An unmanned aerial vehicle mounting device

Abstract

The utility model discloses a kind of unmanned plane mounting device, it is related to unmanned plane accessory technical field, to solve the traditional unmanned plane mounting device in use process, installation mode is limited by wing hanging point quantity, it is difficult to meet the demand of multiple load cooperative operation in the same task, leading to the problem of insufficient unmanned plane platform task execution efficiency, including mounting assembly, parallel assembly and adapter assembly, the mounting assembly includes mounting plate, the upper connecting portion of being set in the top of mounting plate, the mounting slot of being set in the bottom of mounting plate, the wire harness channel of being set in the inside of mounting plate, the first threading slot of being set in the inside of mounting slot and being communicated with wire harness channel, the mounting rack of being set in the inside of mounting slot.The utility model is by design mounting assembly, parallel assembly and adapter assembly, not only can realize the synchronous mounting of multiple load equipment, but also can conveniently adjust the position of mounting equipment, significantly improve the flexibility and practicality of use.

Description

Technical Field

[0001] This utility model relates to the field of drone accessories technology, and more specifically, to a drone mounting device. Background Technology

[0002] Unmanned aerial vehicles (UAVs), or drones for short, are unmanned aircraft controlled by radio remote control equipment and their own program control devices, or operated autonomously, either completely or intermittently, by an onboard computer. Compared to manned aircraft, UAVs are often more suitable for tasks that are too "dull, dirty, or dangerous." UAVs can be categorized into military and civilian applications. In the military field, UAVs are divided into reconnaissance aircraft and target drones. In the civilian field, UAVs combined with industry applications represent the true necessity of UAVs. Currently, applications in aerial photography, agriculture, plant protection, miniature selfies, express delivery, disaster relief, wildlife observation, infectious disease monitoring, surveying, news reporting, power line inspection, disaster relief, film and television shooting, and creating romantic moments have greatly expanded the uses of UAVs. Developed countries are also actively expanding industry applications and developing UAV technology.

[0003] Drones can carry a variety of equipment and sensors to perform different types of tasks. In the civilian market, such as artificial rain enhancement, meteorological detection, emergency support, and fire fighting, there is a strong demand for large drones in aerial operations. Large drones need to carry various mission payloads such as meteorological catalysis equipment, atmospheric detection instruments, and communication relay pods. These are usually fixed to the wings or other hardpoints by racks. Existing ordinary racks mostly adopt a "one-to-one" installation mode, with uniform interface standards and single installation positions, resulting in insufficient payload integration compatibility and inability to meet installation requirements. Based on the above problems, we propose a drone mounting device. Utility Model Content

[0004] The purpose of this utility model is to overcome the shortcomings of the existing technology, adapt to the needs of reality, and provide a drone mounting device to solve the problem that the installation method of traditional drone mounting devices is limited by the number of wing hardpoints, making it difficult to meet the needs of multi-payload collaborative operation in the same task, resulting in insufficient task execution efficiency of the drone platform.

[0005] To solve the above-mentioned technical problems, this utility model provides the following technical solution: a drone mounting device, including a mounting assembly, a parallel assembly, and a converter assembly. The mounting assembly includes a mounting plate, an upper connecting part disposed on the top of the mounting plate, a mounting groove disposed on the bottom of the mounting plate, a wire harness channel disposed inside the mounting plate, a first wire-passing groove disposed at the top of the mounting groove and communicating with the wire harness channel, a mounting frame disposed inside the mounting groove, a wiring conduit disposed on the top of the mounting frame and extending into the first wire-passing groove, and limiting slots disposed on both sides of the mounting frame. The parallel assembly includes a parallel plate disposed between the mounting frames and a second parallel plate disposed between the parallel plates. The system includes a wire-passing groove, mounting grooves on the front and rear sides of the parallel plate, a spring in the inner cavity of the mounting groove, a limiting push plate at one end of the spring, a limiting rod at one end of the limiting push plate and connected to the limiting slot, a movable groove on one side of the top of the parallel plate, a connecting block in the inner cavity of the movable groove, and a connecting slot on the other side of the top of the parallel plate; the adapter assembly includes an adapter sleeve at the bottom of the parallel plate and communicating with the second wire-passing groove, a connecting pipe bracket at the bottom of the adapter sleeve and communicating with the adapter sleeve, a load mounting plate at the bottom of the connecting pipe bracket, and a third wire-passing groove at the bottom of the load mounting plate and communicating with the bottom of the connecting pipe bracket. When the connecting block rotates inside the movable slot, it flips from the inside of the movable slot into the connecting slot of the adjacent parallel plate, at which point the parallel plates are connected to each other.

