CN211033059U - Many unmanned aerial vehicle event support auxiliary device - Google Patents
Many unmanned aerial vehicle event support auxiliary device Download PDFInfo
- Publication number
- CN211033059U CN211033059U CN201921792944.1U CN201921792944U CN211033059U CN 211033059 U CN211033059 U CN 211033059U CN 201921792944 U CN201921792944 U CN 201921792944U CN 211033059 U CN211033059 U CN 211033059U
- Authority
- CN
- China
- Prior art keywords
- camera
- unmanned aerial
- aerial vehicle
- auxiliary device
- motor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Abstract
The utility model belongs to the technical field of unmanned aerial vehicle, specifically be a many unmanned aerial vehicle race guarantee auxiliary device, including wing, fuselage and image acquisition device, image acquisition device includes the rotary disk, the rotary disk sets up the fuselage bottom, be provided with the recess on the rotary disk, be provided with two mesh cameras in the recess, two mesh cameras include first camera and second camera, be provided with wiping mechanism on the recess inner wall of first camera one side, be provided with on the recess inner wall of second camera one side and shelter from the mechanism, the utility model has the advantages of do not influence unmanned aerial vehicle continuation flight when cleaning the dust on the first camera.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, specifically be a many unmanned aerial vehicle event support auxiliary device.
Background
In the process of flying in a match, for example, multiple unmanned aerial vehicles fly in a windy and sandy place due to the terrain or weather, the cameras of the multiple unmanned aerial vehicles are inevitably adhered with dust which can block the cameras from collecting surrounding images and further influence the unmanned aerial vehicles on judging surrounding obstacles, so that the flying of the unmanned aerial vehicles is influenced, the dust needs to be treated in order to ensure the safety of the flying of the unmanned aerial vehicles, but the multiple unmanned aerial vehicles cannot return to the air to be cleaned in the process of the match, so an auxiliary device which can clean the cameras of the multiple unmanned aerial vehicles in time is needed, the cameras of the multiple unmanned aerial vehicles can clearly image through cleaning the dust on the cameras, the safety of flying of the multiple unmanned aerial vehicles is ensured, and in the process of the match, the multiple unmanned aerial vehicles cannot stop in the air to be cleaned in order to improve the score, so still need guarantee when the dust on the clearance camera, do not influence many unmanned aerial vehicle's normal flight, guarantee the efficiency of many unmanned aerial vehicle matches.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a many unmanned aerial vehicle race guarantee auxiliary device for solve among the prior art many unmanned aerial vehicle at the match flight in-process, the camera is infected with the corpse of dust or little winged insect, can not in time clear up, influences many unmanned aerial vehicle flight safety and the problem of efficiency.
In order to achieve the above object, the utility model adopts the following technical scheme: the utility model provides a many unmanned aerial vehicle race support auxiliary device, includes the wing, fuselage and image acquisition device, image acquisition device includes the rotary disk, the rotary disk sets up fuselage bottom, be provided with the recess on the rotary disk, be provided with two mesh cameras in the recess, two mesh cameras include first camera and second camera, be provided with wiping mechanism on the recess inner wall of first camera one side, wiping mechanism includes the supporting seat, the supporting seat sets up the recess inner wall, be provided with first motor on the supporting seat, the output shaft of first motor has the telescopic link, the telescopic link is connected with the cleaning plate, it has chamois to clean the surface parcel of plate, chamois is used for cleaning first camera, be provided with on the recess inner wall of second camera one side and shelter from the mechanism, it includes second motor, image acquisition device to shelter from the mechanism, The output gear is coaxially connected with an output shaft of the second motor, the transmission gear is coaxially connected with one end of the transmission rod, the output gear is in transmission connection with the transmission gear, the shielding plate is connected with the other end of the transmission rod, and the shielding plate corresponds to the second camera.
