Wind power generation line cruise unmanned aerial vehicle with landing buffer protection

Abstract

The utility model relates to the technical field of cruise unmanned aerial vehicles, and discloses a wind power generation line cruise unmanned aerial vehicle with landing buffer protection, which comprises a base, two groups of U-shaped support frames are fixedly mounted at the top of the base, and an unmanned aerial vehicle body is fixedly mounted at the top of each U-shaped support frame. A machine cover is arranged at the top of the unmanned aerial vehicle body; the buffering assembly is arranged in the U-shaped supporting frame and below the U-shaped supporting frame; the buffering assembly comprises a first buffering part and a second buffering part. By arranging the air cushion and the rubber bottom cushion, a soft and wear-resistant buffer layer is jointly formed, impact on the ground during landing of the unmanned aerial vehicle is effectively reduced, the air pump at the top of the supporting plate and the air conveying pipeline communicated with the air pump achieve rapid inflation and deflation control over the air cushion, and the safety of the unmanned aerial vehicle is improved. The unmanned aerial vehicle can adjust the hardness and buffering effect of the air cushion according to landing requirements, and the effect of improving landing buffering of the unmanned aerial vehicle is achieved.

Description

Technical Field

[0001] The utility model relates to the technical field of cruise drones, in particular to a wind power generation line cruise drone with landing buffer protection. Background Technique

[0002] Wind power generation refers to converting the kinetic energy of the wind into electrical energy, which is a clean and renewable energy source and has been increasingly valued by countries around the world. The device required for wind power generation is called a wind power generation set. Such a wind power generation set generally consists of three parts: a wind turbine, a generator, and a tower barrel. During the installation and use of wind turbine units, it is necessary to regularly inspect them, and the inspection of wind turbine units plays an important role in the maintenance of wind power. Regularly evaluating the health status of wind turbine units and real-time monitoring of the operating status of wind turbine units are indispensable links. Among them, it is particularly important to check the dust pollution on the surface of wind turbine unit equipment and whether there are cracks and peeling phenomena on the surface anti-corrosion layer.

[0003] When a wind power generation line cruise drone is performing tasks, it often needs to fly over complex terrains and harsh environmental conditions. During the landing process, if there is insufficient buffer protection, the drone is easily damaged by the impact of the ground. These damages may include fuselage rupture, propeller damage, etc., which will not only affect the service life of the drone but also may cause it to be unable to continue performing tasks. At the same time, during the landing process, if the drone is subjected to excessive impact, it may cause damage to key components such as internal sensors and batteries, thereby affecting its overall performance and stability. By providing landing buffer protection, the impact on the drone can be effectively reduced, thereby improving its stability and reliability and ensuring that the task can be successfully completed. Therefore, it is necessary to design a wind power generation line cruise drone with landing buffer protection. Content of the Utility Model

[0004] The purpose of the utility model is to provide a wind power generation line cruise drone with landing buffer protection to solve the problems raised in the above background technique.

[0005] To achieve the above purpose, the utility model provides the following technical solution: A wind power generation line cruise drone with landing buffer protection, including a base, the top of the base is fixedly installed with U-shaped support frames, and there are two groups in total. The top of the U-shaped support frames is fixedly installed with a drone body, and the top of the drone body is provided with a machine cover; a buffer component, the buffer component is arranged inside and below the U-shaped support frame; the buffer component includes: a buffer part one, the buffer part one is arranged inside and below the U-shaped support frame; a buffer part two, the buffer part two is arranged below the drone body, and the buffer part two is located on one side of the buffer part two.

[0006] Preferably, the first buffer part includes: a connecting bottom plate fixedly installed on the top of the U-shaped support frame; a connecting frame fixedly installed on the outer wall of the U-shaped support frame; an installation rod fixedly installed at the bottom of the connecting bottom plate, and a camera fixedly installed at the bottom of the installation rod, located above the connecting frame.

[0007] Preferably, a connecting installation plate is fixedly installed at the bottom of the connecting frame, and a buffer damper is fixedly installed at the bottom of the connecting installation plate, with two in a group and a total of two groups.

[0008] Preferably, a connecting column is fixedly installed at the bottom of the buffer damper, and an installation groove is opened at the bottom of the connecting column.

[0009] Preferably, a buffer spring is fixedly installed at the top of the inner wall of the installation groove, and a telescopic column is fixedly installed at the bottom of the buffer spring.

[0010] By providing an installation groove with a buffer spring and a telescopic column installed therein, the impact force can be effectively absorbed when the drone lands.

[0011] Preferably, the second buffer part includes: a support plate fixedly installed inside the connecting installation plate, located below the camera; air cushions, with a total of two groups, fixedly installed at the bottom of the base; a rubber bottom pad fixedly installed at the bottom of the air cushions, and an air pump fixedly installed at the top of the support plate.

[0012] By providing air cushions and rubber bottom pads, the buffer effect and stability are further enhanced. By providing an air pump, the air pump is connected to the air cushions through an air delivery pipeline, thereby realizing precise control of the air cushions.