[0006] Preferably, it also includes a drone component, the bottom of which is connected to the upper connecting part, one end of which is provided with a fixing bolt, and the bottom of which is provided with a matching fixing screw hole.

[0007] Preferably, the mount has an elliptical cross-section and a gradient transition design. Starting from the connection point between the mount and the UAV component fuselage, the mount gradually expands to its maximum cross-section at a diffusion angle of 15°.

[0008] Preferably, the height of the mounting frame gradually increases from the nose to the tail of the UAV component, and microscale eddy current generators are provided on both sides of the surface of the mounting base.

[0009] Preferably, the connecting pipe rack is arranged in a figure-eight shape, and the load mounting plates are respectively installed on both sides of the bottom of the connecting pipe rack, and the bottom surface of the load mounting plate is provided with mounting screw holes.

[0010] Compared with the prior art, the beneficial effects of this utility model are: 1. This utility model, through the design of mounting components, parallel components, and adapter components, and by setting a mounting slot at the bottom of the mounting base, and installing multiple mounting frames inside the mounting slot, combined with the flexibly adaptable parallel components and adapter components, can not only realize the synchronous mounting of multiple load-bearing devices, but also conveniently adjust the position of the mounted devices, significantly improving the flexibility and practicality of use.

[0011] 2. This utility model also incorporates a mounting component, a parallel component, and a transition component. A wire harness channel is provided inside the mounting base. A synchronous wiring conduit at the top of the mounting frame connects to the wire harness channel. The top of the parallel plate connects to the wiring conduit via a second wiring groove. The transition sleeve communicates with the second wiring groove, and the connecting pipe rack communicates with the transition sleeve. The load mounting plate communicates with the connecting pipe rack via a third wiring hole. Regardless of the mounting position of the load equipment or the simultaneous mounting of multiple devices, concealed wiring arrangement can be achieved, making the wiring design more scientific, reasonable, and convenient to operate. Attached Figure Description

[0012] Figure 1 This is a schematic diagram of the overall structure of this utility model; Figure 2 This is a schematic diagram of the mounting component structure of this utility model; Figure 3 This is a schematic diagram of the internal structure of the mount of this utility model; Figure 4 This is a schematic diagram of the mounting frame structure of this utility model; Figure 5 This is a schematic diagram of the parallel component structure of this utility model; Figure 6 This is a schematic diagram of the exploded structure of the parallel component of this utility model; Figure 7 This is a schematic diagram of the adapter component structure of this utility model.

[0013] The following are the labeling instructions in the diagram: 1. UAV component; 2. Mounting component; 201. Mounting base; 202. Upper connecting part; 203. Mounting slot; 204. Wiring harness channel; 205. First wiring slot; 206. Mounting frame; 207. Wiring conduit; 208. Limiting slot; 209. Microscale eddy current generator; 3. Parallel component; 301. Parallel plate; 302. Second wiring slot; 303. Mounting slot; 304. Spring; 305. Limiting push plate; 306. Limiting rod; 307. Movable slot; 308. Connecting block; 309. Connecting slot; 4. Adapter component; 401. Adapter sleeve; 402. Connecting tube rack; 403. Load mounting plate; 404. Third wiring slot; 405. Mounting screw hole. Detailed Implementation

