CN215449922U - Unmanned aerial vehicle flow field intelligent control device - Google Patents
Unmanned aerial vehicle flow field intelligent control device Download PDFInfo
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- CN215449922U CN215449922U CN202023308149.6U CN202023308149U CN215449922U CN 215449922 U CN215449922 U CN 215449922U CN 202023308149 U CN202023308149 U CN 202023308149U CN 215449922 U CN215449922 U CN 215449922U
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Abstract
The utility model discloses an intelligent control device for a flow field of an unmanned aerial vehicle, which comprises a base; the upper surface of the base is provided with an anemoscope and a anemoscope; the rear ends of the wing part and the base are provided with tail wings; a turnover shaft is arranged at the joint of the empennage, the wing part and the base; the inner part of the wing part is provided with a vent hole; an automatic blocking door is arranged inside the ventilation hole; a rotating base is arranged in the upper surface of the base in a sinking manner; the center of the rotating base is provided with an air deflector; the controller is connected with the turnover shaft, the automatic door and the rotary base through a data bus; according to the intelligent control device for the flow field of the unmanned aerial vehicle, the anemoscope and the anemoscope are arranged, so that the peripheral wind speed and wind direction of the unmanned aerial vehicle can be measured, and the flow field condition of the unmanned aerial vehicle can be obtained; the air vents, the empennage, the air deflectors and other components can change the flow field condition of the unmanned aerial vehicle, and the intelligent control system can realize real-time control on the flow field; can improve unmanned aerial vehicle's flight efficiency.
Description
Technical Field
The utility model relates to the field of unmanned aerial vehicles, in particular to an intelligent control device for a flow field of an unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. In the process of flying movement of the unmanned aerial vehicle, the speed, the pressure and the like of the unmanned aerial vehicle can be changed due to various factors, and the changes can influence the flight of the unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
In order to overcome the defects of the prior art, the utility model provides an intelligent control device for the flow field of an unmanned aerial vehicle, which can intelligently control the flow field around the unmanned aerial vehicle.
The technical scheme adopted by the utility model for solving the technical problems is as follows: an unmanned aerial vehicle flow field intelligent control device comprises a base; the upper surface of the base is provided with an anemoscope and a anemoscope; the bottoms of the anemoscope and the anemoscope are provided with rotating seats; a converter is arranged in the rotating seat; a controller is fixedly arranged below the converter; the converter is connected with the controller through a data bus; wing parts are arranged on two sides of the base; the rear ends of the wing part and the base are provided with tail wings; a turnover shaft is arranged at the joint of the empennage, the wing part and the base; the inner part of the wing part is provided with a vent hole; an automatic blocking door is arranged inside the ventilation hole; a rotating base is arranged in the upper surface of the base in a sinking manner; the center of the rotating base is provided with an air deflector; the controller is connected with the turnover shaft, the automatic door and the rotary base through a data bus.
Furthermore, the front end of the base is provided with a wind breaking head;
further, the bottom of the base is provided with an assembling hole; the inner wall of the assembling hole is provided with threads;
further, the front end surface of the wing part is an arc surface;
further, a wireless signal transceiver is arranged inside the base;
further, the air deflector is perpendicular to the base.
Compared with the prior art, the utility model has the beneficial effects that: according to the intelligent control device for the flow field of the unmanned aerial vehicle, the anemoscope and the anemoscope are arranged, so that the peripheral wind speed and wind direction of the unmanned aerial vehicle can be measured, and the flow field condition of the unmanned aerial vehicle can be obtained; the air vents, the empennage, the air deflectors and other components can change the flow field condition of the unmanned aerial vehicle, and the intelligent control system can realize real-time control on the flow field; can improve unmanned aerial vehicle's flight efficiency.
Drawings
FIG. 1 is a first overall structural schematic of the present invention;
FIG. 2 is a partial structural view of part A in FIG. 1;
FIG. 3 is a second overall structural schematic of the present invention;
fig. 4 is an overall bottom view of the present invention.
Reference numbers in the figures: 1-a base; 2-an anemometer; 3-a wind direction indicator; 4-a rotating seat; 5-a converter; 6-a controller; 7-a wing part; 8-tail fin; 9-a turning shaft; 10-a vent; 11-automatic door blocking; 12-a rotating base; 13-a wind deflector; 14-a wind breaking head; 15-assembly holes; 16-Wireless transceiver.
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.
