CN215851972U - AI unmanned aerial vehicle test platform - Google Patents
AI unmanned aerial vehicle test platform Download PDFInfo
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- CN215851972U CN215851972U CN202122551909.4U CN202122551909U CN215851972U CN 215851972 U CN215851972 U CN 215851972U CN 202122551909 U CN202122551909 U CN 202122551909U CN 215851972 U CN215851972 U CN 215851972U
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Abstract
The utility model discloses an AI unmanned aerial vehicle test platform, which comprises a test box and a buffer structure, wherein the buffer structure is arranged at the lower end of the test box, an opening is arranged at the upper end of the test box in a penetrating manner, electric push rods are arranged around the upper end of the test box, a protective cover is arranged at the upper end of each electric push rod, a monitoring device is arranged on the right side of the lower end of each protective cover, an air supply box is arranged on the right side of the test box in a penetrating manner, a second motor is arranged at the front end inside the air supply box, a motor shaft extends from one end of the second motor, a rotating frame is arranged at one end of the motor shaft, first motors are arranged on two sides of the upper end inside the rotating frame in a penetrating manner, a motor shaft extends from the lower end of each first motor, and a fan is arranged at one end of the motor shaft. According to the utility model, the unmanned aerial vehicle can be effectively tested and used.
Description
Technical Field
The utility model relates to the field of unmanned aerial vehicles, in particular to an AI unmanned aerial vehicle test platform.
Background
Unmanned aircraft, also known as "drones," are unmanned aircraft that are operated by radio remote control devices and self-contained program control devices, or are operated autonomously, either completely or intermittently, by an onboard computer, and are often more suited to tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.
The use of present stage to unmanned aerial vehicle test platform still has certain not enough, and the mobility effect is relatively poor, and can not provide good test environment, and inconvenient test angle adjustment to supplying air, therefore proposes an AI unmanned aerial vehicle test platform and solves this problem.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the defects in the prior art and provides an AI unmanned aerial vehicle test platform.
In order to achieve the purpose, the utility model adopts the following technical scheme: an AI unmanned aerial vehicle test platform comprises a test box and a buffer structure, wherein the buffer structure is arranged at the lower end of the test box, the upper end of the test box is provided with through openings in a penetrating manner, electric push rods are arranged around the upper end of the test box, a protective cover is arranged at the upper end of each electric push rod, and a monitoring device is arranged on the right side of the lower end of each protective cover;
the right side of test box is run through and is provided with air supply box, air supply box's inside front end is provided with the second motor, the one end that the one end of second motor extended there is motor shaft and motor shaft is provided with rotates the frame, it all runs through on the inside upper end both sides of frame to rotate and is provided with first motor, the lower extreme of first motor extends the one end that has motor shaft and is provided with the fan.
As a further description of the above technical solution:
buffer structure includes the support frame, the lower extreme of support frame is run through and is provided with the dashpot, the inside upper end of dashpot is provided with the telescopic link, the telescopic link is provided with a plurality ofly and equidistant range.
As a further description of the above technical solution:
the side of telescopic link is provided with the fixed block, the upper end of fixed block is connected with the inside upper end of dashpot.
As a further description of the above technical solution:
the side face of the lower end of the telescopic rod is provided with a spring, the lower end of the telescopic rod is provided with a movable plate, and universal wheels are arranged on the periphery of the lower end of the movable plate.
As a further description of the above technical solution:
the front end face of the test box is provided with a display screen, and a control device is arranged at the lower end of the display screen.
As a further description of the above technical solution:
the lower terminal surface of protective cover is provided with the protection pad, and the inner wall of test box all is provided with the protection pad.
As a further description of the above technical solution:
and the right side of the air supply box is provided with a ventilation hole in a penetrating manner, and a dust screen is arranged in the ventilation hole.
As a further description of the above technical solution:
the side of the second motor is provided with a limiting block, and the side of the limiting block is connected with the inner wall of the air supply box.
The utility model has the following beneficial effects:
1. according to the utility model, the buffering protection is carried out on the test box in the moving process through the buffering structure, so that the influence on equipment caused by bumping is avoided, the buffering protection is formed through the protection pad, and the damage caused by the collision of the unmanned aerial vehicle into the test box during the test due to the overlarge air volume is avoided, so that the impact force is reduced.
2. According to the utility model, the flight state of the unmanned aerial vehicle at different angles of air volume is monitored by the monitoring device, and the opening is sealed by driving the protective cover through the electric push rod, so that a good testing environment is improved.
3. According to the utility model, the fan is used for generating air volume to test the unmanned aerial vehicle, the second motor is used for driving the rotating frame to rotate within a certain range to adjust the vertical angle of the air supply, and the first motor is used for driving the fan to adjust the left and right angles of the air supply within a certain range, so that the unmanned aerial vehicle can be tested better.
4. The method can efficiently achieve the flight stability and the adaptive effect of the unmanned aerial vehicle at different wind speeds, simplify the testing steps and improve the testing efficiency.
Drawings
Fig. 1 is an appearance view of an AI unmanned aerial vehicle test platform according to the present invention;
fig. 2 is a front view of a protective cover of an AI unmanned aerial vehicle test platform according to the present invention;
fig. 3 is a schematic diagram of an internal structure of a wind supply box of an AI unmanned aerial vehicle test platform according to the present invention;
fig. 4 is a schematic diagram of a buffer structure of an AI unmanned aerial vehicle test platform according to the present invention.
Illustration of the drawings:
1. a universal wheel; 2. a test box; 3. a control device; 4. a display screen; 5. an electric push rod; 6. a port; 7. a protective cover; 8. a supply air box; 9. a ventilation hole; 10. a dust screen; 11. a protection pad; 12. a monitoring device; 13. a first motor; 14. a limiting block; 15. a second motor; 16. a fan; 17. rotating the frame; 18. a buffer structure; 181. a telescopic rod; 182. a fixed block; 183. a buffer tank; 184. a spring; 185. moving the plate; 186. a support frame.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-4, one embodiment of the present invention is provided: an AI unmanned aerial vehicle test platform, including test box 2 and buffer structure 18, buffer structure 18 sets up the lower extreme at test box 2, buffer structure 18 includes support frame 186, the lower extreme of support frame 186 runs through and is provided with dashpot 183, the inside upper end of dashpot 183 is provided with telescopic link 181, telescopic link 181 is provided with a plurality of and equidistant range, the side of telescopic link 181 is provided with fixed block 182, the upper end of fixed block 182 is connected with the inside upper end of dashpot 183, the lower extreme side of telescopic link 181 is provided with spring 184, the lower extreme of telescopic link 181 is provided with movable plate 185, the lower extreme of movable plate 185 all is provided with universal wheel 1 all around, use test box 2 in the removal process shock attenuation protection through buffer structure 18, avoid causing the influence to equipment because of jolting;
the front end face of the test box 2 is provided with a display screen 4, a control device 3 is arranged at the lower end of the display screen 4, an opening 6 is arranged at the upper end of the test box 2 in a penetrating mode, electric push rods 5 are arranged on the periphery of the upper end of the test box 2, a protective cover 7 is arranged at the upper end of each electric push rod 5, a monitoring device 12 is arranged on the right side of the lower end of each protective cover 7, the unmanned aerial vehicle is monitored in flying states under different air volumes at different angles through the monitoring device 12, a protective pad 11 is arranged on the lower end face of each protective cover 7, protective pads 11 are arranged on the inner wall of the test box 2, and the protective pads 11 are used for buffer protection, so that the situation that the unmanned aerial vehicle collides the inside of the test box 2 to be damaged when being tested due to overlarge air volume is avoided, and the impact force is reduced;
the right side of the test box 2 is provided with an air supply box 8 in a penetrating way, the right side of the air supply box 8 is provided with a ventilating hole 9 in a penetrating way, a dustproof net 10 is arranged inside the ventilating hole 9, the front end inside the air supply box 8 is provided with a second motor 15, the side surface of the second motor 15 is provided with a limiting block 14, the side surface of the limiting block 14 is connected with the inner wall of the air supply box 8, one end of the second motor 15 is extended with a motor shaft, one end of the motor shaft is provided with a rotating frame 17, the two sides of the upper end inside the rotating frame 17 are both provided with a first motor 13 in a penetrating way, the lower end of the first motor 13 is extended with the motor shaft, one end of the motor shaft is provided with a fan 16, the fan 16 is used for generating air volume to test the unmanned aerial vehicle, the second motor 15 drives the rotating frame 17 to rotate within a certain range to adjust the vertical angle of the air supply, and the first motor 13 drives the fan 16 to adjust the left and right angles of the air supply within a certain range, thereby be convenient for to the better test of unmanned aerial vehicle.
The working principle is as follows: come to carry out the bradyseism protection use to test box 2 at the removal in-process through buffer structure 18, avoid causing the influence to equipment because of jolting, come to carry out to unmanned aerial vehicle under the different angle amount of wind through monitoring devices 12, the state monitoring of flight, come to produce the amount of wind through fan 16 and come to use the unmanned aerial vehicle test, and drive through second motor 15 and rotate frame 17 and carry out the rotation of certain limit, come angle modulation about the air supply, and drive fan 16 through first motor 13 and come to carry out the certain limit to the angle about the air supply and adjust, thereby be convenient for to the better test of unmanned aerial vehicle, it seals port 6 to drive protective cover 7 through electric putter 5, improve good test environment.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the utility model.
Claims (8)
1. The utility model provides an AI unmanned aerial vehicle test platform, includes test box (2) and buffer structure (18), its characterized in that: the buffer structure (18) is arranged at the lower end of the test box (2), the upper end of the test box (2) is provided with a through hole (6) in a penetrating manner, electric push rods (5) are arranged on the periphery of the upper end of the test box (2), a protective cover (7) is arranged at the upper end of each electric push rod (5), and a monitoring device (12) is arranged on the right side of the lower end of each protective cover (7);
the right side of test box (2) is run through and is provided with air supply box (8), the inside front end of air supply box (8) is provided with second motor (15), the one end of second motor (15) is extended the one end that has motor shaft and is provided with and rotates frame (17), the inside upper end both sides of rotating frame (17) all run through and are provided with first motor (13), the lower extreme of first motor (13) is extended the one end that has motor shaft and is provided with fan (16).
2. The AI unmanned aerial vehicle test platform of claim 1, wherein: buffer structure (18) include support frame (186), the lower extreme of support frame (186) is run through and is provided with dashpot (183), the inside upper end of dashpot (183) is provided with telescopic link (181), telescopic link (181) are provided with a plurality ofly and equidistant range.
3. The AI unmanned aerial vehicle test platform of claim 2, wherein: the side of telescopic link (181) is provided with fixed block (182), the upper end of fixed block (182) is connected with the inside upper end of dashpot (183).
4. The AI unmanned aerial vehicle test platform of claim 2, wherein: the side face of the lower end of the telescopic rod (181) is provided with a spring (184), the lower end of the telescopic rod (181) is provided with a moving plate (185), and universal wheels (1) are arranged on the periphery of the lower end of the moving plate (185).
5. The AI unmanned aerial vehicle test platform of claim 1, wherein: the front end face of the test box (2) is provided with a display screen (4), and a control device (3) is arranged at the lower end of the display screen (4).
6. The AI unmanned aerial vehicle test platform of claim 1, wherein: the lower terminal surface of protective cover (7) is provided with protection pad (11), and the inner wall of test box (2) all is provided with protection pad (11).
7. The AI unmanned aerial vehicle test platform of claim 1, wherein: the right side of the air supply box (8) is provided with a ventilation hole (9) in a penetrating mode, and a dust screen (10) is arranged inside the ventilation hole (9).
8. The AI unmanned aerial vehicle test platform of claim 1, wherein: and a limiting block (14) is arranged on the side surface of the second motor (15), and the side surface of the limiting block (14) is connected with the inner wall of the air supply box (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122551909.4U CN215851972U (en) | 2021-10-22 | 2021-10-22 | AI unmanned aerial vehicle test platform |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122551909.4U CN215851972U (en) | 2021-10-22 | 2021-10-22 | AI unmanned aerial vehicle test platform |
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| CN215851972U true CN215851972U (en) | 2022-02-18 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114811321A (en) * | 2022-05-20 | 2022-07-29 | 中建二局第一建筑工程有限公司 | Control device for super high-rise concrete pouring quality |
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2021
- 2021-10-22 CN CN202122551909.4U patent/CN215851972U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114811321A (en) * | 2022-05-20 | 2022-07-29 | 中建二局第一建筑工程有限公司 | Control device for super high-rise concrete pouring quality |
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