CN115092393A - Unmanned aerial vehicle carries multi-target detection tracking laser appearance of removing obstacles - Google Patents
Unmanned aerial vehicle carries multi-target detection tracking laser appearance of removing obstacles Download PDFInfo
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- CN115092393A CN115092393A CN202210552619.8A CN202210552619A CN115092393A CN 115092393 A CN115092393 A CN 115092393A CN 202210552619 A CN202210552619 A CN 202210552619A CN 115092393 A CN115092393 A CN 115092393A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B7/00—Cleaning by methods not provided for in a single other subclass or a single group in this subclass
- B08B7/0035—Cleaning by methods not provided for in a single other subclass or a single group in this subclass by radiant energy, e.g. UV, laser, light beam or the like
- B08B7/0042—Cleaning by methods not provided for in a single other subclass or a single group in this subclass by radiant energy, e.g. UV, laser, light beam or the like by laser
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/06—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/18—Heads with mechanism for moving the apparatus relatively to the stand
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G1/00—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
- H02G1/02—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to an unmanned aerial vehicle airborne multi-target detection tracking laser obstacle clearing instrument which comprises an unmanned aerial vehicle body, a laser and an aiming camera, wherein the unmanned aerial vehicle body comprises a shell, the lower surface of the shell is fixedly connected with an electric telescopic rod, a circumferential rotating mechanism is arranged on the electric telescopic rod, an angle adjusting mechanism for mounting the laser is arranged on the circumferential rotating mechanism, and the aiming camera is arranged on the laser; the invention has the advantages that: install the laser instrument on the angle adjustment mechanism that the circumferential direction mechanism went up to set up, consequently, can realize angle adjustment mechanism's circular motion under circumferential direction mechanism's effect, thereby avoided the laser instrument and aimed the camera and to the problem that transmission line surface foreign matter can not be surveyed and traced and take place, and circumferential direction mechanism passes through electric telescopic handle and sets up on the casing of unmanned aerial vehicle body, consequently, can realize that circumferential direction mechanism realizes the lift action along unmanned aerial vehicle's vertical direction under electric telescopic handle's effect, thereby can adapt to the overhead line under the different environment.
Description
Technical Field
The invention relates to an unmanned aerial vehicle airborne multi-target detection tracking laser obstacle clearing instrument.
Background
An overhead line in a power grid mainly refers to an overhead open line, is erected above the ground and is a power transmission line for transmitting electric energy by fixing a transmission conductor on a tower erected on the ground through an insulator. Along with the action of air flow and wind, foreign matters (such as common kites, ribbons, advertising cloth, hemp ropes, kite lines and fish lines) along the overhead line are hung on the wire, so that tripping caused by line grounding and interphase short circuit is very easy to occur, and the tripping of the power transmission line is also caused by long sagging of bird nest straws near the cross arm of the iron tower, so that the power transmission line needs to be patrolled and cleared.
Obstacles in the power transmission network adopt the manual work to blow fire towards obstacle department and clear up the obstacles mostly, the obstacle clearance is lower, high in labor strength, and can cause the damage of conflagration hidden danger and power transmission network, and carry the obstacle through unmanned aerial vehicle and can reduce operating personnel's intensity of labour, unmanned aerial vehicle technique of flaming clears up the application of foreign matter at 110kV transmission line, whole operation process 15min, only need 2 ~ 4 operating personnel, this technique of clearing up is convenient and fast, but very easily causes the conflagration, there is certain potential safety hazard.
Among the prior art, unmanned aerial vehicle can only realize realizing the work of removing obstacles of laser of surveying the tracking to single target, so, when a plurality of target foreign matters appear around the same position in the power transmission network, current unmanned aerial vehicle can only realize removing obstacles to a plurality of target foreign matters of different angles in turn, but this mode of removing obstacles is not only long consuming time, and it is inefficient to remove obstacles, and long-time work has also increaseed unmanned aerial vehicle's electric quantity loss moreover, and then is difficult to guarantee whole equipment's stable use.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle airborne multi-target detection tracking laser obstacle clearing instrument, which can realize the circumferential rotation of the whole device during obstacle clearing and ensure the effect of detecting, tracking and positioning foreign matters on the surface of a line.
