Miniature reconnaissance unmanned aerial vehicle

Abstract

The utility model belongs to the technical field of unmanned aerial vehicles, in particular to a miniature reconnaissance unmanned aerial vehicle, which comprises an unmanned aerial vehicle body and a camera, the bottom of the unmanned aerial vehicle body is connected with a storage box, the bottom of the unmanned aerial vehicle body is provided with a connecting plate, the connecting plate is fixedly connected with a plurality of fins, and the fins are positioned in the storage box. A first motor is arranged in the storage box, and the output end of the first motor is connected with draft fan blades. The heat dissipation efficiency of the unmanned aerial vehicle can be improved by installing the fins and the draft fan blade clamps, firstly, the connecting plates and the fins are made of high-heat-conductivity materials, the connecting plates make contact with electronic elements generating heat on the unmanned aerial vehicle body, the heat can be transmitted to the fins through the connecting plates, the heat dissipation area is increased through the fins, and the heat dissipation efficiency of the unmanned aerial vehicle is improved. And then the first motor is started to drive the draft fan blades to rotate, the draft fan blades rotate to extract air around the fins, the extracted air flows through the fins to take away heat on the fins, and therefore the unmanned aerial vehicle is rapidly cooled.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically a miniature reconnaissance UAV. Background Technology

[0002] Miniature reconnaissance drones are small, lightweight, and easy-to-carry and operate drones, typically used for covert reconnaissance and surveillance missions. They are characterized by low flight noise and small visual and auditory profiles, enabling them to gather intelligence unnoticed. Miniature reconnaissance drones are widely used in military, law enforcement, border security monitoring, special forces operations, and urban counter-terrorism missions. They can perform missions in complex urban environments and varied terrains, providing soldiers with timely and accurate intelligence.

[0003] Patent document CN210592468U discloses a reconnaissance and attack multi-rotor drone, comprising: a fuselage, multiple rotors evenly arranged on the outer surface of the fuselage, an airborne stun grenade mounted on the lower end of the fuselage, an airborne speaker mounted on the outer surface of the fuselage, a high-definition camera mounted on the right side of the outer surface of the fuselage, a through hole located in front of the high-definition camera on the right side of the outer surface of the fuselage, a micro motor installed inside the fuselage, a transmission rod mounted on the output end of the micro motor, a support rod mounted on the other end of the transmission rod, a sponge sleeve covering the outer surface of the support rod, the sponge sleeve contacting the fuselage, and a strip-shaped... A groove, the strip-shaped groove being disposed on the upper side of the through hole, with a brush installed inside the strip-shaped groove by screws. Compared with the prior art, this utility model has the following beneficial effects: "achieving convenient cleaning of dust or fog on high-definition cameras." However, the reconnaissance and broadcasting attack multi-rotor drones mentioned above mainly consider the convenient cleaning of dust or fog on high-definition cameras, without considering that the internal temperature of the drone may become too high during long-term flight. This can cause a decline in the performance of the internal electronic components of the drone, thereby affecting the flight stability and control accuracy of the drone. Therefore, it is necessary to develop a miniature reconnaissance drone that can quickly cool down the drone. Utility Model Content

[0004] The purpose of this invention is to provide a miniature reconnaissance drone to solve the technical problem mentioned in the background art that excessive internal temperature of the drone will cause a decline in the performance of the internal electronic components.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a miniature reconnaissance drone, comprising a drone body and a camera, wherein the camera is mounted on the drone body, and multiple sets of wings are fixedly mounted on the drone body, and the wings are provided with rotating blades;

[0006] A storage box is detachably connected to the bottom of the drone body. A connecting plate is detachably installed on the bottom of the drone body. Several fins are fixedly connected to the connecting plate and are located inside the storage box. A No. 1 motor is installed inside the storage box. An exhaust fan blade is fixedly connected to the output end of the No. 1 motor and is located on the outside of the fins. A sealing plate is installed on the storage box and is located on the outside of the No. 1 motor. A filter screen is fixedly installed on the sealing plate and a dustproof component is provided on the sealing plate to cover the filter screen.

[0007] Preferably, the dustproof assembly includes a carrier box, a second motor, a positive and negative lead screw, a threaded ring, an extension rod, and a dust shield. The carrier box is fixedly installed on the sealing plate and is located above the filter screen. The second motor is fixedly installed inside the carrier box. The positive and negative lead screw is fixedly installed at the output end of the second motor. The threaded ring is threadedly connected to the positive and negative lead screw, and a set of threaded rings is symmetrically arranged. The extension rod is fixedly installed on the threaded ring, and one end of the extension rod extends through the carrier box. A dust shield is fixedly installed at one end of the extension rod, and the symmetrical dust shields are located in front of the filter screen.