[0014] The present invention will be further described below with reference to the accompanying drawings and embodiments: This utility model relates to a drone mounting device, including a mounting assembly 2, a parallel assembly 3, and a transition assembly 4. The mounting assembly 2 includes a mounting plate, an upper connecting part 202 fixedly connected to the top of the mounting plate, a mounting groove 203 formed at the bottom of the mounting plate, a wire harness channel 204 formed inside the mounting plate, a first wire-passing groove 205 formed at the top of the mounting groove 203 and connected to the wire harness channel 204, a mounting frame 206 fixedly connected inside the mounting groove 203, a wiring conduit 207 installed on the top of the mounting frame 206 and extending into the first wire-passing groove 205, and limiting slots 208 formed on both sides of the mounting frame 206. The mounting plate serves as a basic load-bearing structure, connecting the drone to the mounting unit below and providing overall support. The upper connecting part... 202 is used to fix the mounting assembly 2 to the fuselage of the UAV assembly 1. The mounting slot 203 is used to install the mounting bracket 206. The wire harness channel 204 is used to provide a channel for the wire harness from the UAV to the mounting device, avoiding the wire harness being exposed. The first wire pass-through slot 205 is used for the wire harness to pass through. The mounting bracket 206 is used to install the parallel assembly 3. The wiring conduit 207 protects the wire harness and guides it to extend downwards. The limiting slot 208 is used to connect the limiting plug 306. The parallel assembly 3 includes a parallel plate 301 that is snapped between the mounting brackets 206, a second wire pass-through slot 302 opened in the middle of the parallel plate 301, mounting slots 303 opened on the front and rear sides of the parallel plate 301, a spring 304 fixedly connected to the inner cavity of the mounting slot 303, and a spring 304 fixedly connected to the spring 304. The parallel plate 301 is used to achieve lateral connection of multiple mounting units. The second wire-passing groove 302 allows the wire harness to continue to be transmitted downwards. The mounting groove 303 is used to install a spring 304, which provides elastic fixing force so that the limit rod 306 is inserted into the limit groove 208 of the mounting frame 206 to achieve a stable connection. The movable groove 307 is used to install the connecting block 308, which is used to engage. The connecting slots 309 of adjacent parallel plates 301 form a mechanical lock; the adapter assembly 4 includes an adapter sleeve 401 fixedly connected to the bottom of the parallel plate 301 and communicating with the second wire guide slot, a connecting tube rack 402 fixedly connected to the bottom of the adapter sleeve 401 and communicating with the adapter sleeve 401, a load mounting plate 403 fixedly connected to the bottom of the connecting tube rack 402, and a third wire guide slot 404 opened at the bottom of the load mounting plate 403 and communicating with the bottom of the connecting tube rack 402. The adapter sleeve 401 is used to guide the wire harness from the parallel plate 301 to the connecting tube rack 402. The connecting tube rack 402 distributes the load and provides an installation position. The load mounting plate 403 provides an installation interface for the load device. The third wire guide slot 404 allows the wire harness to finally reach the load device.When the connecting block 308 rotates within the cavity of the movable slot 307, it flips from inside the movable slot 307 into the connecting slot 309 of the adjacent parallel plate 301. At this time, the parallel plates 301 are interconnected. This utility model, through the design of the mounting component 2, the parallel component 3, and the adapter component 4, and by providing a mounting slot 203 at the bottom of the mounting base 201, with multiple mounting brackets 206 installed inside the mounting slot 203, combined with the flexibly adaptable parallel component 3 and adapter component 4, not only can the synchronous mounting of multiple load-bearing devices be realized, but the position of the mounted devices can also be easily adjusted, significantly improving the flexibility and practicality of use; this utility model also By designing mounting component 2, parallel component 3, and adapter component 4, and by providing a wire harness channel 204 inside the mounting base 201, with a synchronous wiring conduit 207 connected to the top of the mounting frame 206, and the top of the parallel plate 301 connected to the wiring conduit 207 via a second wiring groove 302, an adapter sleeve 401 connected to the second wiring groove 302, a connecting pipe rack 402 connected to the adapter sleeve 401, and a load mounting plate 403 connected to the connecting pipe rack 402 via a third wiring hole, concealed wiring harness arrangement can be achieved regardless of the mounting position of the load equipment or the simultaneous mounting of multiple devices, making the wiring design more scientific, reasonable, and easy to operate.

[0015] Specifically, it also includes drone component 1, the bottom of drone component 1 is connected to upper connecting part 202, one end of upper connecting part 202 is provided with fixing bolt, and the bottom of drone component 1 is provided with matching fixing screw hole. Drone component 1 is used to provide flight power.

[0016] More specifically, the mount 201 has an elliptical cross-section and a gradient transition design. Starting from the connection point between the mount 201 and the fuselage of the UAV component 1, it gradually expands to the maximum cross-section with a diffusion angle of 15°. This design can reduce air resistance.

[0017] It is worth mentioning that the height of the mounting frame 206 gradually increases from the nose to the tail of the UAV component 1 to meet the spatial layout requirements of different load equipment and avoid obstructing key components. Microscale vortex generators 209 are set on both sides of the surface of the mounting base 201, which can generate tiny vortices on both sides of the surface of the mounting base 201, improve airflow distribution, and enhance flight stability.

[0018] It is worth noting that the connecting pipe rack 402 is arranged in a figure-eight shape, and the load mounting plates 403 are respectively installed on both sides of the bottom of the connecting pipe rack 402 to enhance the structural stability. The bottom surface of the load mounting plate 403 is provided with mounting screw holes 405, and the load equipment is fixed on the load mounting plate 403 through the mounting screw holes 405.

[0019] Working principle: This embodiment provides a drone mounting device. In use, firstly, the bottom of the drone component 1 is connected and fixed to the upper connecting part 202 through fixing bolts and fixing screw holes; then, the mounting units are combined according to the required number and type of load; when multiple parallel plates 301 need to be connected, the connecting block 308 is rotated in the inner cavity of the movable groove 307, so that it flips from the inside of the movable groove 307 into the connecting slot 309 of the adjacent parallel plate 301, realizing the mutual connection between the parallel plates 301; when installing the parallel plate 301, the spring 304 pushes the limiting push plate 305, so that the limiting plug 306 is inserted into the limiting slot 208, and the parallel plate 301 is firmly connected to the mounting frame 206.

[0020] After the wiring harness is led out from inside the UAV component 1, it passes through the wiring harness channel 204, the first wiring groove 205, the wiring conduit 207, the second wiring groove 302, the adapter sleeve 401, the connecting pipe rack 402 and the third wiring groove 404 in sequence, and connects to the load equipment installed on the load mounting plate 403, ensuring the orderly arrangement of the wiring harness.

[0021] The embodiments disclosed herein are preferred embodiments, but are not limited thereto. Those skilled in the art can readily grasp the spirit of this utility model based on the above embodiments and make different extensions and variations. However, as long as they do not depart from the spirit of this utility model, they are all within the protection scope of this utility model.

Claims

1. A drone mounting device, characterized in that, The system includes a mounting assembly (2), a parallel assembly (3), and a converter assembly (4). The mounting assembly (2) includes a mounting plate, an upper connecting part (202) on the top of the mounting plate, a mounting groove (203) on the bottom of the mounting plate, a wire harness channel (204) inside the mounting plate, a first wire-passing groove (205) at the top of the mounting groove (203) and connected to the wire harness channel (204), a mounting frame (206) inside the mounting groove (203), a wiring conduit (207) on the top of the mounting frame (206) and extending into the first wire-passing groove (205), and limiting slots (208) on both sides of the mounting frame (206). The parallel assembly (3) includes a parallel plate (301) between the mounting frames (206), a second wire-passing groove (302) in the middle of the parallel plate (301), and mounting slots (303) on the front and rear sides of the parallel plate (301). The spring (304) in the inner cavity of the mounting groove (303), the limiting push plate (305) at one end of the spring (304), the limiting plug (306) at one end of the limiting push plate (305) and connected in the limiting slot (208), the movable groove (307) on one side of the top of the parallel plate (301), the connecting block (308) in the inner cavity of the movable groove (307), and the connecting slot (309) on the other side of the top of the parallel plate (301); the adapter assembly (4) includes an adapter sleeve (401) at the bottom of the parallel plate (301) and connected to the second wire through slot, a connecting tube frame (402) at the bottom of the adapter sleeve (401) and connected to the adapter sleeve (401), a load mounting plate (403) at the bottom of the connecting tube frame (402), and a third wire through slot (404) at the bottom of the load mounting plate (403) and connected to the bottom of the connecting tube frame (402). When the connecting block (308) rotates in the inner cavity of the movable slot (307), it flips from the inside of the movable slot (307) into the connecting slot (309) of the adjacent parallel plate (301), at which time the parallel plates (301) are connected to each other.

2. The unmanned aerial vehicle mounting device of claim 1, wherein, It also includes a drone component (1), the bottom of the drone component (1) is connected to the upper connecting part (202), one end of the upper connecting part (202) is provided with a fixing bolt, and the bottom of the drone component (1) is provided with a matching fixing screw hole.

3. The unmanned aerial vehicle mounting device of claim 2, wherein, The mount (201) has an elliptical cross-section and a gradient transition design. The mount (201) starts from the connection point between the mount (201) and the fuselage of the UAV component (1) and gradually expands to the maximum cross-section with a diffusion angle of 15°.

4. The unmanned aerial vehicle mounting device of claim 3, wherein, The height of the mounting frame (206) gradually increases from the nose to the tail of the UAV component (1), and microscale eddy current generators (209) are provided on both sides of the surface of the mounting base (201).

5. The UAV mounting device according to claim 4, characterized in that, The connecting pipe frame (402) is arranged in a splayed shape, and load mounting plates (403) are respectively mounted at the bottom of the connecting pipe frame (402), and the bottom surface of the load mounting plate (403) is provided with mounting screw holes (405).

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