CN220640247U - Vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle - Google Patents
Vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle Download PDFInfo
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- CN220640247U CN220640247U CN202321448298.3U CN202321448298U CN220640247U CN 220640247 U CN220640247 U CN 220640247U CN 202321448298 U CN202321448298 U CN 202321448298U CN 220640247 U CN220640247 U CN 220640247U
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- 238000007689 inspection Methods 0.000 title claims abstract description 26
- 238000009434 installation Methods 0.000 claims abstract description 7
- 230000000007 visual effect Effects 0.000 claims abstract description 6
- 238000003331 infrared imaging Methods 0.000 abstract description 15
- 230000002411 adverse Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, and discloses a vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle which comprises a machine body, wherein an installation box is fixedly connected to the end face of the bottom of the machine body, and a clamping assembly is fixedly connected to the installation box. The handle is twisted to drive the rotating shaft and the bevel gear threaded rod to rotate, further drive the threaded sleeve and the slide bar to move up and down, loose the butt of the triangular block, and move the triangular block and the clamping block to one side far away from the connecting piece under the action of the spring and the telescopic rod, so that the connecting piece can be installed and detached. When the connecting piece is installed, the handle is reversely twisted, so that the clamping block and the connecting piece can be clamped. The visual light camera can patrol the power equipment and the surrounding environment, when encountering power line faults, the visual light camera can be disassembled by twisting the handle, then the infrared imaging instrument is installed, and after the infrared imaging instrument is installed, the handle is reversely twisted, so that the clamping block and the connecting piece can be clamped, and the installation of the infrared imaging instrument is realized.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle.
Background
The power inspection refers to ensuring safe and reliable operation of a power system by inspecting, detecting and maintaining power equipment, circuits and the like. The traditional electric power inspection mode mainly comprises manual inspection, and the mode has the problems of high labor cost, low efficiency, high safety risk and the like.
Compared with the traditional power inspection mode, the unmanned aerial vehicle can fly quickly, the power line, the transformer substation and the like are subjected to all-dimensional inspection without dead angles, the inspection efficiency is greatly improved, and the time cost is saved. Meanwhile, the danger and risk possibly encountered by manual inspection, such as high-altitude falling, electric shock and other accidents, can be avoided.
In a word, the unmanned aerial vehicle is used for electric power inspection, so that inspection efficiency can be improved, cost can be reduced, safety and reliability can be improved, and the unmanned aerial vehicle is a novel electric power inspection mode with wide application prospect; in view of the above, we propose a vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle.
Disclosure of Invention
The utility model aims to provide a vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle, which aims to solve the problems in the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a fixed wing electric power inspection unmanned aerial vehicle that takes off and land perpendicularly, includes the organism, the bottom terminal surface fixedly connected with install bin of organism, fixedly connected with chucking subassembly in the install bin, chucking subassembly includes the pivot, the pivot has been cup jointed to the lateral wall of install bin, the one end fixedly connected with handle of pivot, the other end of pivot runs through the lateral wall of install bin, and cup joints with the bevel gear, bevel gear and threaded rod threaded connection, the lateral wall threaded connection of threaded rod has the thread bush, the lateral wall fixedly connected with slide bar of thread bush, the inner wall top fixedly connected with connecting rod two of install bin, the lateral wall and the one end fixedly connected with of telescopic link two, the other end fixedly connected with triangle piece of telescopic link, the bottom terminal surface fixedly connected with fixture block of triangle piece, the bayonet joint on fixture block and the connecting piece, the one end fixedly connected with visual light appearance of installing bin is kept away from to the connecting piece.
Optionally, the one end fixedly connected with infrared imaging appearance of installing box is kept away from to the connecting piece, and infrared imaging appearance can demonstrate power equipment's electric current, voltage heat phenomenon, discovers equipment trouble place, can fix a position power equipment's problem fast, and infrared imaging appearance can be at the night of totally no light simultaneously, or in the adverse circumstances that clouds such as rain, snow are densely covered, observe the target of control clearly.