In order to solve the technical problems, the invention is realized by the following technical scheme: an unmanned aerial vehicle airborne multi-target detection tracking laser obstacle clearance instrument comprises an unmanned aerial vehicle body, a laser and an aiming camera, wherein the unmanned aerial vehicle body comprises a shell, an electric telescopic rod is fixedly connected to the lower surface of the shell, a circumferential rotating mechanism is arranged on the electric telescopic rod, an angle adjusting mechanism for mounting the laser is arranged on the circumferential rotating mechanism, the aiming camera is arranged on the laser, a laser head of the laser and a camera head of the aiming camera are located on the same vertical plane, and a second driving motor for driving the laser to swing and a third driving motor for driving the laser to rotate circumferentially are arranged on the angle adjusting mechanism; the two sides of the shell are provided with buffer mechanisms, each buffer mechanism comprises a cushion block and a buffer spring, and the buffer springs are arranged in the cushion blocks.
Preferably, the circumferential direction mechanism includes a drive motor and a connecting plate, electric telescopic handle includes the piston rod, a drive motor fixed connection is on the piston rod, the connecting plate sets up on a drive motor, the piston rod is flexible to be driven a drive motor realizes the lift action along the vertical direction of unmanned aerial vehicle body, a drive motor drive connecting plate realizes circular motion.
Preferably, a first coupling is arranged on the first driving motor, a first transmission shaft of the connecting plate is arranged on the first coupling, and the connecting plate is a cross-shaped connecting plate.
Preferably, angle adjustment mechanism includes base, swing board and rotates the bull stick of connection on swing board, swing board rotates and connects on the base, second driving motor sets up on the base and links to each other with swing board, third driving motor establishes on the base and links to each other with the bull stick, the laser instrument sets up on the bull stick.
Preferably, the base includes mounting panel, first fixed plate and second fixed plate, the mounting panel sets up the lower surface at the connecting plate, first fixed plate and second fixed plate all set up on the mounting panel between second driving motor and third driving motor, the one end of swing board is equipped with the axis of rotation, the axis of rotation passes through the bearing to be fixed on first fixed plate, be equipped with the second transmission shaft that links to each other with the bull stick on the swing board, the second transmission shaft extends to and links to each other with third driving motor after on the second fixed plate.
Preferably, a second coupler connected with the rotating shaft is arranged on the second driving motor, a third coupler connected with the second transmission shaft is arranged on the third driving motor, a gear assembly is arranged between the second transmission shaft and the rotating rod, and the gear assembly comprises a first bevel gear and a second bevel gear which are meshed with each other.
Preferably, the base further comprises a first mounting seat and a second mounting seat, the first mounting seat and the second mounting seat are fixed on the lower surface of the mounting plate through bolts, the second driving motor is fixedly connected to the lower surface of the first mounting seat, and the third driving motor is fixedly mounted on the lower surface of the second mounting seat.
Preferably, the buffer mechanism comprises support rods arranged on two sides of the shell, and the cushion blocks are fixedly arranged at the bottom ends of the support rods.
Preferably, the inside of cushion is equipped with the cushion chamber, buffer spring fixed mounting is at the interior roof of cushion chamber, the buffer hole has been seted up to the inner bottom wall of cushion chamber, the buffer block has been cup jointed in the inner wall slip of buffer hole, buffer spring is connected with the last fixed surface of buffer block.
Preferably, the lower fixed surface of buffer block installs the buffer layer, the interior roof fixed mounting of cushion chamber has limit switch, the last surface mounting of buffer block has the trigger bar, the trigger bar contacts with limit switch's trigger end, limit switch and unmanned aerial vehicle body electric connection.
