Multi-mode unmanned aerial vehicle
By introducing buffer airbags and electric push rod systems into the drone, the problems of drone drop damage and unstable cameras are solved, and the protection of the drone and the stability and clarity of the cameras are improved.
Patent Information
- Application Number
- CN202510608739.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-05-13
- Publication Date
- 2025-07-22
AI Technical Summary
The drone is prone to dumping or contacting the ground when descending, causing damage, and the camera is unstable, affecting the cost of use and shooting clarity.
A multi-mode drone is designed to use the air inlet duct to expand the buffer airbag, drive the movable protective baffle to protect the body, and combine electric push rods and wiping and adsorption cotton to improve the stability and clarity of the camera.
Effectively prevent damage during drone descent, improve the installation stability of the camera and shooting clarity.
Smart Images

Figure CN120348492A_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the technical field of unmanned aerial vehicles, and specifically to a multi-mode unmanned aerial vehicle. Background Art
[0002] An unmanned aerial vehicle generally refers to an unpiloted aircraft, which is operated by a control station (remote control, computer or autopilot). Unmanned aerial vehicles can be used for various purposes, including sterile control detection, bioburden detection, etc. Please be sure to carefully check important information. An unpiloted aircraft is abbreviated as "unmanned aerial vehicle", and its English abbreviation is "UAV". It is an unpiloted aircraft that is controlled by a radio remote control device and a self-provided program control device, or is completely or intermittently autonomously operated by an on-board computer. Compared with piloted aircraft, unmanned aerial vehicles are often more suitable for tasks that are too "stupid, dirty or dangerous". Unmanned aerial vehicles can be divided into military and civilian according to the application field. In the military aspect, unmanned aerial vehicles are divided into reconnaissance aircraft and target drones. In the civilian aspect, the combination of unmanned aerial vehicles and industrial applications is the real demand for unmanned aerial vehicles; their applications in fields such as aerial photography, agriculture, plant protection, micro selfies, express delivery, disaster relief, observing wild animals, monitoring infectious diseases, mapping, news reporting, power line inspection, disaster relief, film and television shooting, creating romance, etc. have greatly expanded the uses of unmanned aerial vehicles themselves. Developed countries are also actively expanding industrial applications and developing unmanned aerial vehicle technology; When the unmanned aerial vehicle is descending, it is unable to protect the lower part of the unmanned aerial vehicle, resulting in the unmanned aerial vehicle being prone to tipping over or directly contacting the ground during the descent process, causing damage to the unmanned aerial vehicle, increasing the use cost of the unmanned aerial vehicle. At the same time, the camera is usually connected to the unmanned aerial vehicle in a snap-fit manner, making it prone to falling off due to external factors, thus reducing the stability of the camera installation. Summary of the Invention
[0003] In view of the deficiencies of the prior art, the present invention provides a multi-mode drone. By means of an air inlet pipe, external air can enter the interior of the hollow box, and part of the air inside the hollow box can enter the interior of the buffer airbag. Affected by the inflation of the air, the buffer airbag can expand. By using the expansion of the buffer airbag, the diameter of the buffer airbag can be changed. The connecting plate can drive the movable protective baffle to move together under the influence of the expansion of the buffer airbag, so that the connection between the connecting plate and the movable protective baffle can be separated from the lower surface of the fuselage. The movable protective baffle is made of plastic. When the drone descends continuously, the movable protective baffle can swing upward around the connecting plate under the influence of wind to protect the front and rear surfaces of the fuselage. The buffer airbag inside the buffer airbag can reduce the impact when the drone descends. Combined with the protection of the movable protective baffle, it can prevent damage to the drone during the descent process. When the drone is flying, the electric push rod is electrically connected to an external control terminal. Starting the electric push rod can push the limit moving frame to move up and down. When the limit moving frame moves up and down, the limit moving frame can drive the wiping adsorption cotton to move together. By using the wiping adsorption cotton, the water stains and dust on the surface of the sealed placement box can be wiped, thereby improving the clarity of the camera during shooting. By sliding the bottom plate, it can expand the bottom plate outward to adjust between the bottom plates. When the bottom plate expands, the support plate can be used to push the telescopic rod to squeeze the spring, so that the bottom plate can limit the lower surface of the camera, and the rubber seat can limit the upper surface of the camera. By using the elasticity of the spring, when it is not affected by external extrusion, the spring can drive the telescopic rod to push the support plate to move in the reverse direction, thereby clamping and fixing the camera. The fixing rod passes through the interior of the hollow rod and the telescopic rod to fix the telescopic rod. The sealed placement box can waterproof the camera and other advantages.