Optionally, the lateral wall of telescopic link has cup jointed the spring, the lateral wall of connecting rod two is supported to the one end of spring, the lateral wall of triangular block is supported to the other end of spring.
Optionally, the front end of organism is provided with screw one, the both sides fixedly connected with fixed wing of organism, screw one and fixed wing can make unmanned aerial vehicle extension aerial work's time.
Optionally, the bottom fixedly connected with mount pad of fixed wing, the lateral wall of mount pad is provided with the extension rod, the tip fixedly connected with screw second of extension rod, screw second work can drive unmanned aerial vehicle and take off perpendicularly, can make unmanned aerial vehicle take off the operation under the circumstances that does not have supporting equipment such as runway.
Optionally, the one end of threaded rod cup joints with the interior top face of installing the case, the one end of the other end fixedly connected with connecting rod of threaded rod, the other end of connecting rod one rotates with the interior bottom face of installing the case to be connected, can improve the stability of chucking subassembly.
Compared with the prior art, the utility model provides a vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle, which has the following beneficial effects:
1. this fixed wing electric power inspection unmanned aerial vehicle that takes off and land perpendicularly, in order to be convenient for install, twist the handle, drive pivot, bevel gear threaded rod and rotate, further drive thread bush and slide bar up-and-down motion, when the slide bar upward movement, loosen the butt to the triangular block, under the effect of spring and telescopic link, triangular block and fixture block move to the one side of keeping away from the connecting piece, further the fixture block shifts out in the bayonet socket of connecting piece to can install and dismantle the connecting piece. After the connecting piece is installed, the handle is twisted reversely, so that the clamping block and the connecting piece can be clamped, the operation is convenient, and the visual light camera is easy to install for operators.
2. This fixed wing electric power of taking off and land perpendicularly patrols and examines unmanned aerial vehicle, in order to realize the emergence position of location electric power line trouble, when meetting electric power line trouble, twist the handle and can dismantle visual light appearance, then install infrared imaging appearance, after installing the connecting piece, reverse twist the handle to can block fixture block and connecting piece, realize the installation to infrared imaging appearance.
Drawings
FIG. 1 is a schematic view of a three-dimensional structure of the present utility model;
FIG. 2 is a schematic diagram of a structure of an embodiment of the present utility model;
FIG. 3 is a schematic diagram of a second embodiment of the present utility model;
fig. 4 is a schematic view of the structure of the area a of the present utility model.
In the figure: 1. a body; 2. a first propeller; 3. a fixed wing; 4. a second propeller; 5. a mounting box; 6. a connecting piece; 7. a visible light camera; 8. an infrared imager; 9. a rotating shaft; 10. a handle; 11. bevel gears; 12. a first connecting rod; 13. a threaded rod; 14. a thread sleeve; 15. a slide bar; 16. triangular blocks; 17. a clamping block; 18. a second connecting rod; 19. a spring; 20. a telescopic rod.
