CN211694107U - Directional unmanned aerial vehicle counter-braking device - Google Patents
Directional unmanned aerial vehicle counter-braking device Download PDFInfo
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- CN211694107U CN211694107U CN202020199491.8U CN202020199491U CN211694107U CN 211694107 U CN211694107 U CN 211694107U CN 202020199491 U CN202020199491 U CN 202020199491U CN 211694107 U CN211694107 U CN 211694107U
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Abstract
The utility model discloses a directional unmanned aerial vehicle reverse system device, which relates to the technical field of unmanned aerial vehicle reverse system, and comprises a support frame and a reverse system body arranged above the support frame, wherein the upper end of the support frame is fixedly provided with a fixed station, the upper end surface of the fixed station is fixedly provided with a connecting seat, the connecting seat is rotatably connected with a connecting shaft, the upper end of the connecting shaft is fixedly provided with a rotating station, the upper end surface of the rotating station is fixedly provided with a fixed frame, the upper end of the fixed frame is fixedly provided with a connecting shaft sleeve, the utility model is provided with the fixed station, the connecting seat, the rotating station, the connecting shaft, the fixed frame, the connecting shaft sleeve, an adjusting shaft, an adjusting handle, a spring, a stop block and a cushion pad, the horizontal angle and the inclination angle of the reverse system body can be adjusted to proper positions, the reverse system body can be conveniently and rapidly aimed and positioned, so that the reaction device is more convenient to operate and use.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle counter-system technical field specifically is a directional formula unmanned aerial vehicle counter-system device.
Background
An unmanned aerial vehicle, abbreviated as "unmanned aerial vehicle" ("UAV"), is an unmanned aerial vehicle that is operated using a radio remote control device and a self-contained program control device. Unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned dirigible airship, unmanned helicopter, unmanned many rotor crafts, unmanned umbrella wing aircraft etc. it has small, the cost is low, convenient to use, requires advantages such as low to service environment, and anti-unmanned aerial vehicle system refers to the device that utilizes technical means to carry out directional monitoring, interference, decoy, control, destroy to unmanned aerial vehicle.
However traditional unmanned aerial vehicle counteraction device is in the use, because structural constraint, the counteraction organism is not convenient for aim the location fast, brings inconvenience for the operation use, consequently, the technical personnel in the field provide a directional unmanned aerial vehicle counteraction device.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a directional formula unmanned aerial vehicle counter-system device to provide traditional unmanned aerial vehicle counter-system device in solving above-mentioned background art in the use, because structural constraint, counter-system organism is not convenient for aim the location fast, uses the problem of bringing inconvenience for the operation.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides a directional formula unmanned aerial vehicle system of turning over, includes the support frame and sets up the system of turning over organism in the support frame top, the fixed station that is provided with in upper end of support frame, the upper end fixed surface of fixed station is provided with the connecting seat, the connecting seat rotates and is connected with the connecting axle, the fixed rotation platform that is provided with in upper end of connecting axle, the upper end fixed surface who rotates the platform is provided with the mount, the fixed connecting axle sleeve that is provided with in upper end of mount, the fixed regulating spindle that is provided with in both ends of the system of turning over organism, the bottom fixed surface who turns over the system organism is connected with the spring, the bottom fixedly connected with dog of spring, the upper end fixed surface.
As a further aspect of the present invention: the connecting shaft sleeve is rotatably connected with the adjusting shaft, and an adjusting handle is fixedly arranged at one end of the adjusting shaft.
As a further aspect of the present invention: and damping rubber is fixedly arranged at the inner position of the connecting seat.
As a further aspect of the present invention: the inside position department of the anti-system organism is fixed and is provided with the battery, the output of solar panel and the input electric connection of battery.
As a further aspect of the present invention: the bottom surface of the stop block is fixedly provided with a cushion pad, and the cushion pad is a component made of rubber.
As a further aspect of the present invention: the bottom position department of support frame is fixed and is provided with the removal wheel, the side position department of removing the wheel is fixed and is provided with the brake valve.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses set up fixed station, connecting seat, swivel mount, connecting axle, mount, connecting axle sleeve, regulating spindle, adjustment handle, spring, dog and blotter, can transfer the horizontal angle and the inclination of the system organism of turning over to suitable position, improved the structure flexibility of the system of turning over, be convenient for carry out the location of aiming fast with the system of turning over the organism, the dog falls to the spring can play the cushioning effect to the system of turning over organism when rotating the bench for the system of turning over is convenient for operate and use more.
2. The utility model discloses set up solar panel and battery, solar panel can supply the battery savings to use with solar energy transformation for the electric energy, is favorable to improving the duration of unmanned aerial vehicle anti-system device.
Drawings
Fig. 1 is a schematic perspective view of a directional drone countermeasure device;
fig. 2 is a schematic front view of a directional unmanned aerial vehicle reverse braking device;
fig. 3 is an enlarged schematic view of a part a of the directional drone reflex device.
In the figure: 1. a support frame; 2. a fixed table; 201. a connecting seat; 3. a rotating table; 301. a connecting shaft; 4. reversing the machine body; 5. a moving wheel; 501. a brake valve; 6. a fixed mount; 7. connecting the shaft sleeve; 8. an adjustment shaft; 801. an adjusting handle; 9. a solar panel; 10. a storage battery; 11. a spring; 12. a stopper; 121. a cushion pad.