In conclusion, the invention has the advantages that: install the laser instrument on the angle adjustment mechanism that circumferential direction mechanism set up, consequently, can realize angle adjustment mechanism's circular motion under circumferential direction mechanism's effect, thereby avoided laser instrument and aiming camera to the problem emergence that transmission line surface foreign matter can't be surveyed and can't be followed tracks of, obstacle clearing quality is further improved, and circumferential direction mechanism passes through electric telescopic handle and sets up on the casing of unmanned aerial vehicle body, consequently, can realize circumferential direction mechanism and realize the lift action along unmanned aerial vehicle's vertical direction under electric telescopic handle's effect, thereby can adapt to the overhead line under the different environment, the stability of whole laser obstacle clearing appearance has been ensured, secondly, because be equipped with the second driving motor that the drive laser instrument does the swing motion on the angle adjustment mechanism, and the third driving motor that the drive laser instrument does circumferential direction, consequently the laser instrument realizes bowing under the effect of second driving motor, The adjustment of the elevation angle realizes the adjustment of the circumferential direction under the action of the third driving motor, thereby realizing the multi-angle adjustment of the laser, being convenient for the detection and tracking of multi-target foreign matters, solving the problem that the existing unmanned aerial vehicle can only realize the laser obstacle clearance work of realizing the detection and tracking of a single target, the aiming camera is arranged on the laser, and the laser head of the laser and the camera of the aiming camera are positioned on the same vertical plane, so that the aiming camera can be used as the main vision when in use, is used for assisting the special laser to aim and position the target foreign body, and finally the buffer mechanism is set into a structure of a cushion block and a buffer spring, which can control the cushion block to contact with the ground when the unmanned aerial vehicle body lands, because be equipped with buffer spring in the cushion, consequently the elasticity through buffer spring slows down the impact force that unmanned aerial vehicle descending produced to unmanned aerial vehicle body safety descending's effect has been guaranteed.
Drawings
The invention is further described below with reference to the accompanying drawings:
fig. 1 is a schematic structural diagram of an airborne multi-target detection tracking laser obstacle clearing instrument of an unmanned aerial vehicle;
FIG. 2 is a schematic view of the structure of an angle adjustment mechanism on an electric telescopic rod according to the present invention;
FIG. 3 is a schematic structural view of a connecting plate according to the present invention;
FIG. 4 is a schematic structural view of an angle adjustment mechanism according to the present invention;
FIG. 5 is a schematic view of the construction of the swing plate of the present invention;
FIG. 6 is a schematic view of the structure of the spacer of the present invention.
Reference numerals:
1 unmanned aerial vehicle body, 2 electric telescopic handle, 3 first driving motor, 31 first transmission shaft, 4 connecting plates, 5 second driving motor, 51 mounting panel, 52 first mount pad, 53 second mount pad, 54 swinging plates, 55 second transmission shaft, 56 first fixed plate, 57 second fixed plate, 58 first bevel gear, 59 bull stick, 510 second bevel gear, 6 third driving motor, 7 laser instrument, 8 aim camera, 9 cushion blocks, 91 bracing piece, 92 cushion chamber, 93 cushion holes, 94 cushion blocks, 95 cushion layers, 96 limit switch, 97 trigger lever, 10 buffer spring.
Detailed Description
As shown in fig. 1, 2, 3, 4, 5 and 6, an airborne multi-target detection tracking laser obstacle clearance device for an unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a laser 7 and a sighting camera 8, wherein the unmanned aerial vehicle body 1 comprises a shell, an electric telescopic rod 2 is fixedly connected to the lower surface of the shell, a circumferential rotating mechanism is arranged on the electric telescopic rod 2, and an angle adjusting mechanism for mounting the laser is arranged on the circumferential rotating mechanism; aim camera 8 and set up on laser instrument 7, just the laser head of laser instrument 7 and the camera of aiming camera 8 are located same vertical plane, be equipped with the second driving motor 5 that swing motion was done to drive laser instrument 7 on the angle adjustment mechanism to and drive laser instrument 7 is circumferential direction's third driving motor 6, the both sides of casing are equipped with buffer gear, buffer gear includes cushion 9 and buffer spring 10, buffer spring 10 sets up in cushion 9.