By adopting the technical scheme, the first camera is firstly used for image acquisition, when the first camera is dusty, the second motor is started, the second motor drives the output gear to rotate, the output gear drives the transmission gear to rotate, the transmission gear drives the transmission rod to rotate, the transmission rod drives the shielding plate to rotate, the second camera is exposed, the rotating disc is controlled to rotate, the first camera and the second camera are exchanged in position, the second camera is started for image acquisition, the first motor is started, the first motor pushes the wiping plate to move through the telescopic rod, chamois on the surface of the wiping plate wipes dust on the surface of the first camera completely, then the second camera is stopped, the first camera and the second camera are replaced again through the rotating disk, the first camera is started, the second motor is started to rotate reversely, and the shielding plate restores the original position to shield the second camera.
Preferably, a rotating guide rail is arranged between the rotating disk and the machine body, an electric slider is arranged on the rotating guide rail, and the rotating disk is fixedly connected with the electric slider.
Through adopting above-mentioned technical scheme, can move and then control the 360 degrees rotations of rotary disk on rotatory guide rail through controlling electronic slider.
Preferably, the bottom of the machine body is further provided with a support frame, the lower end of the support frame is fixedly provided with a bottom frame, and a plurality of reinforcing cross beams are fixedly arranged between every two adjacent groups of bottom frames.
Through adopting above-mentioned technical scheme, unmanned aerial vehicle is that the chassis lands when falling to the ground, can prevent that the camera from touching down to cause the damage.
Preferably, a crank arm is arranged on one side face of the supporting frame, one end of the crank arm is connected with the supporting frame, and the other end of the crank arm is connected with the bottom frame.
Through adopting above-mentioned technical scheme, adopt the crank arm, can strengthen the structural firmness of support frame and chassis.
Preferably, the underframe and the reinforcing crossbeam form a trapezoidal frame, and thickened shock-absorbing rubber pads are arranged on the lower surfaces of the underframe and the reinforcing crossbeam.
Through adopting above-mentioned technical scheme, adopt chassis and reinforcement crossbeam to constitute trapezoidal frame, this structure makes unmanned aerial vehicle fall to the ground more steady, and this structure is made by the aluminum alloy, has light in weight, and the load pressure of unmanned aerial vehicle can be alleviateed to the characteristic that the structure is firm.
Preferably, a controller is arranged inside the machine body, the controller is electrically connected with the first motor and used for controlling the wiping mechanism to wipe the first camera, and the controller is electrically connected with the second motor and used for controlling the shielding mechanism to rotate.
Preferably, a GPS positioning module is further arranged in the machine body and electrically connected with the controller.
Through adopting above-mentioned technical scheme, the operating personnel of being convenient for in time fixes a position the position at unmanned aerial vehicle place.
Preferably, the number of the wings is four, and the four wings are symmetrically arranged at the top of the fuselage.
Through adopting above-mentioned technical scheme, four wings symmetry sets up and makes unmanned aerial vehicle flight steady.
The utility model has the beneficial technical effects that:
by arranging a first camera and a second camera, a wiping mechanism is arranged on one side of the first camera, a shielding mechanism is arranged on one side of the second camera, in the process of multi-unmanned aerial vehicle competition, the first camera is firstly used for image acquisition, when dust accumulated on the first camera causes unclear acquired images, an electric slider is controlled to control a rotating disc to rotate, the first camera and the second camera are exchanged in position, a second motor is started, the second motor drives an output gear to rotate, the output gear drives a transmission gear to rotate, the transmission gear drives a transmission rod to rotate, the transmission rod drives a shielding plate to rotate, the second camera is exposed, the rotating disc is controlled to rotate, the first camera and the second camera are exchanged in position, the second camera is started to acquire images, the first motor is started, the first motor pushes the wiping plate to move through a telescopic rod, the chamois on wiper surface cleans first camera surperficial dust totally, then the second camera that deactivates, through the rotary disk with first camera and second camera transposition position once more, start first camera, start the reversal of second motor, the shielding plate resumes the normal position and shelters from the second camera, this device is through the alternate use of first camera and second camera, has the advantage that can not influence unmanned aerial vehicle's normal flight when clearing up first camera.
Drawings
Fig. 1 is a front view schematically illustrating an embodiment of the present invention;
fig. 2 is a schematic bottom view of an embodiment of the present invention;
FIG. 3 is a schematic view of a wiping mechanism according to an embodiment of the present invention;
fig. 4 is a schematic structural view of a shielding mechanism according to an embodiment of the present invention;
fig. 5 is a schematic view of a supporting frame according to an embodiment of the present invention;
fig. 6 is a schematic view of a rotary guide rail according to an embodiment of the present invention.
