A kind of inspection unmanned plane protection device

Abstract

The utility model discloses a kind of inspection unmanned aerial vehicle protection devices, it is related to unmanned aerial vehicle technical field.The utility model includes unmanned aerial vehicle and the two protection frames of being set above unmanned aerial vehicle, further include: quick-mounting portion, the quick-mounting portion is provided with several, several The quick-mounting portion is respectively located at the bottom of two protection frames;Anti-drop portion, the anti-drop portion is provided with several, several The anti-drop portion is respectively arranged below two protection frames;The quick-mounting portion includes connecting assembly, and the connecting assembly is arranged at the bottom of protection frame;And reset component, the reset component is provided with several, several The reset component is all located outside unmanned aerial vehicle.The utility model is set to quick-mounting portion, solved the existing protection device in use process, it is inconvenient to install protection frame on unmanned aerial vehicle, need staff to spend a lot of time to operate it, to increase the preparation time required when unmanned aerial vehicle is used, to further affect the efficiency of entire inspection operation problem.

Description

Technical Field

[0001] This utility model belongs to the field of unmanned aerial vehicle (UAV) technology, and in particular relates to a protective device for inspection UAVs. Background Technology

[0002] Inspection drones, as efficient tools in industries such as power, oil and gas, and security, have significantly improved operational efficiency and safety thanks to their flexibility, mobility, and precise detection capabilities. However, in complex environments, they often face risks such as collisions with obstacles, sudden airflow impacts, and corrosion from severe weather, which can easily lead to fuselage damage and component failures. This not only increases maintenance costs but may also interrupt inspection missions or even cause safety accidents. To extend the service life of drones and ensure operational continuity, targeted protective structures are crucial, requiring a balance between protective performance and equipment flexibility to provide reliable protection for inspection drones.

[0003] However, the existing protective devices are not convenient to install on the drone during use, requiring staff to spend a lot of time operating them, which increases the preparation time required for drone use and thus affects the efficiency of the entire inspection operation. Utility Model Content

[0004] The purpose of this utility model is to provide a protective device for inspection drones. By setting up a quick-installation part, it solves the problem that existing protective devices are inconvenient to install the protective frame on the drone during use, requiring staff to spend a lot of time operating it, thereby increasing the preparation time required for drone use and affecting the efficiency of the entire inspection operation.

[0005] To solve the above-mentioned technical problems, this utility model is achieved through the following technical solution:

[0006] This utility model is a protective device for an inspection drone, including a drone and two protective frames mounted on top of the drone. It also includes: a quick-release section, of which several quick-release sections are located at the bottom of the two protective frames; an anti-detachment section, of which several anti-detachment sections are located below the two protective frames; each quick-release section includes a connecting component located at the bottom of the protective frame; and a reset component, of which several reset components are located outside the drone. The connecting component includes a bracket fixedly connected to the bottom of the protective frame, the bracket having two sliding grooves, each with a clamping block slidably connected to its inner wall, and a rubber pad fixedly connected to the side of each clamping block that is close to each other. The two sliding grooves, the two clamping blocks, and the two rubber pads are mirror images of each other, and the reset components are respectively disposed within the two sliding grooves.

[0007] Furthermore, the anti-detachment part includes a limiting component, of which two limiting components are provided, and the two limiting components are respectively disposed on the two clamping blocks; and a buckle component, of which two buckle components are provided, and the two buckle components are disposed on the two clamping blocks; wherein, the two limiting components are arranged in a mirror image, and the two buckle components are distributed circumferentially.

[0008] Furthermore, the reset assembly includes two hinged bases disposed within the slide groove. The hinged base near the clamping block is fixedly connected to the clamping block, and the hinged base away from the clamping block is fixedly connected to the slide groove. An elastic element is disposed between the two hinged bases. The elastic element is located within the slide groove and includes two hinged blocks respectively hinged to the two hinged bases. A spring is disposed between the two hinged blocks, and the spring is fixedly connected to the two hinged blocks respectively on the side near the two hinged blocks. The cooperation of the hinged bases, hinged blocks, and spring can provide a reset elastic force after the clamping block is pulled, thereby achieving rapid fixation of the protective frame and the drone.