[0004] To solve the above technical problems, the present invention provides the following technical solutions: It includes a fuselage. Both sides of the fuselage are fitted with fitting rods. One end of the fitting rod away from the fuselage is fixedly connected to an arm. The side surface of the arm is fixedly connected to an engine box. Inside the engine box is fixedly connected an electric motor, and the output end of the electric motor is fixedly connected to a propeller. The lower surface of the fuselage is fixedly connected to a hollow box. The lower surface of the hollow box is fixedly connected to an air inlet pipe, and the air inlet pipe is communicated with the hollow box. Buffer airbags are arranged on the outer surface of the hollow box, and the buffer airbags are communicated with the hollow box. The front surface of the buffer airbag is provided with a connecting plate, and the front surface of the connecting plate is movably connected to a movable protective baffle through a hinge.
[0005] Preferably, the upper surface of the fuselage is fixedly connected to a sealed placement box. The upper surface of the sealed placement box is fitted with a cover plate. Inside the cover plate is threadedly connected a threaded rod, and the threaded rod is threadedly connected to the sealed placement box.
[0006] Preferably, an installation seat is fixedly connected to the inner bottom wall of the sealed placement box, a stepping motor is fixedly connected to the upper surface of the installation seat, and a rotating plate is fixedly connected to the output end of the stepping motor.
[0007] Preferably, a pressing plate is slidably connected to the upper surface of the rotating plate, a supporting plate is fixedly connected to the upper surface of the pressing plate, and a rubber seat is arranged on the side surface of the supporting plate.
[0008] Preferably, a hollow tube is fixedly connected to the inner wall of the sealed placement box, a spring is fixedly connected to the inside of the hollow tube, one end of the spring far away from the hollow tube is fixedly connected to a telescopic rod, and one end of the telescopic rod far away from the hollow tube is fixedly connected to the supporting plate.
[0009] Preferably, a fixing rod penetrates through the inside of the hollow tube, and one end of the fixing rod close to the hollow tube penetrates through the inside of the telescopic rod.
[0010] Preferably, a limiting moving frame is sleeved on the outer surface of the sealed placement box, a wiping and adsorbing cotton is arranged on the inner wall of the limiting moving frame and is attached to the outer surface of the sealed placement box, and first connecting metal plates are fixedly connected to both sides of the limiting moving frame.
[0011] Preferably, second connecting metal plates are fixedly connected to both sides of the cover plate, an electric push rod is arranged on the lower surface of the second connecting metal plate, and the output end of the electric push rod is fixedly connected to the first connecting metal plate.
[0012] Preferably, a processing system is installed on the main body of the machine body. The processing system includes a battery, a central processing unit, and a spread spectrum communication module. The battery is electrically connected to the central processing unit, and the central processing unit is electrically connected to the spread spectrum communication module. The spread spectrum communication module has a transceiver function, receives the signal output by the adaptation, and demodulates and decodes the signal.
[0013] Preferably, a threaded plate is fixedly connected to the front surface of the machine arm, a bolt is threadedly connected to the inside of the threaded plate, and the bolt is threadedly connected to the machine body.