Detailed Description
Example 1
As shown in fig. 1-2 and 4, the utility model provides a technical scheme that: the utility model provides a fixed wing electric power inspection unmanned aerial vehicle that takes off and land perpendicularly, includes organism 1, and the front end of organism 1 is provided with screw one 2, and the both sides fixedly connected with fixed wing 3 of organism 1, screw one 2 and fixed wing 3 can make unmanned aerial vehicle extension aerial work's time. The bottom fixedly connected with mount pad of fixed wing 3, the lateral wall of mount pad is provided with the extension rod, and the tip fixedly connected with screw two 4 of extension rod, screw two 4 work can drive unmanned aerial vehicle and take off perpendicularly, can make unmanned aerial vehicle take off the operation under the circumstances that does not have corollary equipment such as runway. The bottom terminal surface fixedly connected with install bin 5 of organism 1, the chucking subassembly of fixedly connected with in the install bin 5, the chucking subassembly includes pivot 9, pivot 9 has been cup jointed to the lateral wall of install bin 5, the one end fixedly connected with handle 10 of pivot 9, the lateral wall of install bin 5 is run through to the other end of pivot 9, and cup joint with bevel gear 11, bevel gear 11 and threaded rod 13 threaded connection, the one end of threaded rod 13 cup joints with the interior top face of install bin 5, the one end of threaded rod 13's the other end fixedly connected with connecting rod one 12, the other end of connecting rod one 12 rotates with the interior bottom terminal surface of install bin 5 to be connected, can improve the stability of chucking subassembly. The lateral wall threaded connection of threaded rod 13 has thread bush 14, and the lateral wall fixedly connected with slide bar 15 of thread bush 14, the inner wall top fixedly connected with connecting rod two 18 of install bin 5, the lateral wall of connecting rod two 18 and the one end fixed connection of telescopic link 20, the other end fixedly connected with triangle 16 of telescopic link 20, the lateral wall of telescopic link 20 has cup jointed spring 19, the lateral wall of spring 19 one end butt connecting rod two 18, the lateral wall of spring 19 other end butt triangle 16. The bottom terminal surface fixedly connected with fixture block 17 of triangular block 16, the bayonet socket joint on fixture block 17 and the connecting piece 6, the one end fixedly connected with visible light camera 7 of the connecting piece 6 that keeps away from install bin 5.
When the visible light camera 7 is required to be installed, the handle 10 is twisted to drive the rotating shaft 9 and the threaded rod 13 of the bevel gear 11 to rotate, the threaded sleeve 14 and the slide rod 15 are further driven to move up and down, when the slide rod 15 moves upwards, the abutting joint of the triangular block 16 is loosened, the triangular block 16 and the clamping block 17 move to one side far away from the connecting piece 6 under the action of the spring 19 and the telescopic rod 20, and the clamping block 17 moves out of the bayonet of the connecting piece 6, so that the connecting piece 6 can be installed and detached. When the connector 6 is installed, the handle 10 is twisted in the opposite direction, so that the latch 17 can be latched with the connector 6. The operation is convenient, and the operator can easily install the visible light camera 7.
Example two
As shown in fig. 3, the present utility model is improved on the basis of the first embodiment to obtain a new technical solution: the one end fixedly connected with infrared imaging appearance 8 that the mounting case 5 was kept away from to connecting piece 6, and infrared imaging appearance 8 can demonstrate power equipment's electric current, voltage heat phenomenon, discovers equipment trouble place, can fix a position power equipment's problem fast, and infrared imaging appearance 8 can be at the night of totally no light simultaneously, or in the adverse circumstances that clouds such as rain, snow are densely covered, observe the target of control clearly.
In order to realize the position of the fault of the positioning power line, the handle 10 is twisted to drive the rotating shaft 9 and the threaded rod 13 of the bevel gear 11 to rotate, further drive the threaded sleeve 14 and the slide rod 15 to move up and down, when the slide rod 15 moves up, the abutting joint of the triangular block 16 is loosened, under the action of the spring 19 and the telescopic rod 20, the triangular block 16 and the clamping block 17 move to the side far away from the connecting piece 6, and further the clamping block 17 moves out of the bayonet of the connecting piece 6, so that the visible light camera 7 can be detached. Then the infrared imaging instrument 8 is installed, and after the connecting piece 6 is installed, the handle 10 is reversely twisted, so that the clamping block 17 and the connecting piece 6 can be clamped, and the infrared imaging instrument 8 is installed.
In the utility model, when in use, the handle 10 is twisted to drive the rotating shaft 9 and the threaded rod 13 of the bevel gear 11 to rotate, the threaded sleeve 14 and the slide rod 15 are further driven to move up and down, when the slide rod 15 moves up, the abutting of the triangular block 16 is loosened, the triangular block 16 and the clamping block 17 move to one side far away from the connecting piece 6 under the action of the spring 19 and the telescopic rod 20, and the clamping block 17 is further moved out of the bayonet of the connecting piece 6, so that the connecting piece 6 can be installed and detached. When the connector 6 is installed, the handle 10 is twisted in the opposite direction, so that the latch 17 can be latched with the connector 6. The operation is convenient, and the operator can easily install the visible light camera 7. The visible light camera 7 can patrol the power equipment and the surrounding environment, and can be used for daily patrol work. When encountering power line fault, twist handle 10 can dismantle visible light appearance 7, then install infrared imaging appearance 8, and after installing connecting piece 6, reverse twist handle 10 to can block fixture block 17 and connecting piece 6, realize the installation to infrared imaging appearance 8.
The foregoing utility model has been generally described in great detail, but it will be apparent to those skilled in the art that modifications and improvements can be made thereto. Accordingly, it is intended to cover modifications or improvements within the spirit of the inventive concepts.
Claims (6)
1. The utility model provides a fixed wing electric power inspection unmanned aerial vehicle that takes off and land perpendicularly, includes organism (1), the bottom terminal surface fixedly connected with install bin (5) of organism (1), its characterized in that: fixedly connected with chucking subassembly in install bin (5), chucking subassembly includes pivot (9), pivot (9) have been cup jointed to the lateral wall of install bin (5), the one end fixedly connected with handle (10) of pivot (9), the other end of pivot (9) runs through the lateral wall of install bin (5), and cup joints with bevel gear (11), bevel gear (11) and threaded rod (13) threaded connection, the lateral wall threaded connection of threaded rod (13) has threaded sleeve (14), the lateral wall fixedly connected with slide bar (15) of threaded sleeve (14), the one end fixedly connected with connecting rod two (18) of the inner wall top of install bin (5), the one end fixedly connected with of telescopic link (20) of connecting rod two (18), the other end fixedly connected with triangle piece (16) of telescopic link (20), the bottom terminal surface fixedly connected with fixture block (17) of triangle piece (16), bayonet socket joint on fixture block (17) and connecting piece (6), the one end (6) keep away from the visual fixedly connected with appearance (7) of making a video recording of install bin (5).
2. The vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle according to claim 1, wherein: one end of the connecting piece (6) far away from the mounting box (5) is fixedly connected with an infrared imager (8).
3. The vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle according to claim 1, wherein: the side wall of telescopic link (20) cup joints spring (19), the lateral wall of connecting rod two (18) is supported to the one end of spring (19), the lateral wall of triangular block (16) is supported to the other end of spring (19).
4. The vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle according to claim 1, wherein: the front end of the machine body (1) is provided with a first propeller (2), and two sides of the machine body (1) are fixedly connected with fixed wings (3).
5. The vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle according to claim 4, wherein: the bottom fixedly connected with mount pad of fixed wing (3), the lateral wall of mount pad is provided with the extension rod, the tip fixedly connected with screw two (4) of extension rod.
6. The vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle according to claim 1, wherein: one end of the threaded rod (13) is sleeved with the inner top end face of the installation box (5), one end of a first connecting rod (12) is fixedly connected to the other end of the threaded rod (13), and the other end of the first connecting rod (12) is rotatably connected with the inner bottom end face of the installation box (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321448298.3U CN220640247U (en) | 2023-06-08 | 2023-06-08 | Vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321448298.3U CN220640247U (en) | 2023-06-08 | 2023-06-08 | Vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220640247U true CN220640247U (en) | 2024-03-22 |
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ID=90288765
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321448298.3U Active CN220640247U (en) | 2023-06-08 | 2023-06-08 | Vertical take-off and landing fixed wing electric power inspection unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220640247U (en) |
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2023
- 2023-06-08 CN CN202321448298.3U patent/CN220640247U/en active Active
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