In the figure: 1. an airfoil; 2. a body; 3. rotating the disc; 4. a groove; 6. a first camera; 7. a second camera; 8. a supporting seat; 9. a first motor; 10. a telescopic rod; 11. a second motor; 12. an output gear; 13. a transmission gear; 14. a transmission rod; 15. a shielding plate; 16. rotating the guide rail; 17. an electric slider; 18. a support frame; 19. a chassis; 20. a cross beam; 21. a crank arm, 22; and (4) wiping the board.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
As shown in fig. 1, a multi-unmanned aerial vehicle race support auxiliary device comprises a wing 1, a body 2 and an image acquisition device, wherein the image acquisition device comprises a rotary disk 3, the rotary disk 3 is arranged at the bottom of the body 2, a groove 4 is arranged on the rotary disk 3, a binocular camera is arranged in the groove 4, the binocular camera comprises a first camera 6 and a second camera 7, a wiping mechanism is arranged on the inner wall of the groove 4 at one side of the first camera 6, the wiping mechanism comprises a supporting seat 8, the supporting seat 8 is arranged on the inner wall of the groove 4, a first motor 9 is arranged on the supporting seat 8, an output shaft of the first motor 9 is connected with a telescopic rod 10, the telescopic rod 10 is connected with a wiping plate 22, the surface of the wiping plate 22 is wrapped with chamois which is used for wiping the first camera 6, a shielding mechanism is arranged on the inner wall of the groove 4 at one side of the second camera 7, the shielding mechanism comprises a second motor 11, an output gear 12, a transmission gear 13, a transmission rod 14 and a shielding plate 15, the output gear 12 is coaxially connected with an output shaft of the second motor 11, the transmission gear 13 is coaxially connected with one end of the transmission rod 14, the output gear 12 is in transmission connection with the transmission gear 13, the shielding plate 15 is connected with the other end of the transmission rod 14, and the shielding plate 15 corresponds to the second camera 7.
Firstly, a first camera is used for image acquisition, when the first camera is dusty, a second motor is started, the second motor drives an output gear to rotate, the output gear drives a transmission gear to rotate, the transmission gear drives a transmission rod to rotate, the transmission rod drives a shielding plate to rotate, the second camera is exposed, a rotating disk is controlled to rotate, the first camera and the second camera are exchanged in position, the second camera is started for image acquisition, the first motor is started, the first motor pushes a wiping plate to move through a telescopic rod, chamois on the surface of the wiping plate wipes dust on the surface of the first camera completely, then the second camera is stopped, the first camera and the second camera are replaced again through the rotating disk, the first camera is started, the second motor is started to rotate reversely, and the shielding plate restores the original position to shield the second camera.
As shown in fig. 6, a rotary guide rail 16 is provided between the rotary disk 3 and the body 2, an electric slider 17 is provided on the rotary guide rail 16, and the rotary disk 3 is fixedly connected to the electric slider 17.
It can be understood that, in order to guarantee the stability that unmanned aerial vehicle fell to the ground and the safety of binocular camera, as shown in fig. 5, 2 bottoms of fuselage still are provided with support frame 18, the lower extreme fixed mounting of support frame 18 has chassis 19, adjacent two sets of fixed mounting has many reinforcing beam 20 between the chassis 19.
One side surface of the support frame 18 is provided with a crank arm 21, one end of the crank arm 21 is connected with the support frame 18, and the other end is connected with the underframe 19.
Correspondingly, the underframe 19 and the reinforcing crossbeam 20 form a trapezoidal frame, and thickened shock-absorbing rubber pads are arranged on the lower surfaces of the underframe 19 and the reinforcing crossbeam 20.
Adopt chassis and reinforcement crossbeam to constitute trapezoidal frame, this structure makes unmanned aerial vehicle fall to the ground more steadily, and this structure is made by the aluminum alloy, has light in weight, and the characteristic that the structure is firm can alleviate unmanned aerial vehicle's load pressure, adopts the crank arm, can strengthen the structural firmness of support frame and chassis, whole device simple structure, convenient operation, the effect of use is better for traditional mode.
