CN214420726U - Unmanned aerial vehicle landing gear for automatic power transmission inspection - Google Patents
Unmanned aerial vehicle landing gear for automatic power transmission inspection Download PDFInfo
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- CN214420726U CN214420726U CN202120213727.3U CN202120213727U CN214420726U CN 214420726 U CN214420726 U CN 214420726U CN 202120213727 U CN202120213727 U CN 202120213727U CN 214420726 U CN214420726 U CN 214420726U
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- 230000005611 electricity Effects 0.000 claims abstract description 5
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- 230000033228 biological regulation Effects 0.000 abstract description 2
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Abstract
The utility model relates to an unmanned air vehicle technique field specifically is an automatic unmanned aerial vehicle landing gear of patrolling and examining of transmitting electricity, including the base, the spout has been seted up to one side of base, and the inside of spout is rotated and is connected with the lead screw, and the one end of lead screw is rotated and is connected with first motor, and the outside threaded connection of lead screw has the slider, and the top fixedly connected with fixed block of slider, the inside of fixed block have splint through first electric putter swing joint. The utility model has the advantages that: through setting up the base, when using, place unmanned aerial vehicle on the loading board, then first electric putter drives splint and removes to fix unmanned aerial vehicle's undercarriage in the inside of fixed block, can accomplish the fixed to unmanned aerial vehicle, promote unmanned aerial vehicle's stability, be convenient for promote, and the position accessible slider of fixed block is adjusted, through the regulation to the slider promptly, makes the fixed block can fix the use to the undercarriage of different wide distances, hoisting device's practicality.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, especially an automatic unmanned aerial vehicle landing gear of patrolling and examining of transmission of electricity.
Background
Unmanned aircraft, commonly known as: unmanned planes, unmanned aerial vehicles, unmanned combat airplanes, and bee-type machines; the aerial photography is also called aerial photography, aerial photography or aerial photography, and refers to the earth landform shooting from the air to obtain a top view, namely an aerial image, the aerial photography camera can be controlled by a photographer and can also be automatically shot or remotely controlled, the used platform comprises a helicopter, a multi-axis aircraft, a fire balloon, a small airship, a rocket, a kite, a parachute and the like, the aerial image can clearly express the geographical form, so the aerial photography image is also applied to the aspects of military affairs, traffic construction, hydraulic engineering, ecological research, urban planning and the like besides being used as a ring of photography art, wherein the unmanned aerial vehicle specially used for electric power inspection has larger volume, generally performs inspection work mainly aiming at external high-voltage cables during inspection, and often needs to manually lift the unmanned aerial vehicle to take off after the unmanned aerial vehicle takes off in operation, unmanned aerial vehicle heavier, be not convenient for the manual work to lift unmanned aerial vehicle, consequently, be provided with promotion unmanned aerial vehicle such as shallow usually, promote unmanned aerial vehicle to take off the position after, take off unmanned aerial vehicle after moving, but there is not stable relation of connection between unmanned aerial vehicle and the shallow, the ground in the outskirts is mostly rugged and uneven, when promoting the shallow removal unmanned aerial vehicle, easily make unmanned aerial vehicle from the shallow landing, and unmanned aerial vehicle is when descending, the ground in the outskirts is mostly rugged and uneven, when descending, unmanned aerial vehicle has certain decline impulsive force, often can make unmanned aerial vehicle take place to incline askew circumstances such as topple after ground contact with rugged and uneven, be unfavorable for unmanned aerial vehicle's descending work, in order to solve above-mentioned problem, provide a transmission of electricity and patrol and examine and use unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to overcome prior art's shortcoming, provide an automatic unmanned aerial vehicle landing gear of patrolling and examining of transmitting electricity.