[0013] Preferably, one end of the air pump is communicated with an air delivery pipeline, and the other end of the air delivery pipeline is communicated with the inside of the air cushion.

[0014] The utility model provides a wind power generation line cruise drone with landing buffer protection. It has the following beneficial effects:

[0015] (1) By providing buffer dampers, the setting of two buffer dampers in each group enhances the damping effect, enabling the drone to effectively absorb and disperse the impact force when landing. At the same time, inside the connecting column and its bottom installation groove, the combination of the buffer spring and the telescopic column further improves the buffer performance, achieving the effect of improving the landing stability and safety of the drone.

[0016] (2) The utility model is provided with an air cushion and a rubber bottom cushion, which together constitute a soft and wear-resistant buffer layer, effectively reducing the impact on the ground when the drone lands. The air pump on the top of the support plate and the connected air delivery pipeline realize the rapid inflation and deflation control of the air cushion, enabling the drone to adjust the hardness and buffering effect of the air cushion according to the landing requirements, so as to improve the landing buffering effect of the drone. Brief Description of the Drawings

[0017] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0018] Figure 2 It is a bottom view of the structure of a wind power generation line cruising drone with landing buffer protection according to the utility model;

[0019] Figure 3 It is a top view of the installation structure of a wind power generation line cruising drone with landing buffer protection according to the utility model;

[0020] Figure 4 It is a bottom view of the buffer structure of a wind power generation line cruising drone with landing buffer protection according to the utility model.

[0021] In the figure: 1 base, 2 U-shaped support frame, 3 drone body, 4 machine cover, 5 buffer assembly, 51 buffer part one, 511 connecting bottom plate, 512 mounting rod, 513 camera, 514 connecting frame, 515 connecting mounting plate, 516 buffer damper, 517 connecting column, 518 mounting groove, 519 buffer spring, 5110 telescopic column, 52 buffer part two, 521 support plate, 522 air cushion, 523 rubber bottom cushion, 524 air pump, 525 air delivery pipeline. Detailed Embodiment

[0022] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.

[0023] The examples of the embodiments are shown in the drawings, where the same or similar reference numerals represent the same or similar elements or elements with the same or similar functions from beginning to end. The embodiments described below by referring to the drawings are exemplary and are intended to explain the present utility model, and should not be construed as a limitation to the present utility model. Embodiment

[0024] A preferred embodiment of a wind power line cruising unmanned aerial vehicle with landing buffer protection provided by the present utility model is as follows Figures 1-4 As shown: A wind power line cruising unmanned aerial vehicle with landing buffer protection includes a base 1. The top of the base 1 is fixedly installed with a U-shaped support frame 2, and there are two groups in total. The top of the U-shaped support frame 2 is fixedly installed with an unmanned aerial vehicle body 3, and the top of the unmanned aerial vehicle body 3 is provided with an engine cover 4; a buffer assembly 5, and the buffer assembly 5 is arranged inside and below the U-shaped support frame 2; The buffer assembly 5 includes: a first buffer part 51, and the first buffer part 51 is arranged inside and below the U-shaped support frame 2; a second buffer part 52, and the second buffer part 52 is arranged below the unmanned aerial vehicle body 3, and the second buffer part 52 is located on one side of the second buffer part 52.

[0025] The first buffer part 51 includes: a connecting bottom plate 511, and the connecting bottom plate 511 is fixedly installed on the top of the U-shaped support frame 2; a connecting frame 514, and the connecting frame 514 is fixedly installed on the outer wall of the U-shaped support frame 2; the bottom of the connecting bottom plate 511 is fixedly installed with an installation rod 512, and the bottom of the installation rod 512 is fixedly installed with a camera 513, which is located above the connecting frame 514.

[0026] The bottom of the connecting frame 514 is fixedly installed with a connecting mounting plate 515, and the bottom of the connecting mounting plate 515 is fixedly installed with buffer dampers 516, and two are in a group, and there are two groups in total.

[0027] The bottom of the buffer damper 516 is fixedly installed with a connecting column 517, and the bottom of the connecting column 517 is provided with an installation groove 518.

[0028] The top of the inner wall of the installation groove 518 is fixedly installed with a buffer spring 519, and the bottom of the buffer spring 519 is fixedly installed with a telescopic column 5110.

[0029] By providing the installation groove 518, and the installation groove 518 is equipped with a buffer spring 519 and a telescopic column 5110, it can effectively absorb the impact force when the unmanned aerial vehicle lands.