It should be noted that a controller is arranged inside the body 2, the controller is electrically connected with the first motor 9 and used for controlling the wiping mechanism to wipe the first camera 6, and the controller is electrically connected with the second motor 11 and used for controlling the shielding mechanism to rotate, wherein the control mode is a conventional controller control mode.
Consider that operating personnel conveniently fixes a position unmanned aerial vehicle, still be provided with GPS orientation module in the fuselage 2, GPS orientation module and controller electric connection.
It should be noted that the number of the wings 1 is four, and the four wings 1 are symmetrically arranged on the top of the fuselage 2.
The utility model discloses a theory of operation does: firstly, a first camera is used for image acquisition, when the first camera is dusty, a second motor is started, the second motor drives an output gear to rotate, the output gear drives a transmission gear to rotate, the transmission gear drives a transmission rod to rotate, the transmission rod drives a shielding plate to rotate, the second camera is exposed, a rotating disk is controlled to rotate, the first camera and the second camera are exchanged in position, the second camera is started for image acquisition, the first motor is started, the first motor pushes a wiping plate to move through a telescopic rod, chamois on the surface of the wiping plate wipes dust on the surface of the first camera completely, then the second camera is stopped, the first camera and the second camera are replaced again through the rotating disk, the first camera is started, the second motor is started to rotate reversely, and the shielding plate restores the original position to shield the second camera.
In the description of the present invention, it should be understood that the terms "counterclockwise", "clockwise", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description of the present invention, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Claims (8)
1. The utility model provides a many unmanned aerial vehicle race guarantee auxiliary device, its characterized in that, includes wing (1), fuselage (2) and image acquisition device, image acquisition device includes rotary disk (3), rotary disk (3) set up fuselage (2) bottom, be provided with recess (4) on rotary disk (3), be provided with the binocular camera in recess (4), the binocular camera includes first camera (6) and second camera (7), be provided with on the recess (4) inner wall of first camera (6) one side and clean the mechanism, it includes supporting seat (8) to clean the mechanism, supporting seat (8) set up recess (4) inner wall, be provided with first motor (9) on supporting seat (8), the output shaft of first motor (9) has telescopic link (10), telescopic link (10) are connected with and clean board (22), wipe board (22) surface coating and have chamois leather, chamois leather is used for wiping first camera (6), be provided with on recess (4) inner wall of second camera (7) one side and shelter from the mechanism, it includes second motor (11), output gear (12), drive gear (13), transfer line (14) and shielding plate (15) to shelter from the mechanism, output gear (12) with the output shaft coaxial coupling of second motor (11), drive gear (13) with transfer line (14) one end coaxial coupling, output gear (12) with drive gear (13) transmission is connected, shielding plate (15) with the transfer line (14) other end is connected, shielding plate (15) with second camera (7) are corresponding.
2. The multi-unmanned aerial vehicle event support auxiliary device according to claim 1, wherein a rotating guide rail (16) is arranged between the rotating disk (3) and the main body (2), an electric slider (17) is arranged on the rotating guide rail (16), and the rotating disk (3) is fixedly connected with the electric slider (17).
3. The multi-unmanned aerial vehicle event support auxiliary device as claimed in claim 1, wherein a support frame (18) is further arranged at the bottom of the body (2), an underframe (19) is fixedly mounted at the lower end of the support frame (18), and a plurality of reinforcing cross beams (20) are fixedly mounted between two adjacent groups of underframe (19).
4. A multi-unmanned aerial vehicle event support auxiliary device according to claim 3, wherein a side of the support frame (18) is provided with a crank arm (21), one end of the crank arm (21) is connected with the support frame (18), and the other end is connected with the bottom frame (19).
5. The multi-unmanned aerial vehicle event support auxiliary device of claim 4, wherein the underframe (19) and the reinforcing beam (20) form a trapezoidal frame, and thickened shock-absorbing rubber pads are arranged on the lower surfaces of the underframe (19) and the reinforcing beam (20).