[0008] Preferably, the carrier box is provided with a strip groove, and one end of the extension rod passes through the strip groove and extends out of the interior of the carrier box.

[0009] Preferably, a slide rod is fixedly installed on the sealing plate, and the slide rod is located at the bottom of the filter screen. A slip ring is movably connected to the slide rod, and the slip ring is fixedly connected to the bottom end of the dust cover plate.

[0010] Preferably, a support plate is fixedly installed inside the storage box, and the No. 1 motor is fixedly installed on the support plate.

[0011] Preferably, a plurality of support legs are fixedly installed on the bottom of the drone body. The bottom end of each support leg is movably connected to a buffer base, and the bottom end of the support leg passes through the buffer base. A spring is fixedly installed inside the buffer base, and the top end of the spring is fixedly connected to the bottom end of the support leg. A damper is fixedly installed inside the buffer base, and one end of the damper passes through the interior of the spring and is fixedly connected to the bottom end of the support leg.

[0012] Compared with the prior art, the beneficial effects of this utility model are:

[0013] 1. This utility model improves the heat dissipation efficiency of drones by installing fins and exhaust fan blades. First, both the connecting plate and the fins are made of highly thermally conductive materials. The connecting plate is in contact with the electronic components on the drone body that generate heat, and the heat is transferred to the fins through the connecting plate. The fins increase the heat dissipation area. Then, the dust cover is opened to block the filter, allowing outside air to circulate in the storage box through the filter. Next, the No. 1 motor is started to drive the exhaust fan blades to rotate. The rotation of the exhaust fan blades will draw air around the fins. The drawn air will flow through the fins to carry away the heat on the fins, so that the temperature of the fins is relatively lowered, thus forming a temperature difference. This cycle repeats, thereby quickly cooling the drone and ensuring that the drone will not malfunction due to excessive heat in the electronic components during long-term flight.

[0014] 2. This utility model can reduce the impact force of a drone during landing by installing a spring. When the drone lands, it will first contact the ground through the buffer base. The impact force when the ground contacts the drone will be transmitted to the spring through the buffer base. The elasticity of the spring will absorb part of the impact energy, preventing the impact force from acting directly on the drone. At the same time, the damper will control the spring speed. The combined use of the spring and the damper can effectively reduce the damage caused by the impact force to the drone, and further improve the service life of the drone. Attached Figure Description

[0015] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0016] Figure 2 This is an exploded view of the storage box of this utility model;

[0017] Figure 3 for Figure 2 Enlarged schematic diagram of structure A in the middle;

[0018] Figure 4 for Figure 2 Enlarged schematic diagram of the B-structure;

[0019] Figure 5 This is a schematic diagram of the planar structure of the spring and damper of this utility model.

[0020] In the diagram: 1. Drone body; 2. Camera; 3. Wing; 4. Rotating blade; 5. Storage box; 6. Connecting plate; 7. Fin; 8. Motor 1; 9. Exhaust fan blade; 10. Sealing plate; 11. Filter screen; 12. Carrier box; 13. Motor 2; 14. Positive and negative lead screws; 15. Threaded ring; 16. Strip groove; 17. Extension rod; 18. Dust shield; 19. Sliding rod; 20. Slip ring; 21. Support plate; 22. Support leg; 23. Buffer base; 24. Spring; 25. Damper. Detailed Implementation

[0021] 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.

[0022] Please see Figure 1 - Figure 5 A miniature reconnaissance drone includes a drone body 1 and a camera 2. The camera 2 is mounted on the drone body 1. Multiple sets of wings 3 are fixedly mounted on the drone body 1. Rotating blades 4 are provided on the wings 3. Miniature reconnaissance drones are popular due to their small size, light weight, and portability. They are usually used to perform covert reconnaissance and surveillance missions. The drone flies by rotating blades 4. The wings 3 provide stability for the drone's flight. The camera 2 is a high-resolution surveillance device that can provide clear images and video data. However, during long-term flight, the internal temperature of the drone may become too high, which can cause the performance of the internal electronic components to degrade, thereby affecting the drone's flight stability and control accuracy.

[0023] A storage box 5 is detachably connected to the bottom of the drone body 1. A connecting plate 6 is detachably installed on the bottom of the drone body 1. Several fins 7 are fixedly connected to the connecting plate 6, and the fins 7 are located inside the storage box 5. A first motor 8 is installed inside the storage box 5. An exhaust fan blade 9 is fixedly connected to the output end of the first motor 8, and the exhaust fan blade 9 is located on the outside of the fins 7. A sealing plate 10 is installed on the storage box 5, and the sealing plate 10 is located on the outside of the first motor 8. A filter screen 11 is fixedly installed on the sealing plate 10. A dustproof component is provided on the sealing plate 10, and the dustproof component is used to cover the filter screen 11. When improving the heat dissipation efficiency of the drone, the heat dissipation efficiency of the drone can be improved by installing the fins 7 and the exhaust fan blade 9. First, the connecting plate 6 and the fins 7... All fins 7 are made of highly thermally conductive materials. The connecting plate 6 is in contact with the electronic components on the drone body 1 that generate heat. Heat is transferred to the fins 7 through the connecting plate 6. The fins 7 increase the heat dissipation area. Then, the dust cover 18 is opened to cover the filter 11, allowing outside air to circulate in the storage box 5 through the filter 11. Next, the first motor 8 is started to drive the exhaust fan blades 9 to rotate. The rotation of the exhaust fan blades 9 will draw air around the fins 7. The drawn air will flow through the fins 7 to carry away the heat on the fins 7, so that the temperature of the fins 7 is relatively reduced, thus forming a temperature difference. This cycle repeats, so as to quickly cool down the drone and ensure that the drone will not malfunction due to excessive heat of electronic components during long-term flight.

[0024] Please see Figure 2 , Figure 3 and Figure 4 The dustproof assembly includes a carrier box 12, a second motor 13, a forward and reverse lead screw 14, a threaded ring 15, an extension rod 17, and a dust shield 18. The carrier box 12 is fixedly installed on the sealing plate 10 and is located above the filter screen 11. The second motor 13 is fixedly installed inside the carrier box 12. The forward and reverse lead screw 14 is fixedly installed at the output end of the second motor 13. The threaded ring 15 is threadedly connected to the forward and reverse lead screw 14, and a set of threaded rings 15 is symmetrically arranged. The extension rod 17 is fixedly installed on the threaded ring 15, and one end of the extension rod 17 extends through the carrier box 12. A dust shield 18 is fixedly installed at one end of the extension rod 17, and the symmetrical dust shields 18 are located on the filter screen 11. In front of the filter screen 11, a slotted groove 16 is provided on the carrier box 12, and one end of the extension rod 17 passes through the slotted groove 16 and exits the interior of the carrier box 12. When it is not necessary to cool down the drone (especially when the drone is landing), the control device can start the second motor 13 to drive the positive and negative lead screws 14 to rotate. When the positive and negative lead screws 14 rotate, they will drive the extension rod 17 to move linearly in the slotted groove 16 through the threaded ring 15. When the extension rod 17 moves, it will drive the symmetrical dust cover 18 to move relative to each other. The symmetrical dust cover 18 can block the filter screen 11 by closing together, thereby preventing dust and impurities flying when the drone lands from clogging the filter screen 11.

[0025] Please see Figure 2 and Figure 4 A slide rod 19 is fixedly installed on the sealing plate 10, and the slide rod 19 is located at the bottom of the filter screen 11. A slip ring 20 is movably connected to the slide rod 19, and the slip ring 20 is fixedly connected to the bottom end of the dust cover plate 18. When the positive and negative screws 14 drive the dust cover plate 18 to move, the bottom end of the dust cover plate 18 will also slide synchronously on the slide rod 19 through the slip ring 20. The slide rod 19 and the slip ring 20 further limit the bottom end of the dust cover plate 18, providing stability for the movement of the dust cover plate 18.

[0026] Please see Figure 2 and Figure 3 A support plate 21 is fixedly installed inside the storage box 5, and the No. 1 motor 8 is fixedly installed on the support plate 21. The support plate 21 is used to support the No. 1 motor 8 so that the No. 1 motor 8 can be installed in a suitable position.

[0027] Please see Figure 1 and Figure 5Multiple support legs 22 are fixedly installed on the bottom of the drone body 1. The bottom end of the support legs 22 is movably connected to a buffer base 23, and the bottom end of the support legs 22 passes through the buffer base 23. A spring 24 is fixedly installed inside the buffer base 23, and the top end of the spring 24 is fixedly connected to the bottom end of the support leg 22. A damper 25 is fixedly installed inside the buffer base 23, and one end of the damper 25 passes through the interior of the spring 24 and is fixedly connected to the bottom end of the support leg 22. When mitigating the impact force of the drone during landing, the installation of the spring 24 can reduce the impact force of the drone during landing. When the drone lands, it will first contact the ground through the buffer base 23. The impact force when the ground contacts the drone will be transmitted to the spring 24 through the buffer base 23. The elasticity of the spring 24 will absorb part of the impact energy, preventing the impact force from acting directly on the drone. At the same time, the damper 25 will control the elastic speed of the spring 24. The combined use of the spring 24 and the damper 25 can effectively reduce the damage caused by the impact force to the drone, and further improve the service life of the drone.