The purpose of the utility model is realized through the following technical scheme: an unmanned aerial vehicle landing gear for automatic power transmission inspection comprises a base, wherein a sliding groove is formed in one side of the base, a lead screw is rotatably connected inside the sliding groove, one end of the lead screw is rotatably connected with a first motor, the first motor is fixedly connected to one side of the base, a sliding block is in threaded connection with the outer portion of the lead screw, a fixed block is fixedly connected to the top of the sliding block, a first electric push rod is fixedly connected to one side of the fixed block, and a clamping plate is movably connected inside the fixed block through the first electric push rod;
the connecting groove is formed in one side of the base, a spring is fixedly connected to the inside of the connecting groove, a connecting block is movably connected to the inside of the connecting groove, a bearing plate is fixedly connected to one side of the connecting block, a groove is formed in the base, a second electric push rod is arranged in the groove, a second motor is arranged at one end of the second electric push rod, a first fixture block is connected to one end of the second motor in a rotating mode, a second fixture block is fixedly connected to one side of the bearing plate, and a through groove is formed in the bearing plate.
Optionally, one side of base is provided with the wheelset, the quantity of wheelset is four, four wheelset circumference array is in the bottom of base, one side of base is provided with the pull ring.
Optionally, the number of the sliding blocks is two, the two sliding blocks are symmetrically arranged inside the sliding groove, the shape and the size of the sliding blocks are matched with those of the sliding groove, the sliding blocks are movably connected inside the sliding groove, threaded holes are formed in the sliding blocks, the screw rod is connected inside the sliding blocks through threaded holes in a threaded mode, and the screw rod is driven to move in the sliding groove after rotating.
Optionally, the shape and size of the connecting block are matched with the shape and size of the connecting groove, the connecting block is movably connected inside the connecting groove through a spring, and the connecting block can slide inside the connecting groove.
Optionally, the shape and size of the first fixture block are matched with the shape and size of the inside of the second fixture block, and the first fixture block is located inside the second fixture block.
Optionally, the shape and size of the bearing plate are matched with the shape and size of the base, and the bearing plate is located at the top of the base.
The utility model has the advantages of it is following:
1. by arranging the base, a sliding groove is formed in one side of the base, a lead screw is rotatably connected in the sliding groove, one end of the lead screw is rotatably connected with a first motor, the first motor is fixedly connected to one side of the base, a sliding block is connected to the outer thread of the lead screw, a fixing block is fixedly connected to the top of the sliding block, a first electric push rod is fixedly connected to one side of the fixing block, a clamping plate is movably connected to the inside of the fixing block through the first electric push rod, when the unmanned aerial vehicle is used, the unmanned aerial vehicle is placed on the bearing plate, then the first electric push rod drives the clamping plate to move, so that the undercarriage of the unmanned aerial vehicle is fixed in the fixing block, the fixing of the unmanned aerial vehicle can be completed, the stability of the unmanned aerial vehicle is improved, the unmanned aerial vehicle is convenient to push, the position of the fixing block can be adjusted through the sliding block, when the unmanned aerial vehicle is adjusted, the lead screw is driven to rotate through the first motor, so that the sliding block is driven to move in the sliding groove, can accomplish and adjust the slider, through the regulation to the slider promptly, make the fixed block can fix the use, hoisting device's practicality to the undercarriage of different wide distances.
2. By arranging the bearing plate, one side of the base is provided with a connecting groove, the inside of the connecting groove is fixedly connected with a spring, the inside of the connecting groove is movably connected with a connecting block, one side of the connecting block is fixedly connected with the bearing plate, the inside of the base is provided with a groove, the inside of the groove is provided with a second electric push rod, one end of the second electric push rod is provided with a second motor, one end of the second motor is rotatably connected with a first fixture block, one side of the bearing plate is fixedly connected with a second fixture block, the inside of the bearing plate is provided with a through groove, when the unmanned aerial vehicle descends, the second motor drives the first fixture block to rotate, so that the first fixture block is separated from the second fixture block, the bearing plate is popped out under the action of the spring, when the unmanned aerial vehicle descends, the unmanned aerial vehicle firstly contacts with the bearing plate, the bearing plate absorbs the descending impulsive force of the unmanned aerial vehicle under the action of the spring, and the bearing plate is used as a platform for the unmanned aerial vehicle to descend, its surfacing and accessible spring absorb the impulsive force, and the unmanned aerial vehicle of being convenient for descends work.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic cross-sectional view of a first view of the present invention;
fig. 3 is a schematic cross-sectional view of a second perspective of the present invention;
FIG. 4 is a schematic structural view of the base of the present invention;
fig. 5 is a schematic structural view of the loading plate of the present invention.