[0009] Furthermore, the limiting component includes a second slide groove formed within the clamping block, and two pressing members are disposed within the second slide groove. The two pressing members are mirror images of each other. Each pressing member includes a slider slidably connected to the inner wall of the second slide groove. Two springs are fixedly connected to the side of the slider away from the connecting block, and the sides of both springs away from the slider are fixedly connected to the second slide groove. The two springs are mirror images of each other. With the help of the slider and springs within the second slide groove, the snap-fit ​​assembly can be pressed and limited, enhancing the stability of the snap-fit ​​connection.

[0010] Furthermore, the buckle assembly includes connecting blocks respectively disposed in two slide grooves, each of which is fixedly connected with a buckle, and a handle is fixedly connected to the side of each connecting block away from the two buckles; wherein, both buckles are L-shaped blocks, and the side of each buckle away from the two connecting blocks is chamfered. By using the L-shaped buckles with chamfers, connecting blocks and handles, the two clamping blocks can be quickly hooked and fixed to prevent the protective frame from loosening and falling off.

[0011] This utility model has the following beneficial effects:

[0012] 1. By setting up a quick-release part, the clamping block is pulled along the slide groove, causing the spring to stretch and generate elastic force; after the clamping block is put on the drone shell, it is released, and the spring force drives the clamping block to return to its original position. The rubber pad completes the fixation, realizing the quick installation of the protective frame. The protective frame can be fixed on the drone with simple operation, without the need for staff to spend a lot of time on drone preparation, thus ensuring the overall efficiency of the inspection operation.

[0013] 2. By setting an anti-detachment part, hold the handle and insert the connecting block into the slide groove two. The buckles squeeze each other, causing the slider to compress the spring two. Continue to push the handle, and the buckles interlock. The elasticity of the spring two makes the slider lock the buckle assembly, preventing the protective frame from falling off. The two clamps can be fixed by the buckles, avoiding the protective frame from loosening and falling off the drone during drone operation, thus ensuring the stable operation of the device.

[0014] Of course, any product implementing this utility model does not necessarily need to achieve all of the advantages described above at the same time. Attached Figure Description

[0015] To more clearly illustrate the technical solutions of the embodiments of this utility model, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0016] Figure 1 This is a partial structural schematic diagram of the present invention;

[0017] Figure 2 This is a schematic diagram of the overall structure of this utility model;

[0018] Figure 3 This is a partial cross-sectional view of the connecting component of this utility model;

[0019] Figure 4 This utility model Figure 3 A magnified structural diagram of A in the middle;

[0020] Figure 5 This is a partial cross-sectional view of the limiting component of this utility model;

[0021] Figure 6 This is a schematic diagram of the overall structure of the buckle assembly of this utility model.

[0022] The attached diagram lists the components represented by each number as follows:

[0023] 101. Drone; 102. Protective frame; 2. Quick-release unit; 21. Connecting assembly; 211. Bracket; 212. Slide 1; 213. Clamping block; 214. Rubber pad; 22. Reset assembly; 221. Hinge base; 222. Hinge block; 223. Spring 1; 3. Anti-detachment part; 31. Limiting assembly; 311. Slide 2; 312. Slider; 313. Spring 2; 32. Buckle assembly; 321. Connecting block; 322. Buckle; 323. Handle. Detailed Implementation

[0024] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0025] Please see Figure 1-6 As shown, this utility model is a protective device for an inspection drone, including a drone 101 and two protective frames 102 disposed above the drone 101. It also includes: quick-release parts 2, of which a plurality of quick-release parts 2 are provided, and the plurality of quick-release parts 2 are respectively located at the bottom of the two protective frames 102; and anti-detachment parts 3, of which a plurality of anti-detachment parts 3 are provided, and the plurality of anti-detachment parts 3 are respectively disposed below the two protective frames 102.