[0014] Compared with the prior art, the present invention provides a multi-mode unmanned aerial vehicle, which has the following beneficial effects: 1. The present invention utilizes an air inlet pipe to allow outside air to enter the interior of the hollow box, so that part of the air inside the hollow box can enter the interior of the buffer airbag. The buffer airbag can be expanded under the influence of air filling, and the diameter of the buffer airbag can be changed by utilizing the expansion of the buffer airbag. The connection plate can drive the movable protective baffle to move together under the influence of the expansion of the buffer airbag, so that the connection between the connection plate and the movable protective baffle can be separated from the lower surface of the body. The movable protective baffle is made of plastic. When the drone continuously descends, the movable protective baffle can be swung upward with the connection plate as the center of the circle under the influence of wind to protect the front and rear surfaces of the body, and the buffer airbag in the buffer airbag can reduce the impact of the drone when it descends, and cooperate with the protection of the movable protective baffle, thereby preventing the drone from being damaged during the descent process; 2. When the drone of the present invention is in flight, the electric push rod is electrically connected to the external control end, and the electric push rod is started to push the limit moving frame to move up and down. When the limit moving frame moves up and down, the limit moving frame can drive the wiping absorption cotton to move together, and the wiping absorption cotton can be used to wipe the water stains and dust on the surface of the sealed placement box, thereby improving the clarity of the camera when shooting, and the sliding of the abutment plate can be used to expand the abutment plate outward to adjust the abutment plates. When the abutment plate expands, the support plate can be used to push the telescopic rod to squeeze the spring, so that the abutment plate can limit the lower surface of the camera, and the rubber seat can limit the upper surface of the camera, and the elasticity of the spring can be used to make it not affected by external force, so that the spring can drive the telescopic rod to push the support plate in the opposite direction to move, thereby clamping and fixing the camera, and the fixing rod is passed through the hollow rod tube and the interior of the telescopic rod to fix the telescopic rod, and the sealed placement box can be used to waterproof the camera. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Figure 1 It is a schematic diagram of the overall structure of the present invention; Figure 2 for Figure 1 Schematic diagram of the structure at A in the middle; Figure 3 This is a schematic diagram of the internal structure of the sealed placement box of the present invention; Figure 4 for Figure 3 Schematic diagram of the structure at B in the middle; Figure 5 This is a schematic diagram of the structure of the machine arm of the present invention; Figure 6 It is a schematic diagram of the structure of the machine body of the present invention when viewed from above; Figure 7 This is a schematic diagram of the structure of the limit moving frame of the present invention; Wherein: 1. Body; 2. Sealed placement box; 3. Arm; 4. Motor; 5. Propeller; 6. Machine box; 7. Bolt; 8. Mounting base; 9. Stepper motor; 10. Rotating plate; 11. First connecting metal plate; 12. Second connecting metal plate; 13. Cover plate; 14. Threaded rod; 15. Limit moving frame; 16. Electric push rod; 17. Wiping and adsorbing cotton; 18. Hollow box; 19. Air inlet pipe; 20. Buffer airbag; 21. Connecting plate; 22. Movable protection baffle; 23. Fixed rod; 24. Spring; 25. Hollow pipe; 26. Telescopic rod; 27. Rubber seat; 28. Support plate; 29. Pressing plate; 30. Fitting rod; 31. Threaded plate. Detailed implementation mode
[0016] Next, the technical solutions in the embodiments of the present invention will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
[0017] Please refer to Figure 1-7 , a multi-mode drone, including a body 1. Fitting rods 30 are fitted and connected to both sides of the body 1. One end of the fitting rod 30 away from the body 1 is fixedly connected to an arm 3. A threaded plate 31 is fixedly connected to the front surface of the arm 3. A bolt 7 is threadedly connected inside the threaded plate 31, and the bolt 7 is threadedly connected to the body 1. A machine box 6 is fixedly connected to the side surface of the arm 3. A motor 4 is fixedly connected inside the machine box 6. The output end of the motor 4 is fixedly connected to a propeller 5. Insert the fitting rod 30 into the inside of the body 1, so that the arm 3 can be installed on both sides of the body 1. Turning the bolt 7 can fix the arm 3, so that the device can be used for space flight. Pull out the fitting rod 30 from the inside of the body 1, and the arm 3 can be horizontally installed, so that the body 1 can be placed in water for use, so that the drone has two modes of use. Electrically connect the motor 4 to an external control terminal, so that starting the motor 4 can drive the propeller 5 to rotate. The rotation of the propeller 5 can provide a power source for the flight of the drone, facilitating the drone to travel in the air.
[0018] The lower surface of the body 1 is fixedly connected with a hollow box 18, the lower surface of the hollow box 18 is fixedly connected with an air inlet pipe 19, and the air inlet pipe 19 is communicated with the hollow box 18, the outer surface of the hollow box 18 is provided with a cushioning airbag 20, and the cushioning airbag 20 is communicated with the hollow box 18, the front surface of the cushioning airbag 20 is provided with a connecting plate 21, and the front surface of the connecting plate 21 is movably connected with a movable protective baffle 22 through a hinge. When the drone lands, the air inlet pipe 19 is used to allow outside air to enter the interior of the hollow box 18, so that part of the air inside the hollow box 18 can enter the interior of the cushioning airbag 20, and the cushioning airbag 20 can expand due to the influence of air filling. The expansion of the cushioning airbag 20 can change the diameter of the cushioning airbag 20. The connection plate 21 can be driven by the expansion of the cushioning airbag 20 to move together with the movable protective baffle 22, so that the connection between the connection plate 21 and the movable protective baffle 22 can be separated from the lower surface of the body 1. The movable protective baffle 22 is made of plastic. When the drone continues to descend, the movable protective baffle 22 can be affected by the wind and can swing upward with the connection plate 21 as the center to protect the front and rear surfaces of the body 1. The gas in the cushioning airbag 20 can reduce the impact of the drone when it descends, and cooperate with the protection of the movable protective baffle 22 to prevent damage to the drone during the descent.
[0019] The upper surface of the body 1 is fixedly connected with a sealed placement box 2, and the upper surface of the sealed placement box 2 is embedded with a cover plate 13, and the inner thread of the cover plate 13 is connected with a threaded rod 14, and the threaded rod 14 is threadedly connected with the sealed placement box 2, and the outer surface of the sealed placement box 2 is sleeved with a limit movement frame 15, and the inner wall of the limit movement frame 15 is provided with a wiping adsorption cotton 17, and the wiping adsorption cotton 17 is in contact with the outer surface of the sealed placement box 2, and the two sides of the limit movement frame 15 are fixedly connected with a first connection metal plate 11, and the two sides of the cover plate 13 are fixedly connected with a second connection metal plate 12, and the lower surface of the second connection metal plate 12 is provided with an electric The electric push rod 16 is driven, and the output end of the electric push rod 16 is fixedly connected to the first connecting metal plate 11, the camera is placed inside the sealed placement box 2, and the cover plate 13 can be fixed inside the sealed placement box 2 by turning the screw. When the UAV is flying, the electric push rod 16 is electrically connected to the external control end, and the electric push rod 16 is started to push the limit moving frame 15 to move up and down. When the limit moving frame 15 moves up and down, the limit moving frame 15 can drive the wiping absorption cotton 17 to move together. The wiping absorption cotton 17 can be used to wipe water stains and dust on the surface of the sealed placement box 2, thereby improving the clarity of the camera when shooting.
[0020] The inner bottom wall of the sealed placement box 2 is fixedly connected with a mounting seat 8. The upper surface of the mounting seat 8 is fixedly connected with a stepping motor 9. The output end of the stepping motor 9 is fixedly connected with a rotating plate 10. The upper surface of the rotating plate 10 is slidably connected with a pressing plate 29. The upper surface of the pressing plate 29 is fixedly connected with a support plate 28. A rubber seat 27 is arranged on the side surface of the support plate 28. The inner wall of the sealed placement box 2 is fixedly connected with a hollow tube 25. A spring 24 is fixedly connected inside the hollow tube 25. One end of the spring 24 far from the hollow tube 25 is fixedly connected with a telescopic rod 26, and the end of the telescopic rod 26 far from the hollow tube 25 is fixedly connected with the support plate 28. A fixing rod 23 penetrates through the inside of the hollow tube 25, and the end of the fixing rod 23 close to the hollow tube 25 penetrates through the inside of the telescopic rod 26. Place the camera on the surface of the rotating plate 10. By using the sliding of the pressing plate 29, it can expand the pressing plate 29 outwards to adjust between the pressing plates 29. When the pressing plate 29 expands, it can push the telescopic rod 26 by using the support plate 28 to squeeze the spring 24, so that the pressing plate 29 can limit the lower surface of the camera. The rubber seat 27 can limit the upper surface of the camera. By using the elasticity of the spring 24, when it is not affected by external extrusion, the spring 24 can drive the telescopic rod 26 to push the support plate 28 to move in the reverse direction, so as to clamp and fix the camera. The fixing rod 23 penetrates through the hollow rod tube and the inside of the telescopic rod 26 to fix the telescopic rod 26, so that the camera has a high stability during installation. Electrically connect the stepping motor 9 with an external control terminal. Starting the stepping motor 9 can drive the rotating plate 10 to rotate left and right reciprocally, so as to adjust the angle of the camera.
[0021] The body of the machine 1 is equipped with a processing system. The processing system includes a battery, a central processor and a spread spectrum communication module. The battery is electrically connected to the central processor, and the central processor is electrically connected to the spread spectrum communication module. The spread spectrum communication module has the functions of receiving and transmitting, receiving the signal output by the adaptive, and demodulating and decoding the signal.
[0022] In use, place the camera inside the sealed storage box 2. By turning the screw rod, the cover plate 13 can be fixed inside the sealed storage box 2. Expand the pressing plate 29 outwards to adjust the space between the pressing plates 29. When the pressing plate 29 expands, the support plate 28 can be used to push the telescopic rod 26 to squeeze the spring 24, so that the pressing plate 29 can limit the lower surface of the camera, and the rubber seat 27 can limit the upper surface of the camera. Using the elasticity of the spring 24, when it is not affected by external extrusion, the spring 24 can drive the telescopic rod 26 to push the support plate 28 to move in the reverse direction, thereby clamping and fixing the camera. Pass the fixing rod 23 through the hollow rod tube and the inside of the telescopic rod 26 to fix the telescopic rod 26. Start the electric push rod 16 to push the limit moving frame 15 to move up and down. When the limit moving frame 15 moves up and down, the limit moving frame 15 can drive the wiping and adsorbing cotton 17 to move together. The wiping and adsorbing cotton 17 can be used to wipe the water stains and dust on the surface of the sealed storage box 2. Start the motor 4 to drive the impeller 5 to rotate. The rotation of the impeller 5 can provide a power source for the flight of the drone, facilitating the drone to fly in the air. Use the air inlet pipe 19 to allow external air to enter the inside of the hollow box 18, so that part of the air inside the hollow box 18 can enter the inside of the buffer airbag 20. The buffer airbag 20 can expand under the influence of the air filling. The expansion of the buffer airbag 20 can change the diameter of the buffer airbag 20. The connecting plate 21 can drive the movable protective baffle 22 to move together under the influence of the expansion of the buffer airbag 20, so that the connection between the connecting plate 21 and the movable protective baffle 22 can be separated from the lower surface of the fuselage 1. The movable protective baffle 22 is made of plastic. When the drone continuously descends, the movable protective baffle 22 can swing upwards around the connecting plate 21 under the influence of the wind to protect the front and rear surfaces of the fuselage 1. The buffer airbag 20 inside the buffer airbag 20 can reduce the impact when the drone descends. Combined with the protection of the movable protective baffle 22, it can prevent damage to the drone during the descent process.
