Module controller for inspection unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicle module controllers, in particular to a module controller for routing inspection of an unmanned aerial vehicle, which comprises an unmanned aerial vehicle, and the module controller is arranged on one side of the unmanned aerial vehicle; the installation prompting mechanism is used for facilitating disassembly, assembly and maintenance of the module controller, and the installation prompting mechanism is arranged on the outer side of the module controller; wherein the installation prompting mechanism comprises a module bin fixedly installed on one side of the unmanned aerial vehicle, and the module controller is arranged in the module bin; the module controller can be conveniently taken out through the overhaul assembly, when the module controller is reinstalled, after the module controller is stably connected with the module bin, the prompt component can be automatically triggered, clear installation in-place feedback information can be provided, the risk of loosening or falling in the flight process caused by incompact connection is avoided, and meanwhile the service life of the module controller is prolonged. The protection assembly can close the module bin after the module controller is installed stably, and dust is prevented from entering the module bin.

Description

Technical Field

[0001] This utility model relates to the field of drone module controller technology, and in particular to a module controller for inspection drones. Background Technology

[0002] The widespread application of drones in fields such as power line inspection, pipeline inspection, and security monitoring has led to increasingly diversified mission functions, typically requiring the integration of multiple functional modules, such as image recognition modules, infrared thermal imaging modules, laser ranging modules, and environmental sensing modules. To achieve unified management and coordinated control of these mission modules, independent module controllers are often installed on the drone platform.

[0003] As shown in the reference case "A flight controller for unmanned aerial vehicles that is easy to disassemble and assemble" (publication number "CN213735589U"), a pull-out structural design is adopted. Since the flight controller module is pre-installed in the fixed bracket and then assembled into the fuselage housing through the fixed bracket, the installation position of the flight controller module is determined. Because the fixed bracket and the fuselage housing are detachably connected, they can slide in and out and are locked in place by a latch. This means that the flight controller module is not installed in the fuselage housing as a structural component, which is conducive to disassembly, assembly and maintenance.

[0004] Existing pull-out module controllers lack a clear locking status feedback mechanism after the module controller is connected to the fuselage, making it difficult to determine whether the module is fully connected. If the connection is not stable, the bracket may loosen or slowly slide out during the vibration generated in the drone's flight.

[0005] Therefore, a module controller for inspection drones is proposed to solve the above problems. Utility Model Content

[0006] The purpose of this utility model is to provide a module controller for inspection drones to solve the above problems. It improves the lack of a clear locking status feedback mechanism after the module controller is connected to the fuselage, which makes it difficult to determine whether the module is fully connected. If the connection is not stable, the bracket may loosen or slowly slide out during the vibration generated by the drone in flight.

[0007] This utility model achieves the above-mentioned objectives through the following technical solution: a module controller for an inspection drone, comprising: a drone, wherein a module controller is disposed on one side of the drone; a prompting installation mechanism, wherein the prompting installation mechanism is disposed on the outside of the module controller for facilitating disassembly, assembly, and maintenance of the module controller; wherein the prompting installation mechanism includes a module compartment fixedly mounted on one side of the drone, the module controller is disposed inside the module compartment, a maintenance component is disposed inside the module compartment, and a protective component is disposed on one side of the module controller. When maintenance is required, the module controller can be easily removed through the maintenance component, making maintenance operations simpler and faster. When reinstalling the module controller, once it is stably connected to the module compartment, the prompting component can be automatically triggered, providing clear installation feedback information, avoiding the risk of loosening or falling during flight due to improper connection. At the same time, the protective component can seal the module compartment after the module controller is stably installed to prevent dust from entering.

[0008] Preferably, the maintenance assembly includes a slide rail fixedly installed inside the module compartment. The module controller is slidably disposed inside the slide rail. Multiple telescopic rods are fixedly installed on one side of the slide rail. Springs are fixedly installed inside the telescopic rods. The other ends of the multiple telescopic rods are fixedly installed with the same limiting frame. The limiting frame is located outside the module controller. A warning whistle is fixedly installed on the surface of the module controller. One side of the limiting frame is in contact with the warning whistle. During use, the spring pushes the telescopic rods to extend, causing the limiting frame to fit tightly against the outside of the module controller to form a limit. When the module controller is fully slid into the preset installation position, the limiting frame contacts the warning whistle under the action of the telescopic force and exerts a squeezing force on it, thereby triggering the warning whistle to emit an audible warning, reminding the module controller that it has been installed in place.