[0026] The quick-release unit 2 includes a connecting component 21, which is located at the bottom of the protective frame 102; and a reset component 22, of which several reset components 22 are located outside the drone 101. The connecting component 21 includes a bracket 211 fixedly connected to the bottom of the protective frame 102. The bracket 211 has two sliding grooves 212, and clamping blocks 213 are slidably connected to the inner walls of the two sliding grooves 212. Rubber pads 214 are fixedly connected to the sides of the two clamping blocks 213 that are close to each other. The two sliding grooves 212, the two clamping blocks 213, and the two rubber pads 214 are mirror images of each other. Several reset components 22 are respectively disposed in the two sliding grooves 212. Each reset component 22 includes two hinged bases disposed in the sliding groove 212. 221, the hinge base 221 on the side near the clamping block 213 is fixedly connected to the clamping block 213, and the hinge base 221 on the side away from the clamping block 213 is fixedly connected to the slide groove 212. An elastic element is provided between the two hinge bases 221. The elastic element is located in the slide groove 212 and includes two hinge blocks 222 respectively hinged on the two hinge bases 221. A spring 223 is provided between the two hinge blocks 222. The spring 223 is fixedly connected to the two hinge blocks 222 on the side near the two hinge blocks 222 respectively. By setting the quick-release part 2, the protective frame 102 can be fixed on the drone 101 with simple operation, without the need for staff to spend a lot of time on the preparation of the drone 101, thus ensuring the overall efficiency of the inspection operation.

[0027] The anti-detachment part 3 includes two limiting components 31, each disposed on one of the two clamping blocks 213; and two snap-fit ​​components 32, each disposed on one of the two clamping blocks 213. The two limiting components 31 are mirror images of each other, and the two snap-fit ​​components 32 are circumferentially distributed. Each limiting component 31 includes a second sliding groove 311 formed within the clamping block 213, containing two pressing members. The two pressing members are mirror images of each other, each including a slider 312 slidably connected to the inner wall of the second sliding groove 311. Two second springs 313 are fixedly connected to the side of the slider 312 away from the connecting block 321. The side away from the slider 312 is fixedly connected to the second slide groove 311; the two second springs 313 are mirror images of each other, and the buckle assembly 32 includes connecting blocks 321 respectively disposed in the two slide grooves 311. Each connecting block 321 is fixedly connected to a buckle 322, and the side of the two connecting blocks 321 away from the two buckles 322 is fixedly connected to a handle 323; the two buckles 322 are both L-shaped blocks, and the side away from the two connecting blocks 321 is chamfered. By setting the anti-detachment part 3, the two clamping blocks 213 can be fixed by the buckles 322, which can prevent the protective frame 102 from loosening and falling off the drone 101 during the operation of the drone 101, thereby ensuring the stable operation of the device.

[0028] A specific application of this embodiment is as follows: In use, the protective frame 102 can be moved above the drone 101, where the drone 101 is a Honeycomb Aerospace HC-332, which adopts a hybrid power system and is provided with lift by three sets of six rotors coaxially mounted on the top and bottom. By changing the rotor speed, the attitude is adjusted to achieve position control. It is equipped with a fully automatic flight control system and can complete tasks such as autonomous take-off and landing and flight along a route according to preset instructions. Then, the clamping block 213 is pulled open so that it slides in the slide groove 212. At this time, under the action of several hinge bases 221 and several hinge blocks 222, the spring 223 will be stretched and generate elastic force. Then, the two clamping blocks 213 can be put on the shell of the drone 101. Then, the clamping blocks 213 are released. At this time, under the action of the elastic force of the spring 223, the two clamping blocks 213 will be driven to return to their original position, thereby putting the rubber pad 214 on the drone 101. On the outer casing, at this time, two buckle assemblies 32 can be placed, and two handles 323 can be held. Several connecting blocks 321 can be inserted into the slide groove 311. When the two opposite buckles 322 come into contact with each other, they will be squeezed against each other, thereby squeezing several sliders 312. At this time, several springs 313 will be compressed and generate elastic force. At this time, the two handles 323 can be pushed to make several buckles 322 interlock and hook each other. At this time, under the action of the elastic force of the springs 313, the sliders 312 will lock the buckle assembly 32. When it is necessary to remove the protective frame 102, the two moving handles 323 can be engaged to move one upward and the other downward. At this time, several buckles 322 will separate. Then the two buckle assemblies 32 can be pulled open to make the two clamps 213 unrestricted. Then the quick-release part 2 can be operated in reverse to remove the protective frame 102.