Install the laser instrument on the angle adjustment mechanism that circumferential direction mechanism set up, consequently can realize angle adjustment mechanism's circular motion under circumferential direction mechanism's effect, thereby avoided the laser instrument and aimed camera to the problem that transmission line surface foreign matter can not be surveyed and traced and taken place, the quality of removing obstacles is further improved, and circumferential direction mechanism passes through electric telescopic handle and sets up on the casing of unmanned aerial vehicle body, consequently can realize circumferential direction mechanism along unmanned aerial vehicle's vertical direction and realize the lift action under electric telescopic handle's effect, thereby can adapt to the overhead line under the different environment, the stability of whole laser removing obstacles appearance has been ensured, secondly, because be equipped with the second driving motor that the drive laser instrument does the swing motion on the angle adjustment mechanism, and the third driving motor that the drive laser instrument does circumferential direction, therefore the laser instrument realizes bowing under the effect of second driving motor, The adjustment of the elevation angle realizes the adjustment of the circumferential direction under the action of the third driving motor, thereby realizing the multi-angle adjustment of the laser, being convenient for the detection and tracking of multi-target foreign matters, solving the problem that the existing unmanned aerial vehicle can only realize the laser obstacle clearance work of realizing the detection and tracking of a single target, the aiming camera is arranged on the laser, and the laser head of the laser and the camera of the aiming camera are positioned on the same vertical plane, so that the aiming camera can be used as the main vision when in use, is used for assisting the special laser to aim and position the target foreign body, and finally the buffer mechanism is set into a structure of a cushion block and a buffer spring, which can control the cushion block to contact with the ground when the unmanned aerial vehicle body lands, because be equipped with buffer spring in the cushion, consequently the elasticity through buffer spring slows down the impact force that unmanned aerial vehicle descending produced to unmanned aerial vehicle body safety descending's effect has been guaranteed.
The circumferential rotating mechanism comprises a first driving motor 3 and a connecting plate 4, the electric telescopic rod 2 comprises a piston rod, the first driving motor is fixedly connected to the piston rod, the connecting plate is arranged on the first driving motor, the piston rod stretches and retracts to drive the first driving motor to realize lifting action along the vertical direction of the unmanned aerial vehicle body, the first driving motor drives the connecting plate to realize circular motion, the connecting plate increases the installation area of the angle adjusting mechanism and ensures the stability of the angle adjusting mechanism, a first coupler is arranged on the first driving motor 3, a first transmission shaft 31 of the connecting plate 4 is arranged on the first coupler, the connecting plate 4 is a cross-shaped connecting plate, the first coupler and the first transmission shaft 31 can quickly realize the connection between the connecting plate 4 and the first driving motor 3, and the connecting plate 4 is arranged into a cross-shaped connecting plate, on the one hand can reduce the weight of connecting plate 4, guarantee the stability of 1 flight of unmanned aerial vehicle body, on the other hand, cross connecting plate makes the tip at connecting plate 4 of installing of each angle adjustment mechanism mutual independence, enables the even distribution of angle adjustment mechanism moreover on connecting plate 4, has ensured the stability of connecting plate 4 laser head when circumferential direction.
The angle adjusting mechanism comprises a base, a swinging plate 54 and a rotating rod 59 rotatably connected to the swinging plate 54, the swinging plate 54 is rotatably connected to the base, the second driving motor 5 is arranged on the base and connected with the swinging plate 54, the third driving motor 6 is arranged on the base and connected with the rotating rod 59, the laser 7 is arranged on the rotating rod 59, the aiming camera 8 is arranged on the lower surface of the laser 7, the angle adjusting mechanism is arranged into a structure of the base, the swinging plate 54 and the rotating rod 59, when the angle adjusting mechanism is used, the second driving motor 5 rotates to drive the swinging plate 54 to rotate, the rotating rod 59 is arranged on the swinging plate 54, therefore, the swinging plate 54 can drive the laser 7 on the rotating rod 59 to synchronously rotate, the third driving motor 6 rotates to drive the rotating rod 59 to rotate, so that the laser 7 synchronously rotates along with the rotating rod 59, and the rotating rod 59 and the swinging plate 54 are independent, the swing plate 54 and the rotating rod 59 can be driven to rotate simultaneously, so that the device is suitable for different angle adjusting requirements and different obstacle clearing environments.
The base comprises a mounting plate 51, a first fixing plate 56 and a second fixing plate 57, the mounting plate 51 is arranged on the lower surface of the connecting plate 4, the first fixing plate 56 and the second fixing plate 57 are both arranged on the mounting plate 51 between the second driving motor 5 and the third driving motor 6, one end of the swinging plate 54 is provided with a rotating shaft which is fixed on the first fixing plate 56 through a bearing, the swinging plate 54 is provided with a second transmission shaft 55, a gear assembly is arranged between the second transmission shaft 55 and a rotating rod 59, the second transmission shaft 55 extends to the second fixing plate 57 and then is connected with the third driving motor 6, the mounting plate 51 can increase the contact area between the base and the connecting plate 4, the fixing quality of the whole base on the connecting plate 4 is ensured, the arrangement of the first fixing plate 56 and the second fixing plate 57 can respectively realize the rotation of the swinging rod and the second transmission shaft 55, secondly, a gear assembly is arranged between the second transmission shaft 55 and the rotating rod 59, so that the smooth transmission between the second transmission shaft 55 and the rotating rod 59 can be ensured, and the rotating speed of the rotating rod 59 can be controlled by adjusting the transmission ratio of the gear assembly when in use.