In the figure: 1-base, 2-sliding groove, 3-screw rod, 4-first motor, 5-sliding block, 6-fixed block, 7-first electric push rod, 8-clamping plate, 9-connecting groove, 10-spring, 11-connecting block, 12-bearing plate, 13-groove, 14-second electric push rod, 15-second motor, 16-first fixture block, 17-second fixture block, 18-through groove, 19-wheel set and 20-pull ring.
Detailed Description
The invention will be further described with reference to the accompanying drawings, but the scope of the invention is not limited to the following description.
As shown in fig. 1-5, an unmanned aerial vehicle landing gear for automatic power transmission inspection comprises a base 1, a chute 2 is formed in one side of the base 1, a lead screw 3 is rotatably connected to the inside of the chute 2, a first motor 4 is rotatably connected to one end of the lead screw 3, the first motor 4 is fixedly connected to one side of the base 1, a slider 5 is in threaded connection with the outside of the lead screw 3, a fixed block 6 is fixedly connected to the top of the slider 5, a first electric push rod 7 is fixedly connected to one side of the fixed block 6, a clamping plate 8 is movably connected to the inside of the fixed block 6 through the first electric push rod 7, when the unmanned aerial vehicle landing gear is used, the unmanned aerial vehicle is placed on a bearing plate 12, then the first electric push rod 7 drives the clamping plate 8 to move, so that the landing gear of the unmanned aerial vehicle is fixed inside the fixed block 6, the fixation of the unmanned aerial vehicle can be completed, the stability of the unmanned aerial vehicle is improved, and the unmanned aerial vehicle is convenient to push, the position of the fixed block 6 can be adjusted through the slide block 5, and when the adjustment is performed, the first motor 4 drives the screw rod 3 to rotate, so that the slide block 5 is driven to move in the chute 2, the adjustment of the slide block 5 can be completed, namely, the fixed block 6 can be fixedly used for landing gears with different widths through the adjustment of the slide block 5, and the practicability of the device is improved;
one side of the base 1 is provided with a connecting groove 9, the inside of the connecting groove 9 is fixedly connected with a spring 10, the inside of the connecting groove 9 is movably connected with a connecting block 11, one side of the connecting block 11 is fixedly connected with a bearing plate 12, the inside of the base 1 is provided with a groove 13, the inside of the groove 13 is provided with a second electric push rod 14, one end of the second electric push rod 14 is provided with a second motor 15, one end of the second motor 15 is rotatably connected with a first fixture block 16, one side of the bearing plate 12 is fixedly connected with a second fixture block 17, the inside of the bearing plate 12 is provided with a through groove 18, when the unmanned aerial vehicle lands, the second motor 15 drives the first fixture block 16 to rotate, so that the first fixture block 16 is separated from the second fixture block 17, the bearing plate 12 is popped out under the action of the spring 10, when the unmanned aerial vehicle lands, the unmanned aerial vehicle firstly contacts with the bearing plate 12, the descending impulsive force of the unmanned aerial vehicle is absorbed by the bearing plate 12 under the action of the spring 10, and loading board 12 is as unmanned aerial vehicle's descending platform, and its surfacing and accessible spring 10 absorb the impulsive force, and the unmanned aerial vehicle of being convenient for descends work.
As an optimal technical solution of the utility model: one side of the base 1 is provided with four wheel sets 19, the number of the wheel sets 19 is four, four wheel sets 19 are circumferentially arrayed at the bottom of the base 1, one side of the base 1 is provided with a pull ring 20, the number of the sliding blocks 5 is two, the two sliding blocks 5 are symmetrically arranged inside the sliding groove 2, after the screw rod 3 rotates, the two sliding blocks 5 are driven to simultaneously approach to the central part of the base 1 or move away from the central part, the shape and size of the sliding blocks 5 are matched with the shape and size of the sliding groove 2, the sliding blocks 5 are movably connected inside the sliding groove 2, the sliding blocks 5 are internally provided with threaded holes, the screw rod 3 is in threaded connection inside the sliding blocks 5 through the threaded holes, the shape and size of the connecting block 11 is matched with the shape and size of the connecting groove 9, the connecting block 11 is movably connected inside the connecting groove 9 through a spring 10, the shape and size of the first clamping block 16 is matched with the shape and size inside the second clamping block 17, the first fixture block 16 is located inside the second fixture block 17, the shape and size of the bearing plate 12 are matched with the shape and size of the base 1, and the bearing plate 12 is located on the top of the base 1.
The working process of the utility model is as follows: when the unmanned aerial vehicle landing device is used, the unmanned aerial vehicle is placed on the bearing plate 12, then the first electric push rod 7 drives the clamping plate 8 to move, so that the landing gear of the unmanned aerial vehicle is fixed inside the fixing block 6, the fixing of the unmanned aerial vehicle can be completed, the position of the fixing block 6 can be adjusted through the sliding block 5, when the unmanned aerial vehicle is adjusted, the first motor 4 drives the screw rod 3 to rotate, so that the sliding block 5 is driven to move in the sliding groove 2, the adjustment of the sliding block 5 can be completed, namely, the fixing block 6 can be used for fixing the landing gears with different widths through the adjustment of the sliding block 5, when the unmanned aerial vehicle lands, the second motor 15 drives the first fixture block 16 to rotate, so that the first fixture block 16 is separated from the second fixture block 17, the bearing plate 12 is popped up under the action of the spring 10, when the unmanned aerial vehicle lands, the unmanned aerial vehicle firstly contacts with the bearing plate 12, the bearing plate 12 absorbs the descending impulsive force of the unmanned aerial vehicle under the action of the spring 10, and bearing plate 12 is as unmanned aerial vehicle's landing platform, and its surperficial level and accessible spring 10 absorbs the impulsive force.
In conclusion, when the unmanned aerial vehicle landing gear for automatic power transmission inspection is used, the base 1 is arranged, the sliding groove 2 is formed in one side of the base 1, the screw rod 3 is rotatably connected inside the sliding groove 2, the first motor 4 is rotatably connected to one end of the screw rod 3, the first motor 4 is fixedly connected to one side of the base 1, the sliding block 5 is in threaded connection with the outer portion of the screw rod 3, the fixed block 6 is fixedly connected to the top of the sliding block 5, the first electric push rod 7 is fixedly connected to one side of the fixed block 6, the clamping plate 8 is movably connected to the inside of the fixed block 6 through the first electric push rod 7, when the unmanned aerial vehicle landing gear is used, the unmanned aerial vehicle is placed on the bearing plate 12, then the clamping plate 8 is driven by the first electric push rod 7 to move, so that the unmanned aerial vehicle landing gear is fixed inside the fixed block 6, the unmanned aerial vehicle can be fixed, the stability of the unmanned aerial vehicle is improved, and the unmanned aerial vehicle is convenient to push, the position of the fixed block 6 can be adjusted through the slide block 5, when adjusting, the screw rod 3 is driven to rotate through the first motor 4, so as to drive the slide block 5 to move in the chute 2, thus the adjustment of the slide block 5 can be completed, namely, the fixed block 6 can be fixedly used for landing gears with different widths through the adjustment of the slide block 5, the practicability of the lifting device is realized, through arranging the bearing plate 12, one side of the base 1 is provided with the connecting groove 9, the inside of the connecting groove 9 is fixedly connected with the spring 10, the inside of the connecting groove 9 is movably connected with the connecting block 11, one side of the connecting block 11 is fixedly connected with the bearing plate 12, the inside of the base 1 is provided with the groove 13, the inside of the groove 13 is provided with the second electric push rod 14, one end of the second electric push rod 14 is provided with the second motor 15, one end of the second motor 15 is rotatably connected with the first fixture block 16, one side of the bearing plate 12 is fixedly connected with the second fixture block 17, the through groove 18 has been seted up to the inside of loading board 12, when unmanned aerial vehicle descended, second motor 15 drove first fixture block 16 and rotates, make first fixture block 16 break away from second fixture block 17, make loading board 12 pop out under spring 10's effect, when unmanned aerial vehicle descended, unmanned aerial vehicle at first contacted with loading board 12, loading board 12 absorbs unmanned aerial vehicle's decline impulsive force under spring 10's effect, and loading board 12 is as unmanned aerial vehicle's landing platform, its surfacing and accessible spring 10 absorb the impulsive force, be convenient for unmanned aerial vehicle descends work.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an automatic unmanned aerial vehicle landing gear of patrolling and examining of transmitting electricity which characterized in that: the clamping device comprises a base (1), wherein a sliding groove (2) is formed in one side of the base (1), a lead screw (3) is rotatably connected to the inside of the sliding groove (2), one end of the lead screw (3) is rotatably connected with a first motor (4), the first motor (4) is fixedly connected to one side of the base (1), a sliding block (5) is connected to the outside of the lead screw (3) through threads, a fixed block (6) is fixedly connected to the top of the sliding block (5), a first electric push rod (7) is fixedly connected to one side of the fixed block (6), and a clamping plate (8) is movably connected to the inside of the fixed block (6) through the first electric push rod (7); connecting groove (9) have been seted up to one side of base (1), inside fixedly connected with spring (10) of connecting groove (9), the inside swing joint of connecting groove (9) has connecting block (11), one side fixedly connected with loading board (12) of connecting block (11), recess (13) have been seted up to the inside of base (1), the inside of recess (13) is provided with second electric putter (14), the one end of second electric putter (14) is provided with second motor (15), the one end of second motor (15) is rotated and is connected with first fixture block (16), one side fixedly connected with second fixture block (17) of loading board (12), through groove (18) have been seted up to the inside of loading board (12).
2. An unmanned aerial vehicle landing gear for automatic inspection of power transmission according to claim 1, characterized in that: one side of base (1) is provided with wheelset (19), the quantity of wheelset (19) is four, four wheelset (19) circumference array is in the bottom of base (1), one side of base (1) is provided with pull ring (20).
3. An unmanned aerial vehicle landing gear for automatic inspection of power transmission according to claim 1, characterized in that: the quantity of slider (5) is two, two slider (5) symmetry sets up the inside at spout (2), the shape size of slider (5) and the shape size looks adaptation of spout (2), slider (5) swing joint is in the inside of spout (2), the threaded hole is seted up to the inside of slider (5), lead screw (3) are through the inside of screw hole threaded connection in slider (5).
4. An unmanned aerial vehicle landing gear for automatic inspection of power transmission according to claim 1, characterized in that: the shape and size of the connecting block (11) are matched with the shape and size of the connecting groove (9), and the connecting block (11) is movably connected inside the connecting groove (9) through a spring (10).
5. An unmanned aerial vehicle landing gear for automatic inspection of power transmission according to claim 1, characterized in that: the shape and size of the first fixture block (16) are matched with the shape and size of the interior of the second fixture block (17), and the first fixture block (16) is located inside the second fixture block (17).
6. An unmanned aerial vehicle landing gear for automatic inspection of power transmission according to claim 1, characterized in that: the bearing plate (12) is matched with the base (1) in shape and size, and the bearing plate (12) is located at the top of the base (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120213727.3U CN214420726U (en) | 2021-01-26 | 2021-01-26 | Unmanned aerial vehicle landing gear for automatic power transmission inspection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120213727.3U CN214420726U (en) | 2021-01-26 | 2021-01-26 | Unmanned aerial vehicle landing gear for automatic power transmission inspection |
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| Publication Number | Publication Date |
|---|---|
| CN214420726U true CN214420726U (en) | 2021-10-19 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202120213727.3U Expired - Fee Related CN214420726U (en) | 2021-01-26 | 2021-01-26 | Unmanned aerial vehicle landing gear for automatic power transmission inspection |
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| CN (1) | CN214420726U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118004475A (en) * | 2024-04-08 | 2024-05-10 | 国网山东省电力公司泰安供电公司 | Inspection unmanned aerial vehicle platform for detecting power faults |
-
2021
- 2021-01-26 CN CN202120213727.3U patent/CN214420726U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118004475A (en) * | 2024-04-08 | 2024-05-10 | 国网山东省电力公司泰安供电公司 | Inspection unmanned aerial vehicle platform for detecting power faults |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211019 |