[0009] Preferably, the limiting frame is U-shaped, and the side of the limiting frame away from the warning whistle is sloping. A buffer pad is fixedly installed on the inner side of the limiting frame. The buffer pad is located on the outer side of the module controller. When the module controller is installed, the buffer pad fits against the outer surface of the module controller and can buffer when the module controller is pushed to the final limiting position, while improving the protection performance of the module controller in the limiting state.

[0010] Preferably, a power connector is fixedly installed on one side of the drone. The power connector extends into the module compartment and contacts the module controller. When the module controller is installed, the power connector automatically contacts and connects to its electrical interface to complete the connection of power and signal paths. When the module controller is slid out for replacement or maintenance, the two separate, automatically disconnecting the electrical connection for easy operation.

[0011] Preferably, a pull plate is fixedly installed on one side of the limiting frame, and one side of the pull plate extends out of the module compartment. When maintenance is required, the limiting frame can be moved by pulling the pull plate to move the limiting frame away from the module controller, thereby releasing the limiting constraint on the module controller and facilitating its easy removal for maintenance.

[0012] Preferably, the protective component includes a cover plate fixedly installed on one side of the module compartment, a connecting seat provided at the bottom of the module controller, the module controller being fixedly connected to the connecting seat, both sides of the connecting seat being slidably connected to slide rails, and one side of the cover plate being fixedly connected to the connecting seat. By pulling the cover plate, the connecting seat and the module controller as a whole can be driven to slide out from inside the module compartment, realizing an integrated disassembly operation. After the cover plate is closed, it can seal the module compartment and effectively prevent dust from entering.

[0013] Preferably, a sealing plate is fixedly installed on one side of the cover plate, the sealing plate is in contact with the inner wall of the module compartment, and two sealing grooves are fixedly installed on the surface of the sealing plate. When the cover plate and the module compartment are closed, the sealing plate and the sealing grooves cooperate to achieve a double seal on the module compartment when the cover plate is closed, effectively preventing dust and moisture from entering and ensuring the normal use of the module controller in harsh environments.

[0014] The beneficial effects of this utility model are:

[0015] 1. The module controller can be easily removed through the maintenance component. When reinstalling the module controller, once it is stably connected to the module compartment, the prompt component can be automatically triggered to provide clear installation feedback information, avoiding the risk of loosening or falling during flight due to improper connection. At the same time, the protective component can seal the module compartment after the module controller is stably installed to prevent dust from entering.

[0016] 2. By pulling the cover, the connector and module controller can be slid out of the module compartment as a whole, realizing integrated disassembly. After the cover is closed, it can seal the module compartment and effectively prevent dust from entering. Attached Figure Description

[0017] Figure 1 This is a schematic diagram of the structure of this utility model;

[0018] Figure 2 This is a schematic diagram of the prompting and installation mechanism of this utility model;

[0019] Figure 3 This is a schematic diagram of the maintenance component structure of this utility model;

[0020] Figure 4 This is a schematic diagram of the cover plate and connecting seat structure of this utility model.

[0021] In the diagram: 1. Drone; 2. Module controller; 3. Installation prompt mechanism; 31. Module compartment; 32. Maintenance component; 321. Slide rail; 322. Telescopic rod; 323. Spring; 324. Limit frame; 325. Power connection frame; 326. Warning whistle; 327. Pull plate; 328. Buffer pad; 33. Protective component; 331. Cover plate; 332. Sealing plate; 333. Sealing groove; 334. Connecting seat. Detailed Implementation

[0022] 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.

[0023] In practical implementation: such as Figure 1-4 As shown, a module controller for an inspection drone includes: a drone 1, with a module controller 2 disposed on one side of the drone 1; and a prompting installation mechanism 3, which is disposed on the outside of the module controller 2 to facilitate disassembly, assembly, and maintenance of the module controller 2. The prompting installation mechanism 3 includes a module compartment 31 fixedly mounted on one side of the drone 1, with the module controller 2 disposed inside the module compartment 31, a maintenance component 32 disposed inside the module compartment 31, and a protective component 33 disposed on one side of the module controller 2. When maintenance is required, the module controller 2 can be easily removed through the maintenance component 32, making maintenance operations simpler and faster. When reinstalling the module controller 2, once it is stably connected to the module compartment 31, the prompting component can be automatically triggered, providing clear installation feedback information to avoid the risk of loosening or falling during flight due to improper connection. Simultaneously, the protective component 33 can seal the module compartment 31 after the module controller 2 is stably installed to prevent dust from entering.

[0024] As a platform device for performing inspection tasks, the UAV 1 typically includes basic components such as a flight control unit, a propulsion system, a mission payload unit, a power module, a module controller 2, and a structural shell. The maintenance component 32 and the protection component 33 serve as auxiliary structures of this utility model, respectively assisting in the disassembly and assembly of the module controller 2 and providing sealing protection for the operating environment. Both are located in the external structural area of ​​the module controller 2 and are independent of the core flight control system, electrical connection structure, and mission execution module of the UAV 1, and will not interfere with the control logic and mission execution performance of the equipment.

[0025] like Figure 2 and Figure 3As shown, the maintenance component 32 includes a slide rail 321 fixedly installed inside the module compartment 31. The module controller 2 is slidably disposed inside the slide rail 321. Multiple telescopic rods 322 are fixedly installed on one side of the slide rail 321. Springs 323 are fixedly installed inside the telescopic rods 322. The other end of the multiple telescopic rods 322 is fixedly installed with the same limiting frame 324. The limiting frame 324 is located outside the module controller 2. A warning whistle 326 is fixedly installed on the surface of the module controller 2. One side of the limiting frame 324 is in contact with the warning whistle 326. During use, the spring 323 pushes the telescopic rods 322 to extend, causing the limiting frame 324 to fit tightly against the outside of the module controller 2 to form a limit. When the module controller 2 is fully slid into the preset installation position, the limiting frame 324 contacts the warning whistle 326 under the action of the telescopic force. When the module controller 2 is installed, a pressure is applied to the module controller 2, triggering the whistle 326 to emit an audible alert. The limit frame 324 is U-shaped, with the side of the limit frame 324 away from the whistle 326 being beveled. A buffer pad 328 is fixedly installed on the inner side of the limit frame 324, and the buffer pad 328 is located on the outer side of the module controller 2. The U-shape of the limit frame 324 allows it to wrap around the outer structure of the module controller 2 on three sides, improving the stability of the limit. The beveled side of the limit frame 324 can move synchronously when the module controller 2 is inserted, facilitating the installation of the module controller 2. The buffer pad 328 fits against the outer surface of the module controller 2, providing cushioning when the module controller 2 is pushed to the final limit position, while also improving the protective performance of the module controller 2 in the limit state.

[0026] A power connector frame 325 is fixedly installed on one side of the UAV 1. One side of the power connector frame 325 extends into the module compartment 31 and contacts the module controller 2. When the module controller 2 is installed, the power connector frame 325 automatically contacts and connects with its electrical interface to complete the connection of power and signal paths. When the module controller 2 is slid out for replacement or maintenance, the two separate and the electrical connection is automatically disconnected. The operation is simple. A pull plate 327 is fixedly installed on one side of the limit frame 324. One side of the pull plate 327 extends out of the module compartment 31. When maintenance is required, the limit frame 324 can be moved by pulling the pull plate 327 to move the limit frame 324 away from the module controller 2, thereby releasing the limiting constraint on the module controller 2 and making it easy to pull out for maintenance.

[0027] like Figure 2 and Figure 4As shown, the protective component 33 includes a cover plate 331 fixedly installed on one side of the module compartment 31. A connecting seat 334 is provided at the bottom of the module controller 2, and the module controller 2 is fixedly connected to the connecting seat 334. Both sides of the connecting seat 334 are slidably connected to the slide rails 321. One side of the cover plate 331 is fixedly connected to the connecting seat 334. By pulling the cover plate 331, the connecting seat 334 and the module controller 2 can be driven to slide out of the module compartment 31 as a whole, achieving integrated disassembly. After the cover plate 331 is closed, it can seal the compartment. The module compartment 31 is sealed to effectively prevent dust from entering. A sealing plate 332 is fixedly installed on one side of the cover plate 331. The sealing plate 332 is in contact with the inner wall of the module compartment 31. Two sealing grooves 333 are fixedly installed on the surface of the sealing plate 332. When the cover plate 331 and the module compartment 31 are closed, the sealing plate 332 and the sealing grooves 333 cooperate to achieve a double seal on the module compartment 31 when the cover plate 331 is closed, effectively preventing dust and moisture from entering and ensuring the normal use of the module controller 2 in harsh environments.

