CN220616195U - AI discernment aircraft that charges - Google Patents
AI discernment aircraft that charges Download PDFInfo
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- CN220616195U CN220616195U CN202322313471.5U CN202322313471U CN220616195U CN 220616195 U CN220616195 U CN 220616195U CN 202322313471 U CN202322313471 U CN 202322313471U CN 220616195 U CN220616195 U CN 220616195U
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- 238000011897 real-time detection Methods 0.000 abstract description 3
- 230000008901 benefit Effects 0.000 description 6
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- 241000883990 Flabellum Species 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000005611 electricity Effects 0.000 description 2
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- 238000005286 illumination Methods 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
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- 241000196324 Embryophyta Species 0.000 description 1
- 241001465754 Metazoa Species 0.000 description 1
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Abstract
The utility model discloses an AI identification charging aircraft, which comprises an aircraft body, wherein two mounting plates are fixedly arranged on the bottom surface of the aircraft body, a fixing frame is fixedly arranged on the bottom surfaces of the two mounting plates, a solar panel is fixedly arranged on the top surface of the aircraft body, two lamps are fixedly arranged on the front side of the aircraft body, and two infrared range finders are fixedly arranged on the front side of the aircraft body. Through the infrared range finder and the solar panel that set up, whether the place ahead of aircraft can real-time detection have the barrier at flight in-process infrared range finder, judge through central processing unit and calculate the distance with the barrier and control the treater again and let the aircraft dodge, avoid bumping into with the barrier and lead to the organism to damage, can charge for power module through solar panel when can't return to the navigation of battery electric quantity far away from the aircraft appears, can control the aircraft and fly back when the electric quantity is enough to return to the navigation, do not need the manual work to look for, the practicality is good.
Description
Technical Field
The utility model belongs to the technical field of charged aircrafts, and particularly relates to an AI (advanced technology interface) identification charged aircrafts.
Background
Use of an aircraft in civil fields: police, urban management, agriculture, geology, weather, electric power, rescue and relief work, video shooting and other industries, and the aircraft has wide application. The aircraft is an unmanned aircraft that is maneuvered using a radio remote control device and a self-contained programmed control device, or is operated autonomously, either entirely or intermittently, by an on-board computer. Aircraft can be classified into military and civilian applications according to the field of application. For military purposes, unmanned aerial vehicles are classified into reconnaissance and drones. In civil aspects, the aircraft is currently applied to the fields of aerial photography, agriculture, plant protection, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, mapping, news reporting, electric power inspection, disaster relief and the like, the application of the unmanned aerial vehicle is greatly expanded, and the application and the development of unmanned aerial vehicle technology in developed countries are also actively expanded.
The AI intelligent recognition function has been applied to aspects such as cell-phone, car, air conditioner, refrigerator, and the like, it lets loaded down with trivial details process become simple, and aircraft + AI's combination has also promoted the aircraft trade to trend to a road that has stronger function, and current AI discernment charges aircraft inconvenient operation, need rotate AI discernment camera and observe when needing to look around surrounding environment, and flight distance is farther, the unable in time accurate judgement aircraft the place ahead of naked eye has the barrier, make the aircraft collide with the barrier and lead to the organism to damage easily, and only can pass through artifical looking for through aircraft position information when unable back voyage of battery electric quantity, the practicality is poor, based on this we propose an AI discernment charges aircraft.
Disclosure of Invention
Aiming at the defects of the prior art, the utility model aims to provide the AI identification charging aircraft, which solves the problems that the operation and observation of the existing AI identification charging aircraft are inconvenient, the distance between the AI identification charging aircraft and an obstacle cannot be accurately judged, and the AI identification charging aircraft can only be manually searched when the battery power is insufficient and the navigation cannot be carried out, and has poor practicability.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an AI discernment charging aircraft, includes the aircraft body, the bottom surface fixed mounting of aircraft body has two mounting panels, the bottom surface of two mounting panels is all fixed mounting has the mount, the top surface fixed mounting of aircraft body has solar panel, the front side fixed mounting of aircraft body has two lamps and lanterns, the front side fixed mounting of aircraft body has two infrared rangefinder, the both sides of aircraft body are all fixed mounting has four support arms, the one end of four support arms is all fixed mounting has the motor casing, the inside fixed mounting of motor casing has servo motor, the output fixed mounting of servo motor has rotary fan blade, the outside fixed mounting of motor casing has two connecting rods, the one end fixed mounting of two connecting rods has the protection frame, the inside fixed mounting of aircraft body has power module, the inside fixed mounting of aircraft body has wireless transmission module, the inside fixed mounting of aircraft body has central processing unit, the inside fixed mounting of aircraft body has control treater, the input end fixed mounting of control treater has four support arms, the output end fixed mounting of motor drive motor has four movable mounting of motor housing, the four movable mounting of motor housing has four movable mounting of wheels, the four movable mounting of motor housing has four movable mounting of axial bars, the fixed mounting of four movable mounting of motor housing has the top surface, the fixed mounting of four movable mounting of the axial bars, one side of the aircraft body is fixedly provided with a USB interface.
Preferably, the input end of the solar panel is electrically connected with the output end of the power module.
Through above-mentioned technical scheme, advantage lies in that solar panel can turn into the electric energy with solar energy, can stop it and have the place of sun for power module electricity storage when the aircraft can't return journey, alright control aircraft return journey when the electric quantity is enough, facilitate the use.
Preferably, the output end of the servo motor movably penetrates through the top end of the motor shell and extends to the bottom end of the rotary fan blade, the connecting rod is arc-shaped, and the radian of the connecting rod is the same as that of the protective frame.
Through above-mentioned technical scheme, advantage lies in can drive rotatory flabellum through servo motor and rotate and drive the aircraft body and fly, and the protection frame can protect the normal operating of rotatory flabellum, has increased the security when the aircraft operates.
Preferably, the output end of the electric push rod movably penetrates through the bottom surface of the inner cavity of the aircraft body and extends to the top surface of the resisting plate, and one end of the AI identification camera is hinged to the outer side of the shaft rod.
Through above-mentioned technical scheme, advantage lies in can drive the angle removal about AI discernment camera through electric putter drive axostylus axostyle, has increased the observation angle of aircraft.
Preferably, the input end of the AI-recognition camera is electrically connected with the input end of the central processing unit, the output end of the control processor is electrically connected with the input end of the central processing unit, the output end of the central processing unit is electrically connected with the output end of the wireless transmission module, and the input end of the central processing unit is electrically connected with the power supply module.
Through the technical scheme, the intelligent control system has the advantages that the wireless transmission module can mutually communicate with the terminal of the user through the central processing unit to transmit instructions to the control processor, and the power module provides electric quantity for normal operation of the central processing unit and the control processor, so that the intelligent control system is convenient to use.
Preferably, the bottom end of the data line is fixedly arranged at the output end of the infrared range finder, the input end of the lamp is electrically connected with the output end of the power module, and the output end of the USB interface is electrically connected with the input end of the power module.
Through above-mentioned technical scheme, the advantage lies in can be through the USB interface for power module electric power storage, and power module provides the electric quantity for lamps and lanterns for its illumination, also uses the position that the personnel made things convenient for the naked eye to observe the aircraft for the aircraft provides good field of vision, can detect the obstacle of aircraft flight in-process through the infrared range finder, avoids colliding with the obstacle and leads to the organism to damage.
Preferably, the input end of the servo motor is electrically connected with the output end of the control processor, and the input end of the electric push rod is electrically connected with the output end of the control processor.
Through above-mentioned technical scheme, the advantage lies in can come control servo motor's rotational speed through control processor, the speed and the altitude of being convenient for adjust the aircraft, and control processor also can be through the observation angle of electric putter regulation AI discernment camera, makes it more convenient when observing.
Compared with the prior art, the utility model has the beneficial effects that:
1. through the wireless transmission module that sets up, when using, use personnel to hold control terminal and receive the instruction of intercommunicating through wireless transmission module, power module provides the electric quantity for lamps and lanterns and observe for its illumination and make things convenient for use personnel's naked eye, then can control the central processing unit and circulate to the electric current size in the servo motor through control processor, control servo motor drives the rotational speed of rotatory flabellum and makes the aircraft body rise the protection frame and can protect rotatory flabellum and avoid colliding, can pass through AI discernment camera when the aircraft rises and transmit the picture that receives to protection frame rethread wireless transmission module and will transmit to the terminal and be convenient for use personnel and observe, control the electric putter through control electric putter makes its flexible adjustment that drives AI discernment camera and carry out the angle through the offset plate when needing to adjust viewing angle, the position that does not need to adjust the aircraft is observed to the person of facilitating the use personnel, whether the place ahead of infrared range finder can real-time detection aircraft is through central processing unit judgement and calculate out the distance with the obstacle, central processing unit just can avoid through control processor control aircraft when reaching dangerous distance, can not pass through control processor control aircraft when the aircraft distance through the remote battery and can't be convenient for charge back to the solar panel when can't return to the electric quantity to the high enough when the solar panel is required to charge.
2. Through the infrared range finder and the solar panel that set up, whether the place ahead that the infrared range finder can real-time detection aircraft has the obstacle to pass through data line transmission to central processing unit and judge and calculate the distance with the obstacle at flight in-process, central processing unit just can let the aircraft keep out through the rotational speed of control processor control servo motor when reaching dangerous distance, avoid bumping with the obstacle and lead to the organism to damage, if appear the aircraft apart from too far battery electric quantity can't return to the time stop the aircraft in the eminence that has the sun just can charge for power module through solar panel, can control the aircraft to fly back when the electric quantity is enough to return to the time, do not need the manual work to seek, the practicality is good.
Drawings
FIG. 1 is a schematic view of a three-dimensional appearance structure of the present utility model;
FIG. 2 is an enlarged schematic view of the structure of FIG. 1A according to the present utility model;
FIG. 3 is a schematic view of a right-side cross-sectional structure of the present utility model;
FIG. 4 is an enlarged schematic view of the structure of FIG. 3B according to the present utility model;
FIG. 5 is a schematic diagram of the front view of the present utility model;
FIG. 6 is an enlarged schematic view of the structure of FIG. 5C according to the present utility model;
fig. 7 is a schematic view of a left-hand cross-sectional structure of the present utility model.
In the figure: 1. an aircraft body; 2. a lamp; 3. a fixed block; 4. an infrared range finder; 5. AI identifies the camera; 6. a fixing frame; 7. a wireless transmission module; 8. a mounting plate; 9. a support arm; 10. a motor housing; 11. a connecting rod; 12. a protective frame; 13. rotating the fan blades; 14. a solar panel; 15. a USB interface; 16. a fixed plate; 17. an electric push rod; 18. a shaft lever; 19. a movable member; 20. a power module; 21. a central processing unit; 22. a control processor; 23. a data line; 24. a fixing plate; 25. a servo motor; 26. and (5) a retaining plate.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and fully with reference to the accompanying drawings, in which it is evident that the embodiments described are only some, but not all embodiments of the utility model. All other embodiments, which can be made by one of ordinary skill in the art without undue burden on the person of ordinary skill in the art based on the embodiments of the present utility model, are within the scope of the present utility model.
As shown in fig. 1 to 7, an AI-recognition charging aircraft comprises an aircraft body 1, wherein two mounting plates 8 are fixedly mounted on the bottom surface of the aircraft body 1, a fixing frame 6 is fixedly mounted on the bottom surfaces of the two mounting plates 8, a solar panel 14 is fixedly mounted on the top surface of the aircraft body 1, two lamps 2 are fixedly mounted on the front side of the aircraft body 1, two infrared distance meters 4 are fixedly mounted on the front side of the aircraft body 1, four supporting arms 9 are fixedly mounted on two sides of the aircraft body 1, a motor casing 10 is fixedly mounted at one end of each of the four supporting arms 9, a servo motor 25 is fixedly mounted inside the motor casing 10, a rotary fan blade 13 is fixedly mounted at the output end of the servo motor 25, two connecting rods 11 are fixedly mounted on the outer side of the motor casing 10, a protection frame 12 is fixedly mounted at one end of each of the two connecting rods 11, the power module 20 is fixedly arranged in the aircraft body 1, the wireless transmission module 7 is fixedly arranged in the aircraft body 1, the central processor 21 is fixedly arranged in the aircraft body 1, the control processor 22 is fixedly arranged in the aircraft body 1, the data line 23 is fixedly arranged at the input end of the control processor 22, the fixed plate 24 is fixedly arranged in the aircraft body 1, the electric push rod 17 is fixedly arranged on the top surface of the fixed plate 24, the bearing plate 26 is fixedly arranged at the output end of the electric push rod 17, the fixed disk 16 is fixedly arranged on the bottom surface of the aircraft body 1, the four fixed blocks 3 are fixedly arranged on the bottom surface of the fixed disk 16, the four shaft rods 18 are fixedly arranged on the opposite sides of the four fixed blocks 3, the movable pieces 19 are movably arranged on the outer sides of the four shaft rods 18, the AI identification camera 5 is fixedly arranged on the outer sides of the movable pieces 19, one side of the aircraft body 1 is fixedly provided with a USB interface 15.
The working principle of the technical scheme is as follows:
when the intelligent solar energy power supply system is used, a user holds the control terminal to receive an interaction instruction through the wireless transmission module 7, the power module 20 supplies electric quantity for the lamp 2 to illuminate and facilitates observation by naked eyes of the user, then the control processor 22 can control the central processing unit 21 to circulate to the current in the servo motor 25, the servo motor 25 is controlled to drive the rotating speed of the rotating fan blade 13 to enable the aircraft body 1 to lift the protection frame 12 to protect the rotating fan blade 13 from collision, when the aircraft is lifted, the received picture can be transmitted to the protection frame 12 through the AI identification camera 5 and then transmitted to the terminal through the wireless transmission module 7 to facilitate observation by the user, when the observation angle needs to be adjusted, the control processor 22 controls the electric push rod 17 to enable the electric push rod 17 to stretch out and draw back to drive the AI identification camera 5 to adjust the angle through the control panel 26, the position of the user does not need to be adjusted when the aircraft is required to observe, the infrared range finder 4 can detect whether an obstacle is in front of the aircraft in real time, the distance between the central processing unit 21 and the obstacle is calculated through the central processing unit 21, when the dangerous distance between the aircraft is reached, the central processing unit 21 can conveniently pass through the control processor 22 to transmit the received picture to the protection frame 12 and the obstacle, when the dangerous distance is reached, the solar energy power supply system can not be recovered to the solar energy power supply system can not be charged by the user when the solar energy power supply system can return to the solar energy power supply system can not charge the solar energy power supply system through the practical solar energy power supply system when the aircraft can return to the practical power supply system when the aircraft can return the aircraft to the actual power supply has the actual power.
In another embodiment, as shown in fig. 1-7, the input of the solar panel 14 is electrically connected to the output of the power module 20.
The solar panel 14 can convert solar energy into electric energy, and can stop the aircraft at a place with the sun for the power module 20 to store electricity when the aircraft cannot return, and the aircraft can be controlled to return when the electric quantity is enough, so that the aircraft is convenient to use.
In another embodiment, as shown in fig. 1-7, the output end of the servo motor 25 movably penetrates the top end of the motor housing 10 and extends to the bottom end of the rotary fan blade 13, the connecting rod 11 is arc-shaped, and the arc of the connecting rod 11 is the same as that of the protecting frame 12.
The rotating fan blades 13 can be driven by the servo motor 25 to rotate so as to drive the aircraft body 1 to fly, and the protective frame 12 can protect the normal operation of the rotating fan blades 13, so that the safety of the aircraft during operation is improved.
In another embodiment, as shown in fig. 1-7, the output end of the electric push rod 17 movably penetrates the bottom surface of the inner cavity of the aircraft body 1 and extends to the top surface of the retaining plate 26, and one end of the AI identification camera 5 is hinged to the outer side of the shaft 18.
The electric push rod 17 can drive the shaft rod 18 to drive the AI recognition camera 5 to move up and down in an angle, so that the observation angle of the aircraft is increased.
In another embodiment, as shown in fig. 1-7, the input end of the AI-recognition camera 5 is electrically connected to the input end of the central processor 21, the output end of the control processor 22 is electrically connected to the input end of the central processor 21, the output end of the central processor 21 is electrically connected to the output end of the wireless transmission module 7, and the input end of the central processor 21 is electrically connected to the power module 20.
The wireless transmission module 7 can mutually communicate with the terminal of the user to transmit instructions to the control processor 22 through the central processing unit 21, and the power module 20 provides electric quantity for the normal operation of the central processing unit 21 and the control processor 22, so that the wireless transmission system is convenient to use.
In another embodiment, as shown in fig. 1-7, the bottom end of the data line 23 is fixedly mounted at the output end of the infrared range finder 4, the input end of the lamp 2 is electrically connected with the output end of the power module 20, and the output end of the USB interface 15 is electrically connected with the input end of the power module 20.
The power module 20 can be charged through the USB interface 15, the power module 20 provides electric quantity for the lamp 2 to illuminate, a good visual field is provided for the aircraft, a person can observe the position of the aircraft conveniently and naked eyes, the infrared range finder 4 can detect obstacles in the flight process of the aircraft, and the damage to the aircraft caused by collision with the obstacles is avoided.
In another embodiment, as shown in fig. 1-7, the input end of the servo motor 25 is electrically connected to the output end of the control processor 22, and the input end of the electric putter 17 is electrically connected to the output end of the control processor 22.
The rotating speed of the servo motor 25 can be controlled through the control processor 22, so that the flying speed and the flying height of the aircraft can be conveniently adjusted, and the control processor 22 can also adjust the observation angle of the AI recognition camera 5 through the electric push rod 17, so that the observation is more convenient.
The working principle and the using flow of the utility model are as follows: when in use, a user holds the control terminal to receive an interaction instruction through the wireless transmission module 7, the power module 20 supplies electric quantity to the lamp 2 to illuminate the lamp and facilitate observation by naked eyes of the user, then the control processor 22 can control the current flowing into the servo motor 25 from the central processor 21, the servo motor 25 is controlled to drive the rotating speed of the rotating fan blade 13 to enable the aircraft body 1 to lift the protective frame 12 to protect the rotating fan blade 13 from collision, when the aircraft is lifted, the received picture can be transmitted to the protective frame 12 through the AI identification camera 5 and then transmitted to the terminal through the wireless transmission module 7 to facilitate observation by the user, when the observation angle is required to be adjusted, the control processor 22 controls the electric push rod 17 to stretch to drive the AI identification camera 5 through the retaining plate 26 to adjust the angle, the position of the aircraft is not required to be adjusted for the observation by the user, in the flying process, the infrared range finder 4 can detect whether an obstacle exists in front of the aircraft in real time, judges and calculates the distance from the obstacle through the central processor 21, when the dangerous distance is reached, the central processor 21 can control the aircraft to evade through the control processor 22, if the aircraft is far away from the dangerous distance and the battery power can not return, the aircraft can be stopped at the high place with the sun and can charge the power module 20 through the solar panel 14, when the power is enough to return, the aircraft can be controlled to fly back without manual searching, the practicability is good, and through the infrared range finder 4 and the solar panel 14, in the flying process, the infrared range finder 4 can detect whether the obstacle exists in front of the aircraft in real time, transmits data to the central processor 21 through the data line 23, judges and calculates the distance from the obstacle, when the dangerous distance is reached, the central processing unit 21 can control the rotating speed of the servo motor 25 through the control processor 22 to enable the aircraft to evade, the aircraft is prevented from being damaged due to collision with obstacles, if the aircraft is far away from the dangerous distance and the battery power cannot return, the aircraft is stopped at a place with the sun, the solar panel 14 can charge the power module 20, the aircraft can be controlled to fly back when the power is enough to return, the aircraft does not need to be found manually, and the practicability is good.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. AI discernment aircraft that charges, including aircraft body (1), its characterized in that: the utility model discloses a wireless aircraft, including aircraft body (1), motor casing (10) are all fixed mounting in the bottom surface of aircraft body (1), bottom surface of two mounting plates (8) is all fixed mounting has mount (6), the top surface fixed mounting of aircraft body (1) has solar panel (14), the front side fixed mounting of aircraft body (1) has two lamps and lanterns (2), the front side fixed mounting of aircraft body (1) has two infrared range finder (4), the both sides of aircraft body (1) are all fixed mounting has four support arms (9), the one end of four support arms (9) is all fixed mounting has motor casing (10), the inside fixed mounting of motor casing (10) has servo motor (25), the output fixed mounting of servo motor (25) has rotary fan blade (13), the outside fixed mounting of motor casing (10) has two connecting rods (11), the one end fixed mounting of two connecting rods (11) has protection frame (12), the inside fixed mounting of aircraft body (1) has power module (20), the inside fixed mounting of aircraft body (1) has motor casing (1), inside fixed mounting has central processing unit (22), the intelligent control system comprises an aircraft body (1), wherein a control processor (22) is fixedly arranged at the input end of the control processor, a data wire (23) is fixedly arranged in the aircraft body (1), a fixed plate (24) is fixedly arranged in the aircraft body, an electric push rod (17) is fixedly arranged on the top surface of the fixed plate (24), a retaining plate (26) is fixedly arranged at the output end of the electric push rod (17), a fixed disc (16) is fixedly arranged on the bottom surface of the aircraft body (1), four fixed blocks (3) are fixedly arranged on the bottom surface of the fixed disc (16), four shaft rods (18) are fixedly arranged on opposite sides of the four fixed blocks (3), a movable piece (19) is movably arranged on the outer side of the four shaft rods (18), an AI identification camera (5) is fixedly arranged on the outer side of the movable piece (19), and a USB interface (15) is fixedly arranged on one side of the aircraft body (1).
2. The AI-identifying charged aircraft of claim 1, wherein: the input end of the solar panel (14) is electrically connected with the output end of the power module (20).
3. The AI-identifying charged aircraft of claim 1, wherein: the output end of the servo motor (25) movably penetrates through the top end of the motor casing (10) and extends to the bottom end of the rotary fan blade (13), the connecting rod (11) is arc-shaped, and the radian of the connecting rod (11) is the same as that of the protecting frame (12).
4. The AI-identifying charged aircraft of claim 1, wherein: the output end of the electric push rod (17) movably penetrates through the bottom surface of the inner cavity of the aircraft body (1) and extends to the top surface of the resisting plate (26), and one end of the AI identification camera (5) is hinged to the outer side of the shaft rod (18).
5. The AI-identifying charged aircraft of claim 1, wherein: the input end of the AI identification camera (5) is electrically connected with the input end of the central processing unit (21), the output end of the control processor (22) is electrically connected with the input end of the central processing unit (21), the output end of the central processing unit (21) is electrically connected with the output end of the wireless transmission module (7), and the input end of the central processing unit (21) is electrically connected with the power module (20).
6. The AI-identifying charged aircraft of claim 1, wherein: the bottom end of the data line (23) is fixedly arranged at the output end of the infrared range finder (4), the input end of the lamp (2) is electrically connected with the output end of the power module (20), and the output end of the USB interface (15) is electrically connected with the input end of the power module (20).
7. The AI-identifying charged aircraft of claim 1, wherein: the input end of the servo motor (25) is electrically connected with the output end of the control processor (22), and the input end of the electric push rod (17) is electrically connected with the output end of the control processor (22).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322313471.5U CN220616195U (en) | 2023-08-28 | 2023-08-28 | AI discernment aircraft that charges |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322313471.5U CN220616195U (en) | 2023-08-28 | 2023-08-28 | AI discernment aircraft that charges |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220616195U true CN220616195U (en) | 2024-03-19 |
Family
ID=90234736
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322313471.5U Active CN220616195U (en) | 2023-08-28 | 2023-08-28 | AI discernment aircraft that charges |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220616195U (en) |
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2023
- 2023-08-28 CN CN202322313471.5U patent/CN220616195U/en active Active
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