[0030] Furthermore, in this embodiment, by providing buffer dampers 516, the setting of two buffer dampers 516 in each group enhances the shock absorption effect, enabling the unmanned aerial vehicle to effectively absorb and disperse the impact force when landing. At the same time, in the connecting column 517 and the installation groove 518 at its bottom, the combination of the buffer spring 519 and the telescopic column 5110 further improves the buffer performance, enhancing the landing stability and safety of the unmanned aerial vehicle. Embodiment

[0031] On the basis of Embodiment 1, a preferred embodiment of a wind power line cruising unmanned aerial vehicle with landing buffer protection provided by the present utility model is as follows Figures 1-4As shown: The buffer part two 52 includes: a support plate 521, which is fixedly installed inside the connection mounting plate 515 and is located below the camera 513; an air cushion 522, which is fixedly installed at the bottom of the base 1 and there are two groups in total; a rubber bottom pad 523 is fixedly installed at the bottom of the air cushion 522, and an air pump 524 is fixedly installed at the top of the support plate 521.

[0032] By providing the air cushion 522 and the rubber bottom pad 523, the buffer effect and stability are further enhanced. By providing the air pump 524, the air pump is connected to the air cushion 522 through an air delivery pipeline 525, thereby realizing precise control of the air cushion.

[0033] One end of the air pump 524 is communicatively provided with an air delivery pipeline 525, and the other end of the air delivery pipeline 525 is communicatively provided inside the air cushion 522.

[0034] Furthermore, in this embodiment, by providing the air cushion 522 and the rubber bottom pad 523, they jointly constitute a soft and wear-resistant buffer layer, effectively reducing the impact on the ground when the drone lands. The air pump 524 at the top of the support plate 521 and the air delivery pipeline 525 connected thereto realize rapid inflation and deflation control of the air cushion 522, enabling the drone to adjust the hardness and buffer effect of the air cushion according to the landing requirements.

[0035] During use, first, when the drone is about to land, the buffer damper 516 and the buffer spring 519 in the buffer part one 51 will first absorb most of the impact force, and the telescopic column 5110 will deform under the impact, further dispersing the impact force. At the same time, the air cushion 522 in the buffer part two 52 will be quickly inflated under the action of the air pump 524, forming a soft buffer layer with the ground, further reducing the vibration and impact when the drone lands. The rubber bottom pad 523 can increase the friction with the ground and prevent the drone from sliding during landing.

[0036] Finally, it should be noted that: The above are only the preferred embodiments of the present utility model and are not used to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, for those skilled in the art, they can still modify the technical solutions recorded in the foregoing embodiments, or perform equivalent replacements for some of the technical features. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present utility model shall be included within the protection scope of the present utility model.

Claims

1. A wind power line cruising drone with landing buffer protection, comprising a base (1), characterized in that: The top of the base (1) is fixedly installed with U-shaped support frames (2), and there are two groups in total. The top of the U-shaped support frames (2) is fixedly installed with a drone body (3), and a machine cover (4) is arranged on the top of the drone body (3); A buffer assembly (5), and the buffer assembly (5) is arranged inside and below the U-shaped support frame (2); The buffer assembly (5) includes: A first buffer part (51), and the first buffer part (51) is arranged inside and below the U-shaped support frame (2); A second buffer part (52), and the second buffer part (52) is arranged below the drone body (3), and the second buffer part (52) is located on one side of the second buffer part (52).

2. The wind power line cruising drone with landing buffer protection according to claim 1, wherein: The first buffer part (51) includes: A connecting bottom plate (511), and the connecting bottom plate (511) is fixedly installed on the top of the U-shaped support frame (2); A connecting frame (514), and the connecting frame (514) is fixedly installed on the outer wall of the U-shaped support frame (2); The bottom of the connecting bottom plate (511) is fixedly installed with a mounting rod (512), and the bottom of the mounting rod (512) is fixedly installed with a camera (513), which is located above the connecting frame (514).

3. The wind power line cruising drone with landing buffer protection according to claim 2, wherein: The bottom of the connecting frame (514) is fixedly installed with a connecting mounting plate (515), and the bottom of the connecting mounting plate (515) is fixedly installed with buffer dampers (516), and two of them are in a group, and there are two groups in total.

4. The wind power line cruising drone with landing buffer protection according to claim 3, wherein: The bottom of the buffer damper (516) is fixedly installed with a connecting column (517), and an installation groove (518) is opened at the bottom of the connecting column (517).

5. A wind power line cruising drone with landing buffer protection according to claim 4, characterized in that: The top of the inner wall of the installation groove (518) is fixedly installed with a buffer spring (519), and the bottom of the buffer spring (519) is fixedly installed with a telescopic column (5110).

6. The wind power line cruising drone with landing buffer protection according to claim 1, characterized in that: The second buffer part (52) includes: A support plate (521), and the support plate (521) is fixedly installed on the inner side of the connecting mounting plate (515), and is located below the camera (513); Air cushions (522), and the air cushions (522) are fixedly installed at the bottom of the base (1), and there are two groups in total; The bottom of the air cushion (522) is fixedly installed with a rubber bottom pad (523), and the top of the support plate (521) is fixedly installed with an air pump (524).

7. A wind power line cruising drone with landing buffer protection according to claim 6, characterized in that: One end of the air pump (524) is communicated with an air delivery pipeline (525), and the other end of the air delivery pipeline (525) is communicated with the inside of the air cushion (522).

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