[0028] In use, the spring 323 pushes the telescopic rod 322 to extend, causing the limiting frame 324 to fit tightly against the outer side of the module controller 2, forming a limit. When the module controller 2 is fully slid into the preset installation position, the limiting frame 324, under the action of the telescopic force, contacts the indicator whistle 326 and exerts a squeezing force on it, thereby triggering the indicator whistle 326 to emit an audible alert, reminding the module controller 2 that it has been installed in place. During the installation of the module controller 2, the buffer pad 328 fits against the outer surface of the module controller 2, which can buffer when the module controller 2 is pushed to the final limit position, and at the same time improve the protective performance of the module controller 2 in the limit state. When the module controller 2 is installed, the power connection frame 32... 5. Automatically connects to its electrical interface to complete the connection of power and signal paths. When the module controller 2 slides out for replacement or maintenance, the two separate automatically, making the electrical connection easy to operate. When maintenance is required, the limit frame 324 can be moved by pulling the pull plate 327 to move the limit frame 324 away from the module controller 2, releasing the limit constraint on the module controller 2. By pulling the cover plate 331, the connecting seat 334 and the module controller 2 can be driven to slide out of the module compartment 31. When the cover plate 331 and the module compartment 31 are closed, the cooperation of the sealing plate 332 and the sealing groove 333 achieves a double seal on the module compartment 31 when the cover plate 331 is closed, effectively preventing dust and moisture from entering.

[0029] Furthermore, it should be understood that although this specification describes embodiments, not every embodiment contains only one independent technical solution. This narrative style is merely for clarity. Those skilled in the art should consider the specification as a whole, and the technical solutions in each embodiment can also be appropriately combined to form other embodiments that can be understood by those skilled in the art.

Claims

1. A module controller for a patrol unmanned aerial vehicle, characterized in that, The utility model relates to a kind of unmanned aerial vehicle (1), one side of the unmanned aerial vehicle (1) is provided with module controller (2);Prompt installation mechanism (3) is used to facilitate the prompt installation mechanism (3) for the disassembly and repair of module controller (2) is arranged on the outside of module controller (2);Wherein, the prompt installation mechanism (3) includes module bin (31) fixedly installed on one side of unmanned aerial vehicle (1), the module controller (2) is arranged in the inside of module bin (31), repair assembly (32) is arranged in the inside of module bin (31), and protective assembly (33) is arranged on one side of module controller (2). The repair assembly (32) includes a slide rail (321) fixedly installed in the module bin (31), the module controller (2) is slidably arranged in the inside of the slide rail (321), a plurality of telescopic rods (322) are fixedly installed on one side of the slide rail (321), a spring (323) is fixedly installed in the inside of the telescopic rod (322), the same limit frame (324) is fixedly installed at the other end of the plurality of telescopic rods (322), the limit frame (324) is located on the outside of the module controller (2), a prompt whistle (326) is fixedly installed on the surface of the module controller (2), and one side of the limit frame (324) is in contact with the prompt whistle (326). The limit frame (324) is arranged in U shape, the other side of the limit frame (324) away from the prompt whistle (326) is arranged in inclined surface shape, a buffer pad (328) is fixedly installed on the inside of the limit frame (324), and the buffer pad (328) is located on the outside of the module controller (2). One side of the unmanned aerial vehicle (1) is fixedly installed with an electricity receiving frame (325), the electricity receiving frame (325) extends to the inside of the module bin (31) on one side and is in contact with one side of the module controller (2).

2. The module controller for a patrol unmanned aerial vehicle according to claim 1, wherein: One side of the limit frame (324) is fixedly installed with a pull plate (327), and the pull plate (327) extends out of the module bin (31) on one side.

3. The module controller for a patrol drone according to claim 2, wherein: The protective assembly (33) includes a cover plate (331) fixedly installed on one side of the module bin (31), a connecting seat (334) is arranged at the bottom of the module controller (2), the module controller (2) is fixedly connected with the connecting seat (334), the connecting seat (334) is slidably connected with the slide rail (321) on both sides, and one side of the cover plate (331) is fixedly connected with the connecting seat (334).

4. The module controller for a patrol drone according to claim 1, wherein: One side of the cover plate (331) is fixedly installed with a sealing plate (332), the sealing plate (332) is in contact with the inner wall of the module bin (31), and two sealing grooves (333) are fixedly installed on the surface of the sealing plate (332).

5. The module controller for a patrol drone according to claim 3, wherein: ​ 6. The module controller for a patrol drone according to claim 1, wherein: ​ 7. The module controller for a patrol drone according to claim 6, wherein: ​

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