The second driving motor 5 is provided with a second coupler connected with the rotating shaft, the third driving motor 6 is provided with a third coupler connected with the second transmission shaft 55, the gear assembly comprises a first bevel gear 58 and a second bevel gear 510 which are meshed with each other, the first bevel gear 58 is arranged on the second transmission shaft 55, the second bevel gear 510 is arranged on the rotating rod 59, the second coupler can realize the reliability of the connection between the second driving motor 5 and the rotating shaft, the third coupler can realize the reliability of the connection between the third driving motor 6 and the second transmission shaft 55, the connection between the second transmission shaft 55 and the rotating rod 59 is realized through the meshing transmission of the first bevel gear 58 and the second bevel gear 510, and the circular motion of the rotating rod 59 is ensured. The base still includes first mount pad 52 and second mount pad 53, first mount pad 52 and second mount pad 53 all pass through the lower surface of bolt fastening at mounting panel 51, second driving motor 5 fixed connection is at the lower surface of first mount pad 52, third driving motor 6 fixed mounting is at the lower surface of second mount pad 53, can realize that second driving motor 5 and third driving motor 6 are mutually independent to install on mounting panel 51.
Buffer gear is including installing the bracing piece 91 in the casing both sides, 9 fixed mounting in the bottom of bracing piece 91 of cushion, in this embodiment, make unmanned aerial vehicle body 1 when the level is placed, can play certain supporting role to it through bracing piece 91 and cushion 9. Secondly, cushion 9's inside is equipped with cushion chamber 92, buffer spring 10 fixed mounting is at the interior roof of cushion chamber 92, buffer hole 93 has been seted up to cushion chamber 92's interior diapire, buffer block 94 has been cup jointed in the inner wall slip of buffer hole 93, buffer spring 10 is connected with the last fixed surface of buffer block 94, and the setting of buffer hole 93 can guarantee the gliding straightness accuracy of buffer block 94 in cushion 9, guarantees the stationarity of buffer spring 10 compression. Finally, buffer block 94's lower fixed surface installs buffer layer 95, the interior roof fixed mounting of cushion chamber 92 has limit switch 96, buffer block 94's last surface mounting has trigger bar 97, trigger bar 97 and limit switch 96's trigger end contact, limit switch 96 and unmanned aerial vehicle body 1 electric connection, in this embodiment, unmanned aerial vehicle body 1 is descending the in-process, and buffer spring 10 drives buffer block 94 upwards to slide in buffer hole 93 to make trigger bar 97 and limit switch 96 contact, unmanned aerial vehicle at this moment has descended safely.
The above description is only an embodiment of the present invention, but the technical features of the present invention are not limited thereto, and any changes or modifications within the technical scope of the present invention by those skilled in the art are covered by the present invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle machine carries multi-target and surveys tracking laser instrument of removing obstacles, includes the unmanned aerial vehicle body, the unmanned aerial vehicle body includes the casing, its characterized in that: the laser aiming device comprises a shell, and is characterized by further comprising a laser and an aiming camera, wherein an electric telescopic rod is fixedly connected to the lower surface of the shell, a circumferential rotating mechanism is arranged on the electric telescopic rod, an angle adjusting mechanism for mounting the laser is arranged on the circumferential rotating mechanism, the aiming camera is arranged on the laser, a laser head of the laser and a camera of the aiming camera are positioned on the same vertical plane, and a second driving motor for driving the laser to swing and a third driving motor for driving the laser to rotate circumferentially are arranged on the angle adjusting mechanism; the two sides of the shell are provided with buffer mechanisms, each buffer mechanism comprises a cushion block and a buffer spring, and the buffer springs are arranged in the cushion blocks.