[0028] The working principle is as follows: By installing fins 7 and exhaust fan blades 9, the heat dissipation efficiency of the drone can be improved. First, both the connecting plate 6 and the fins 7 are made of highly thermally conductive materials. The connecting plate 6 comes into contact with the electronic components on the drone body 1 that generate heat. Heat is transferred to the fins 7 through the connecting plate 6, increasing the heat dissipation area. Then, the dust cover 18 is opened to block the filter 11, allowing outside air to circulate in the storage box 5 through the filter 11. Next, the first motor 8 is started to drive the exhaust fan blades 9 to rotate. The rotation of the exhaust fan blades 9 draws air around the fins 7. The drawn air flows over the fins 7 to carry away the heat on the fins 7, causing the temperature of the fins 7 to decrease relatively, thus creating a temperature difference. This cycle continues. This allows for rapid cooling of the drone, ensuring it won't malfunction due to overheating of electronic components during extended flights. The spring 24 mitigates the impact force during landing. Upon landing, the drone first contacts the ground via the buffer base 23. The impact force is transmitted through the buffer base 23 to the spring 24, whose elasticity absorbs some of the impact energy, preventing direct impact on the drone. Simultaneously, the damper 25 controls the spring speed. The combined use of the spring 24 and damper 25 effectively reduces damage to the drone from impacts, further extending its lifespan.

[0029] It will be apparent to those skilled in the art that this invention is not limited to the details of the exemplary embodiments described above, and that it can be implemented in other specific forms without departing from the spirit or essential characteristics of this invention. Therefore, the embodiments should be considered illustrative and non-limiting in all respects, and the scope of this invention is defined by the appended claims rather than the foregoing description. Thus, it is intended that all variations falling within the meaning and scope of equivalents of the claims be included within this invention. No reference numerals in the claims should be construed as limiting the scope of the claims.

Claims

1. A miniature reconnaissance drone, comprising a drone body (1) and a camera (2), characterized in that: The camera (2) is mounted on the drone body (1), and multiple sets of wings (3) are fixedly mounted on the drone body (1). The wings (3) are provided with rotating blades (4). The bottom of the drone body (1) is detachably connected to a storage box (5). The bottom of the drone body (1) is detachably installed with a connecting plate (6). Several fins (7) are fixedly connected to the connecting plate (6), and the fins (7) are located inside the storage box (5). A first motor (8) is installed inside the storage box (5). An exhaust fan blade (9) is fixedly connected to the output end of the first motor (8), and the exhaust fan blade (9) is located outside the fins (7). A sealing plate (10) is installed on the storage box (5), and the sealing plate (10) is located outside the first motor (8). A filter screen (11) is fixedly installed on the sealing plate (10), and a dustproof component is provided on the sealing plate (10), and the dustproof component is used to cover the filter screen (11).

2. The miniature reconnaissance drone according to claim 1, characterized in that: The dustproof assembly includes a carrier box (12), a second motor (13), a positive and negative lead screw (14), a threaded ring (15), an extension rod (17), and a dust cover (18). The carrier box (12) is fixedly installed on the sealing plate (10) and is located above the filter screen (11). The second motor (13) is fixedly installed inside the carrier box (12). The positive and negative lead screw (14) is fixedly installed at the output end of the second motor (13). The threaded ring (15) is threadedly connected to the positive and negative lead screw (14), and a set of threaded rings (15) are symmetrically arranged. The extension rod (17) is fixedly installed on the threaded ring (15), and one end of the extension rod (17) extends through the carrier box (12). A dust cover (18) is fixedly installed at one end of the extension rod (17), and the symmetrical dust covers (18) are located in front of the filter screen (11).

3. A miniature reconnaissance drone according to claim 2, characterized in that: The carrier box (12) is provided with a strip groove (16), and one end of the extension rod (17) passes through the strip groove (16) and exits the interior of the carrier box (12).

4. A miniature reconnaissance drone according to claim 1, characterized in that: A slide rod (19) is fixedly installed on the sealing plate (10), and the slide rod (19) is located at the bottom of the filter screen (11). A slip ring (20) is movably connected to the slide rod (19), and the slip ring (20) is fixedly connected to the bottom end of the dust cover plate (18).

5. A miniature reconnaissance drone according to claim 1, characterized in that: The storage box (5) is fixedly installed with a support plate (21), and the No. 1 motor (8) is fixedly installed on the support plate (21).

6. A miniature reconnaissance drone according to claim 1, characterized in that: The bottom of the UAV body (1) is fixedly equipped with multiple support legs (22). The bottom end of the support leg (22) is movably connected to a buffer base (23), and the bottom end of the support leg (22) passes through the buffer base (23). A spring (24) is fixedly installed in the buffer base (23), and the top end of the spring (24) is fixedly connected to the bottom end of the support leg (22). A damper (25) is fixedly installed in the buffer base (23), and one end of the damper (25) passes through the interior of the spring (24) and is fixedly connected to the bottom end of the support leg (22).

Images