[0029] In the description of this specification, references to terms such as "an embodiment," "example," "specific example," etc., indicate that a specific feature, structure, material, or characteristic described in connection with that embodiment or example is included in at least one embodiment or example of the present invention. In this specification, the illustrative expressions of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials, or characteristics described may be combined in any suitable manner in one or more embodiments or examples.

[0030] The preferred embodiments of this utility model disclosed above are merely illustrative of the present utility model. These preferred embodiments do not exhaustively describe all details, nor do they limit the utility model to the specific implementations described. Clearly, many modifications and variations can be made based on the content of this specification. This specification selects and specifically describes these embodiments to better explain the principles and practical applications of this utility model, thereby enabling those skilled in the art to better understand and utilize it. This utility model is limited only by the claims and their full scope and equivalents.

Claims

1. A protective device for an inspection drone, comprising a drone (101) and two protective frames (102) disposed above the drone (101), characterized in that, Also includes: Quick-release section (2), a plurality of quick-release sections (2) are provided, and the plurality of quick-release sections (2) are respectively located at the bottom of two protective frames (102); Anti-detachment part (3), a plurality of anti-detachment parts (3) are provided, and the plurality of anti-detachment parts (3) are respectively provided below the two protective frames (102); The quick-release part (2) includes a connecting component (21), which is disposed at the bottom of the protective frame (102); as well as A reset component (22) is provided in a plurality of such components, and all such reset components (22) are located outside the UAV (101); The connecting assembly (21) includes a bracket (211) fixedly connected to the bottom of the protective frame (102). The bracket (211) has two sliding grooves (212). The inner walls of the two sliding grooves (212) are slidably connected with clamping blocks (213). The two clamping blocks (213) are fixedly connected with rubber pads (214) on the side that is close to each other. Among them, the two slides (212) are mirror images of each other, the two clamps (213) are mirror images of each other, the two rubber pads (214) are mirror images of each other, and several reset components (22) are respectively set in the two slides (212).

2. The inspection drone protection device according to claim 1, characterized in that, The anti-detachment part (3) includes a limiting component (31), and two limiting components (31) are provided, with the two limiting components (31) respectively disposed on two clamping blocks (213); and Two buckle components (32) are provided, and both buckle components (32) are provided on two clamping blocks (213); Among them, the two limiting components (31) are set in a mirror image, and the two buckle components (32) are distributed in a circle.

3. The inspection drone protection device according to claim 2, characterized in that, The reset assembly (22) includes two hinged bases (221) disposed in the first slide groove (212). The hinged base (221) on the side closer to the clamping block (213) is fixedly connected to the clamping block (213), and the hinged base (221) on the side away from the clamping block (213) is fixedly connected to the first slide groove (212). An elastic element is disposed between the two hinged bases (221). The elastic element is located in the first groove (212).

4. The inspection drone protection device according to claim 3, characterized in that, The limiting component (31) includes a second slide groove (311) opened in the clamping block (213), and two extrusion members are provided in the second slide groove (311); The two extrusion components are mirror images of each other.

5. The inspection drone protection device according to claim 4, characterized in that, The buckle assembly (32) includes connecting blocks (321) respectively disposed in two slide grooves (311), each of the two connecting blocks (321) is fixedly connected with a buckle (322), and a handle (323) is fixedly connected to the side of the two connecting blocks (321) away from the two buckles (322). Both buckles (322) are L-shaped blocks, and the side of each buckle away from the two connecting blocks (321) is chamfered.

6. The inspection drone protection device according to claim 5, characterized in that, The elastic element includes two hinge blocks (222) respectively hinged on two hinge bases (221), and a spring (223) is provided between the two hinge blocks (222). The spring (223) is fixedly connected to the two hinge blocks (222) respectively on the side close to the two hinge blocks (222).

7. A protection device for an inspection drone according to claim 6, characterized in that, The extrusion component includes a slider (312) that is slidably connected to the inner wall of the slide groove (311). Two springs (313) are fixedly connected to the side of the slider (312) away from the connecting block (321). The side of the two springs (313) away from the slider (312) is fixedly connected to the slide groove (311). Among them, the two springs (313) are mirror images of each other.

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