6. The multi-unmanned aerial vehicle event support auxiliary device according to claim 1, wherein a controller is arranged inside the main body (2), the controller is electrically connected with the first motor (9) and used for controlling a wiping mechanism to wipe the first camera (6), and the controller is electrically connected with the second motor (11) and used for controlling a shielding mechanism to rotate.
7. The multi-unmanned-aerial-vehicle event support auxiliary device of claim 6, wherein a GPS positioning module is further arranged in the body (2), and the GPS positioning module is electrically connected with the controller.
8. The multi-unmanned aerial vehicle event support auxiliary device as claimed in any one of claims 1-7, wherein the number of the wings (1) is four, and the four wings (1) are symmetrically arranged on the top of the fuselage (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921792944.1U CN211033059U (en) | 2019-10-23 | 2019-10-23 | Many unmanned aerial vehicle event support auxiliary device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921792944.1U CN211033059U (en) | 2019-10-23 | 2019-10-23 | Many unmanned aerial vehicle event support auxiliary device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211033059U true CN211033059U (en) | 2020-07-17 |
Family
ID=71531237
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921792944.1U Expired - Fee Related CN211033059U (en) | 2019-10-23 | 2019-10-23 | Many unmanned aerial vehicle event support auxiliary device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211033059U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112389652A (en) * | 2020-11-20 | 2021-02-23 | 贵州师范大学 | Land use changes shoots and uses unmanned aerial vehicle with picture transmission function |
-
2019
- 2019-10-23 CN CN201921792944.1U patent/CN211033059U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112389652A (en) * | 2020-11-20 | 2021-02-23 | 贵州师范大学 | Land use changes shoots and uses unmanned aerial vehicle with picture transmission function |
| CN112389652B (en) * | 2020-11-20 | 2022-08-23 | 贵州师范大学 | Land use changes shoots and uses unmanned aerial vehicle with picture transmission function |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110899186B (en) | Unmanned aerial vehicle cleaning device, cleaning system, control method of unmanned aerial vehicle cleaning device and cleaning system, and storage medium | |
| CN105728398A (en) | Automatic flight surface cleaning robot for photovoltaic array | |
| CN211033059U (en) | Many unmanned aerial vehicle event support auxiliary device | |
| CN209220110U (en) | A kind of four-wheel suspension type high-altitude exterior wall perspex clean robot | |
| CN111361753A (en) | Unmanned aerial vehicle fixed cloud platform of taking photo by plane | |
| CN210100032U (en) | Airfield runway foreign matter detection and cleaning robot based on AR technology | |
| CN215043710U (en) | Environment emergency monitoring unmanned aerial vehicle | |
| CN215794502U (en) | A cloud platform elevating system for surveying and mapping unmanned aerial vehicle | |
| CN207301805U (en) | A kind of big visual angle unmanned plane for taking photo by plane | |
| CN212709970U (en) | Unmanned aerial vehicle inspection device | |
| CN207384192U (en) | Unmanned plane available for cleaning high-altitude glass | |
| CN202398569U (en) | Device for cleaning scanning equipment of automotive chassis | |
| CN214190143U (en) | Camera pod | |
| CN213892889U (en) | Optical lens for unmanned aerial vehicle | |
| CN115196006A (en) | Multifunctional surveying and mapping unmanned aerial vehicle for surveying and mapping geographic information | |
| CN112455682A (en) | Environment monitoring aircraft with remote monitoring function of shouting | |
| CN209174516U (en) | A kind of photovoltaic plant and glass curtain wall cleaning flight deduster | |
| CN218317374U (en) | Beyond visual range reconnaissance unmanned aerial vehicle | |
| CN220054138U (en) | Unmanned aerial vehicle for aerial photography and inspection | |
| CN213362904U (en) | Inspection and dust removal locomotive combined system for photo-thermal power station | |
| CN219790540U (en) | Infrared imaging inspection search and rescue unmanned aerial vehicle | |
| CN216887246U (en) | Multi-functional retractable unmanned aerial vehicle photoelectricity nacelle | |
| CN216981976U (en) | A dust removal defogging structure for aviation remote sensing camera | |
| CN211167453U (en) | Topographic surveying and mapping unmanned aerial vehicle | |
| CN216323511U (en) | Tunnel traffic safety early warning device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200717 Termination date: 20211023 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |