one side of the surface of the second spring 508. Through the arrangement of the support column 501, the slide groove 502, the first spring 503, the first soft pad 504, the slider ring 505, the support leg 506, the second soft pad 507, the second spring 508 and the buffer pad 509, when the UAV needs to land after working, the buffer pad 509 contacts the ground first, and the second spring 508 on the buffer pad 509 acts to hit the second soft pad 507, and then the support leg 506 on the second soft pad 507 is acted upon by the landing force to drive the slider ring 505, so that the slider ring 505 slides onto the first soft pad 504, thereby squeezing the first spring 503, so that the UAV is cushioned when landing.

[0020] Furthermore, three groups of slide grooves 502 are provided, and the slide grooves 502 and the slider ring 505 form a sliding structure. Through the provision of the slide grooves 502, the slider ring 505 can be easily moved at one end of the support column 501.

[0021] Furthermore, three groups of first springs 503 are provided. The first springs 503 form a buffer structure with the slider ring 505 through the support column 501 . Through the provision of the first springs 503 , the three groups of first springs 503 play a buffering role on the slider ring 505 through the first cushion 504 .

[0022] Furthermore, the power storage mechanism 4 includes a fixed frame 401, a bracket 402 and a solar panel 403. The fixed frame 401 is fixedly connected to one side of the surface of the fixed frame 2, and brackets 402 are provided at both ends of the fixed frame 401. A solar panel 403 is fixedly installed at one end of the bracket 402. Through the arrangement of the fixed frame 401, the bracket 402 and the solar panel 403, when the drone is working, the solar panel 403 installed on the bracket 402 on the fixed frame 401 can absorb sunlight, thereby extending the flight time of the drone.

[0023] Furthermore, three groups of solar panels 403 are provided, and the solar panels 403 and the battery 3 are electrically connected. Through the provision of the solar panels 403, the three groups of solar panels 403 can absorb sunlight faster and store it in the battery 3, thereby increasing the storage time.

[0024] Working principle: When the UAV is landing, the buffer pad 509 contacts the ground first, and then the second spring 508 on the buffer pad 509 exerts force to hit the second soft pad 507, and then the support leg 506 on the second soft pad 507 is acted upon by the landing force to drive the slider ring 505, so that the slider ring 505 slides onto the first soft pad 504, thereby squeezing the first spring 503 to cushion the landing of the UAV. When the UAV is flying and the power is insufficient, the solar panel 403 installed on the bracket 402 on the fixed frame 401 can absorb sunlight, so that the UAV has a longer flight time, thereby improving the flight time and the working efficiency of the UAV.

[0025] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A drone device for detecting power equipment, comprising a drone housing (1) and a buffer mechanism (5), characterized in that: A fixing frame (2) is connected to one side of the surface of the drone housing (1), a storage battery (3) is fixed to one side of the surface of the drone housing (1), a power storage mechanism (4) is provided on one side of the surface of the drone housing (1), and a buffer mechanism (5) is provided on one side of the bottom of the drone housing (1); The buffer mechanism (5) comprises a support column (501), a slide groove (502), a first spring (503), a first soft pad (504), a slider ring (505), a support leg (506), a second soft pad (507), a second spring (508) and a buffer pad (509). One side of the surface of the drone housing (1) is fixedly connected to the support column (501), a slide groove (502) is provided inside the support column (501), and one end of the slide groove (502) is fixedly installed with the first spring. A spring (503) is provided, a first soft pad (504) is fixed on one side of the surface of the first spring (503), a slider ring (505) is provided at one end of the slide groove (502), a support leg (506) is sleeved on one end of the slider ring (505), a second soft pad (507) is provided on one side of the surface of the support leg (506), a second spring (508) is fixedly installed on the surface of the second soft pad (507), and a buffer pad (509) is provided on one side of the surface of the second spring (508).

2. The UAV device for power equipment inspection according to claim 1, characterized in that: The sliding grooves (502) are provided in three groups, and the sliding grooves (502) and the slider ring (505) form a sliding structure.

3. The UAV device for power equipment inspection according to claim 1, characterized in that: The first springs (503) are provided in three groups, and the first springs (503) form a buffer structure through the support column (501) and the slider ring (505).

4. The UAV device for power equipment inspection according to claim 1, characterized in that: The power storage mechanism (4) comprises a fixing frame (401), a bracket (402) and a solar panel (403); one side of the surface of the fixing frame (2) is fixedly connected to the fixing frame (401); brackets (402) are provided at both ends of the fixing frame (401); and one end of the bracket (402) is fixedly mounted with the solar panel (403).

5. The UAV device for power equipment inspection according to claim 4, characterized in that: The solar panels (403) are provided in three groups, and the solar panels (403) are electrically connected to the battery (3).

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