[0023] Although the embodiments of the present invention have been shown and described, for those of ordinary skill in the art, it can be understood that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. A multi-mode unmanned aerial vehicle, comprising a fuselage (1), characterized in that: On both sides of the body (1), there are fitted and connected with fitting rods (30). One end of the fitting rod (30) far from the body (1) is fixedly connected with an arm (3). On the side surface of the arm (3), there is fixedly connected with a machine box (6). Inside the machine box (6), there is fixedly connected with a motor (4). The output end of the motor (4) is fixedly connected with a propeller (5). On the lower surface of the body (1), there is fixedly connected with a hollow box (18). On the lower surface of the hollow box (18), there is fixedly connected with an air inlet pipe (19), and the air inlet pipe (19) is communicated with the hollow box (18). On the outer surface of the hollow box (18), there are provided buffer air bags (20), and the buffer air bags (20) are communicated with the hollow box (18). On the front surface of the buffer air bag (20), there is a connecting plate (21). On the front surface of the connecting plate (21), there is movably connected with a movable protection baffle (22) through a hinge.
2. The multi-mode drone according to claim 1, characterized in that: On the upper surface of the body (1), there is fixedly connected with a sealed placement box (2). On the upper surface of the sealed placement box (2), there is fitted and connected with a cover plate (13). Inside the cover plate (13), there is a threaded rod (14) in threaded connection, and the threaded rod (14) is in threaded connection with the sealed placement box (2).
3. The multimode drone according to claim 2, characterized in that: On the inner bottom wall of the sealed placement box (2), there is fixedly connected with a mounting seat (8). On the upper surface of the mounting seat (8), there is fixedly connected with a stepping motor (9). The output end of the stepping motor (9) is fixedly connected with a rotating plate (10).
4. The multi-mode drone according to claim 3, characterized in that: On the upper surface of the rotating plate (10), there is a sliding connection with a pressing plate (29). On the upper surface of the pressing plate (29), there is fixedly connected with a supporting plate (28). On the side surface of the supporting plate (28), there is a rubber seat (27).
5. The multi-mode drone according to claim 2, characterized in that: On the inner wall of the sealed placement box (2), there is fixedly connected with a hollow tube (25). Inside the hollow tube (25), there is fixedly connected with a spring (24). One end of the spring (24) far from the hollow tube (25) is fixedly connected with a telescopic rod (26), and one end of the telescopic rod (26) far from the hollow tube (25) is fixedly connected with the supporting plate (28).
6. The multimode drone according to claim 5, characterized in that: Inside the hollow tube (25), there is a fixed rod (23) passing through, and one end of the fixed rod (23) close to the hollow tube (25) passes through the inside of the telescopic rod (26).
7. A multi-mode unmanned aerial vehicle according to claim 2, wherein: On the outer surface of the sealed placement box (2), there is a limited displacement frame (15) sleeved. Inside the limited displacement frame (15), there is a wiping and adsorbing cotton (17), and the wiping and adsorbing cotton (17) is attached to the outer surface of the sealed placement box (2). On both sides of the limited displacement frame (15), there are fixedly connected with first connecting metal plates (11).
8. The multimode drone according to claim 2, wherein: On both sides of the cover plate (13), there are fixedly connected with second connecting metal plates (12). On the lower surface of the second connecting metal plate (12), there is an electric push rod (16), and the output end of the electric push rod (16) is fixedly connected with the first connecting metal plate (11).
9. A multi-mode drone according to claim 1, characterized in that: The body (1) is installed with a processing system. The processing system includes a battery, a central processor, and a spread spectrum communication module. The battery is electrically connected to the central processor, and the central processor is electrically connected to the spread spectrum communication module. The spread spectrum communication module has a transceiver function, receives the signal output by self - adaptation, and demodulates and decodes the signal.
10. A multi-mode drone according to claim 1, characterized in that: A threaded plate (31) is fixedly connected to the front surface of the arm (3). A bolt (7) is threadedly connected inside the threaded plate (31), and the bolt (7) is threadedly connected to the machine body (1).