Detailed Description
Please refer to fig. 1-3, in the embodiment of the utility model, an oriented unmanned aerial vehicle reverse system device, including support frame 1 and the reverse system organism 4 of setting in support frame 1 top, the fixed station 2 that is provided with in upper end of support frame 1, the fixed surface of upper end of fixed station 2 is provided with connecting seat 201, connecting seat 201 rotates and is connected with connecting axle 301, the fixed rotation platform 3 that is provided with in upper end of connecting axle 301, the fixed surface that is provided with in upper end of rotation platform 3 is provided with mount 6, the fixed connecting axle sleeve 7 that is provided with in upper end of mount 6, the fixed regulating spindle 8 that is provided with in both ends of reverse system organism 4, the fixed surface in bottom of reverse system organism 4 is connected with spring 11, spring 11's bottom fixedly connected with dog 12, the fixed surface.
In fig. 1: the connecting shaft sleeve 7 is rotatably connected with the adjusting shaft 8, and an adjusting handle 801 is fixedly arranged at one end of the adjusting shaft 8, so that the purpose of conveniently rotating the adjusting shaft 8 is achieved.
In fig. 2: the fixed damping rubber that is provided with of inside position department of connecting seat 201 has reached the purpose of being convenient for rotate revolving stage 3.
In fig. 2: the fixed battery 10 that is provided with in inside position department of the anti-machine body 4, the output of solar panel 9 and the input electric connection of battery 10 have reached and have made solar panel 9 can convert solar energy into the electric energy and supply the purpose that battery 10 savings was used.
In fig. 3: the fixed blotter 121 that is provided with in bottom surface position department of dog 12, blotter 121 is the component that a material is rubber, has reached the purpose that can play the cushioning effect.
In fig. 1: the bottom end of the support frame 1 is fixedly provided with a movable wheel 5, and the side position of the movable wheel 5 is fixedly provided with a brake valve 501, so that the purpose of moving the device conveniently is achieved.
The utility model discloses a theory of operation is: in the process of using the unmanned aerial vehicle reverse control device, when the horizontal angle of the reverse control machine body 4 needs to be adjusted, the reaction machine body 4 is rotated on the fixed platform 2 until the horizontal angle of the reaction machine body 4 is adjusted to be proper, when the inclination angle of the reverse mechanism body 4 needs to be adjusted, the connecting shaft sleeve 7 is rotatably connected with the adjusting shaft 8, the adjusting handle 801 is used for rotating the adjusting shaft 8 until the inclination angle of the reverse mechanism body 4 is adjusted to be proper, so that the reverse mechanism body 4 can be conveniently and quickly aimed and positioned for use, after the use is finished, the adjusting handle 801 is loosened, the stop block 12 falls on the rotating table 3, the spring 11 can play a role of buffering, when the device needs to be moved, the brake valve 501 is opened, the pushing device is moved, the solar panel 9 is fixedly arranged on the surface of the upper end of the reverse control machine body 4, and solar energy can be converted into electric energy by the solar panel 9 to be stored and used by the storage battery 10.
The above-mentioned, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. The utility model provides a directional formula unmanned aerial vehicle reverse system device, includes support frame (1) and sets up reverse system organism (4) in support frame (1) top, its characterized in that, the fixed station (2) that is provided with in upper end of support frame (1), the fixed connecting seat (201) that is provided with of upper end surface of fixed station (2), connecting seat (201) rotate and are connected with connecting axle (301), the fixed rotating station (3) that is provided with in upper end of connecting axle (301), the fixed mount (6) that is provided with in upper end surface of rotating station (3), the fixed connecting axle sleeve (7) that is provided with in upper end of mount (6), the fixed regulating spindle (8) that is provided with in both ends of reverse system organism (4), the fixed spring (11) that is connected with in bottom surface of reverse system organism (4), the fixed dog (12) that is connected with in bottom of, and a solar panel (9) is fixedly arranged on the upper end surface of the reaction machine body (4).
2. The directional unmanned aerial vehicle reaction device of claim 1, characterized in that the connecting shaft sleeve (7) is rotatably connected with an adjusting shaft (8), and an adjusting handle (801) is fixedly arranged at one end of the adjusting shaft (8).
3. A directional drone reaction device according to claim 1, characterised in that the connection seat (201) is fixed with damping rubber at its inner position.
4. The device of claim 1, wherein a storage battery (10) is fixedly arranged at an inner position of the countering body (4), and an output end of the solar panel (9) is electrically connected with an input end of the storage battery (10).
5. A directional drone reaction device according to claim 1, characterized in that a cushion (121) is fixed on the bottom surface of the block (12), the cushion (121) is a rubber member.
6. A directional unmanned aerial vehicle opposing device according to claim 1, wherein a bottom end position of the support frame (1) is fixedly provided with a movable wheel (5), and a side position of the movable wheel (5) is fixedly provided with a brake valve (501).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020199491.8U CN211694107U (en) | 2020-02-24 | 2020-02-24 | Directional unmanned aerial vehicle counter-braking device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020199491.8U CN211694107U (en) | 2020-02-24 | 2020-02-24 | Directional unmanned aerial vehicle counter-braking device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211694107U true CN211694107U (en) | 2020-10-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020199491.8U Active CN211694107U (en) | 2020-02-24 | 2020-02-24 | Directional unmanned aerial vehicle counter-braking device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211694107U (en) |
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2020
- 2020-02-24 CN CN202020199491.8U patent/CN211694107U/en active Active
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Legal Events
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230414 Address after: 421000 Chayuan Village Industrial Park, Yanfeng Industrial Cluster, Hengyang City, Hunan Province Patentee after: Hunan Jinbei Pharmaceutical Machinery Technology Co.,Ltd. Address before: No.3 Xingye Road, industrial project cluster district, Yanfeng District, Hengyang City, Hunan Province, 421000 Patentee before: HENGYANG YUN YAN AVIATION TECHNOLOGY Co.,Ltd. |