2. The unmanned aerial vehicle machine carries multi-target detection tracking laser instrument of removing obstacles of claim 1, its characterized in that: circumferential direction mechanism includes a driving motor and connecting plate, electric telescopic handle includes the piston rod, a driving motor fixed connection is on the piston rod, the connecting plate sets up on a driving motor, the flexible drive of piston rod a driving motor realizes the lift action along the vertical direction of unmanned aerial vehicle body, a driving motor drives the connecting plate and realizes circular motion.
3. The unmanned aerial vehicle machine carries multi-target detection tracking laser obstacle clearing appearance of claim 2, characterized in that: the first driving motor is provided with a first coupler, a first transmission shaft of a connecting plate is installed on the first coupler, and the connecting plate is a cross-shaped connecting plate.
4. The unmanned aerial vehicle machine carries multi-target detection tracking laser obstacle clearing appearance of claim 2, characterized in that: the angle adjusting mechanism comprises a base, a swinging plate and a rotating rod connected to the swinging plate in a rotating mode, the swinging plate is connected to the base in a rotating mode, the second driving motor is arranged on the base and connected with the swinging plate, the third driving motor is arranged on the base and connected with the rotating rod, and the laser is arranged on the rotating rod.
5. The unmanned aerial vehicle machine carries multi-target detection tracking laser obstacle clearing appearance of claim 4, characterized in that: the base includes mounting panel, first fixed plate and second fixed plate, the mounting panel sets up the lower surface at the connecting plate, first fixed plate and second fixed plate all set up on the mounting panel between second driving motor and third driving motor, the one end of swing board is equipped with the axis of rotation, the axis of rotation passes through the bearing to be fixed on first fixed plate, be equipped with the second transmission shaft that links to each other with the bull stick on the swing board, the second transmission shaft extends to and links to each other with third driving motor after on the second fixed plate.
6. The unmanned aerial vehicle machine carries multi-target detection tracking laser obstacle clearing appearance of claim 5, characterized in that: the driving mechanism is characterized in that a second coupler connected with the rotating shaft is arranged on the second driving motor, a third coupler connected with the second transmission shaft is arranged on the third driving motor, a gear assembly is arranged between the second transmission shaft and the rotating rod, and the gear assembly comprises a first bevel gear and a second bevel gear which are meshed with each other.
7. The unmanned aerial vehicle machine carries multi-target and surveys tracking laser appearance of removing obstacles of claim 6, its characterized in that: the base still includes first mount pad and second mount pad, first mount pad and second mount pad are all through the lower surface of bolt fastening at the mounting panel, second driving motor fixed connection is at the lower surface of first mount pad, third driving motor fixed mounting is at the lower surface of second mount pad.
8. The unmanned aerial vehicle machine carries multi-target detection tracking laser instrument of removing obstacles of claim 1, its characterized in that: the buffer mechanism comprises support rods arranged on two sides of the shell, and the cushion blocks are fixedly arranged at the bottom ends of the support rods.
9. The unmanned aerial vehicle machine carries multi-target detection tracking laser instrument of removing obstacles of claim 8, its characterized in that: the inside of cushion is equipped with the cushion chamber, buffer spring fixed mounting is at the interior roof of cushion chamber, the buffer hole has been seted up to the inner bottom wall of cushion chamber, the buffer block has been cup jointed in the inner wall slip of buffer hole, buffer spring is connected with the last fixed surface of buffer block.
10. The unmanned aerial vehicle machine carries multi-target detection tracking laser obstacle clearing appearance of claim 9, characterized in that: the lower fixed surface of buffer block installs the buffer layer, the interior roof fixed mounting of cushion chamber has limit switch, the last surface mounting of buffer block has the trigger bar, the trigger bar contacts with limit switch's trigger end, limit switch and unmanned aerial vehicle body electric connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210552619.8A CN115092393A (en) | 2022-05-19 | 2022-05-19 | Unmanned aerial vehicle carries multi-target detection tracking laser appearance of removing obstacles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210552619.8A CN115092393A (en) | 2022-05-19 | 2022-05-19 | Unmanned aerial vehicle carries multi-target detection tracking laser appearance of removing obstacles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN115092393A true CN115092393A (en) | 2022-09-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210552619.8A Pending CN115092393A (en) | 2022-05-19 | 2022-05-19 | Unmanned aerial vehicle carries multi-target detection tracking laser appearance of removing obstacles |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN115092393A (en) |
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2022
- 2022-05-19 CN CN202210552619.8A patent/CN115092393A/en active Pending
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