The intelligent control device for the unmanned aerial vehicle flow field is described in detail with reference to fig. 1-4 as follows: an unmanned aerial vehicle flow field intelligent control device comprises a base 1; an anemoscope 2 and a anemoscope 3 are arranged on the upper surface of the base 1; the bottoms of the anemoscope 2 and the anemoscope 3 are both provided with a rotating seat 4; a converter 5 is arranged in the rotating seat 4; a controller 6 is fixedly arranged below the converter 5; the converter 5 is connected with the controller 6 through a data bus; wing parts 7 are arranged on two sides of the base 1; the rear ends of the wing part 7 and the base 1 are provided with tail wings 8; a turnover shaft 9 is arranged at the joint of the tail wing 8, the wing part 7 and the base 1; the wing part 7 is internally provided with a ventilation hole 10; an automatic blocking door 11 is arranged inside the ventilation hole 10; a rotating base 12 is arranged in the upper surface of the base 1 in a recessed manner; an air deflector 13 is arranged at the center of the rotating base 12; the controller 6 is connected with the turning shaft 9, the automatic door 11 and the rotary base 12 through a data bus.
The front end of the base 1 is provided with a wind breaking head 14; the bottom of the base 1 is provided with an assembling hole 15; the inner wall of the assembling hole 15 is provided with threads; the front end surface of the wing part 7 is an arc surface; a wireless signal transceiver is arranged in the base 1; the air deflector 13 is perpendicular to the base 1.
The working principle is as follows: the inside of the converter 5 is a slit optical coupler; under the action of wind, the anemoscope 2 and the anemoscope 3 rotate; the central shaft rotates in the slit optical coupler, an electric signal is output, the electric signal enters the controller 6, and the flow field around the unmanned aerial vehicle is obtained through translation, analysis and other processes.
The controller 6 controls the flow field by controlling the turnover shaft 9, the automatic door 11, the rotary base 12 and other components; the overturning shaft 9 overturns to enable the tail wing 8 to be in different angle states so as to change the airflow passing through the unmanned aerial vehicle and change the lower pressure and the upper pressure; the automatic door 11 can be opened and closed in a telescopic way, and whether the ventilation holes 10 can ventilate is controlled, so that the air passing rate of the wing part 7 is changed, and the air resistance is changed along with the change; the rotating base 12 drives the air deflector 13 to rotate, so as to change the flowing path of the air flow.
Be connected the device with unmanned aerial vehicle through pilot hole 15, through data bus connection, controller 6 can adjust unmanned aerial vehicle's various data, further control flow field. Meanwhile, data can be shared to an external mobile phone terminal through the wireless signal transceiver, and the flow field condition of the unmanned aerial vehicle can be known at any time.
In summary, the intelligent control device for the unmanned aerial vehicle flow field is provided with the anemoscope and the anemoscope, and the anemoscope can measure the wind speed and the wind direction around the unmanned aerial vehicle, so that the flow field condition of the unmanned aerial vehicle is obtained; the air vents, the empennage, the air deflectors and other components can change the flow field condition of the unmanned aerial vehicle, and the intelligent control system can realize real-time control on the flow field; can improve unmanned aerial vehicle's flight efficiency.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. An unmanned aerial vehicle flow field intelligent control device is characterized by comprising a base; the upper surface of the base is provided with an anemoscope and a anemoscope; the bottoms of the anemoscope and the anemoscope are provided with rotating seats; a converter is arranged in the rotating seat; a controller is fixedly arranged below the converter; the converter is connected with the controller through a data bus;
wing parts are arranged on two sides of the base; the rear ends of the wing part and the base are provided with tail wings; a turnover shaft is arranged at the joint of the empennage, the wing part and the base; the inner part of the wing part is provided with a vent hole; an automatic blocking door is arranged inside the ventilation hole;
a rotating base is arranged in the upper surface of the base in a sinking manner; the center of the rotating base is provided with an air deflector;
the controller is connected with the turnover shaft, the automatic door and the rotary base through a data bus.
2. The unmanned aerial vehicle flow field intelligent control device of claim 1, characterized in that: the front end of the base is provided with a wind breaking head.
3. The unmanned aerial vehicle flow field intelligent control device of claim 1, characterized in that: the bottom of the base is provided with an assembling hole; and the inner wall of the assembling hole is provided with threads.
4. The unmanned aerial vehicle flow field intelligent control device of claim 1, characterized in that: the front end surface of the wing part is an arc surface.
5. The unmanned aerial vehicle flow field intelligent control device of claim 1, characterized in that: the base is internally provided with a wireless signal transceiver.
6. The unmanned aerial vehicle flow field intelligent control device of claim 1, characterized in that: the air deflector is perpendicular to the base.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023308149.6U CN215449922U (en) | 2020-12-30 | 2020-12-30 | Unmanned aerial vehicle flow field intelligent control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023308149.6U CN215449922U (en) | 2020-12-30 | 2020-12-30 | Unmanned aerial vehicle flow field intelligent control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215449922U true CN215449922U (en) | 2022-01-07 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023308149.6U Active CN215449922U (en) | 2020-12-30 | 2020-12-30 | Unmanned aerial vehicle flow field intelligent control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215449922U (en) |
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2020
- 2020-12-30 CN CN202023308149.6U patent/CN215449922U/en active Active
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