CN220076699U - Unmanned aerial vehicle frame line structure for electric power iron tower - Google Patents
Unmanned aerial vehicle frame line structure for electric power iron tower Download PDFInfo
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- CN220076699U CN220076699U CN202321297267.2U CN202321297267U CN220076699U CN 220076699 U CN220076699 U CN 220076699U CN 202321297267 U CN202321297267 U CN 202321297267U CN 220076699 U CN220076699 U CN 220076699U
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- aerial vehicle
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- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 title claims abstract description 20
- 229910052742 iron Inorganic materials 0.000 title claims abstract description 10
- 238000003825 pressing Methods 0.000 claims description 21
- 238000000034 method Methods 0.000 abstract description 5
- 238000003860 storage Methods 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 210000003781 tooth socket Anatomy 0.000 description 1
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle frame structure for an electric power iron tower, which relates to the field of unmanned aerial vehicles and comprises a machine body, a machine frame and a bracket, wherein the machine frame is used for supporting an unmanned aerial vehicle propeller and is rotationally connected to the edge of the machine body, the bracket is fixedly connected to the upper surface of the machine body, a limiting mechanism is arranged on the upper surface of the machine body and is used for locking the unfolding state and the storage state of the machine frame, and the limiting mechanism comprises a locking plate, a sliding rod, a sliding rail and a connecting frame. According to the folding locking device, the locking assembly and the limiting mechanism are arranged, so that the unmanned aerial vehicle can be folded in the manual carrying process, the locking is convenient, the frame can be folded and locked only by rotating the rotating rod, and the operation is simple and convenient.
Description
Technical Field
The utility model relates to the field of unmanned aerial vehicles, in particular to an unmanned frame line structure for an electric power iron tower.
Background
Unmanned aircraft is abbreviated as "unmanned plane", english abbreviation is "UVA", is unmanned plane operated by radio remote control equipment and self-provided program control device, or is operated by the vehicle-mounted computer completely or intermittently autonomously, compared with unmanned plane, unmanned plane is more suitable for the task of being too "dull, dirty or dangerous", unmanned plane can be classified into military and civil according to application field, military aspect, unmanned plane is classified into reconnaissance plane and target plane, civil aspect, unmanned plane and industry application, is the real just need of unmanned plane; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.
When unmanned aerial vehicle carries out the during operation of overhead line to electric power iron tower, operational environment generally goes up, and the inside vehicle of mountain area can't get into, can only artifical walking get into, just needs the manual work to carry unmanned aerial vehicle into the mountain area inside at this moment, but unmanned aerial vehicle's frame is longer, and general unmanned aerial vehicle frame can't be folded and is inconvenient for carrying out manual handling operation, greatly reduced the transport unmanned aerial vehicle get into the work efficiency in mountain area.
Disclosure of Invention
The utility model aims at: in order to solve the problem that the unmanned aerial vehicle frame is long and inconvenient to carry, the unmanned aerial vehicle frame line structure for the electric power iron tower is provided.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the unmanned aerial vehicle frame line structure comprises a frame, a frame and a bracket, wherein the frame is used for supporting an unmanned aerial vehicle propeller and is rotationally connected to the edge of the frame, the bracket is fixedly connected to the upper surface of the frame, the upper surface of the frame is provided with a limiting mechanism, the limiting mechanism is used for locking the unfolding state and the storage state of the frame, and the limiting mechanism comprises a locking plate, a sliding rod, a sliding rail and a connecting frame;
the sliding rail is fixedly connected to the outer wall of the bracket in a surrounding manner, the sliding rod is connected to the inner wall of the sliding rail in a sliding manner, and the sliding rail is used for guiding and limiting the sliding of the sliding rod;
the locking plate is fixedly connected to the lower portion of one end of the sliding rod, the locking plate is used for locking the rotation of the frame, and the connecting frame is fixedly connected to the upper end of the sliding rail.
As still further aspects of the utility model: a locking component is arranged above the bracket and comprises tooth grooves, a rotating rod, a pressing plate, a gear and a spring;
the rotating rod is rotatably connected to the upper surface of the machine body and penetrates through the upper portion of the support, one end of the connecting frame is fixedly connected with the rotating rod, and the rotating rod drives the locking plate to rotate through the connecting frame so as to release the limit of the machine frame;
the tooth groove is formed in the upper surface of the top end of the support and is positioned on the outer side of the rotating rod, the pressing plate and the gear are connected to the outer wall of the rotating rod in a sliding mode, and the gear is meshed with the tooth groove and used for locking rotation of the rotating rod;
the spring is sleeved on the outer wall of the rotating rod, the spring is positioned between the gear and the machine body, and the spring is used for providing upward moving force for the gear after downward moving.
As still further aspects of the utility model: the locking groove has been seted up to one side of frame, the thickness of locking groove with the thickness phase-match of locking board, just when the frame rotated to vertical state, the horizontal height of locking groove and the horizontal height phase-match of locking board.
As still further aspects of the utility model: the pressing plate is of a circular ring structure, the pressing plate is connected with the gear through the connecting block, and the gear can be pushed downwards through pressing the pressing plate.
As still further aspects of the utility model: the frame, the locking plate, the sliding rod and the connecting frame are provided with a plurality of sliding rods and are distributed at equal intervals in circumference, and the number of the sliding rods and the connecting frames are matched.
As still further aspects of the utility model: the bottom of fuselage is located the downside fixedly connected with limiting plate of frame for it is spacing to rotate downwards of frame.
As still further aspects of the utility model: the locking plate is arranged in an arc shape, and in an initial state, the locking plate is attached to the frame.
Compared with the prior art, the utility model has the beneficial effects that:
through setting up locking subassembly and stop gear, make unmanned aerial vehicle can fold at the in-process of manual handling, and the locking is convenient, only need rotate the dwang alright folding locking to the frame, easy operation is convenient.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic diagram of a limiting mechanism according to the present utility model;
FIG. 3 is a schematic view of the bottom structure of the present utility model;
FIG. 4 is a schematic view of a locking assembly according to the present utility model;
fig. 5 is an exploded view of the locking assembly of the present utility model.
In the figure: 1. a body; 2. a frame; 3. a limiting mechanism; 301. a locking plate; 302. a slide bar; 303. a slide rail; 304. a connecting frame; 4. a locking assembly; 401. tooth slots; 402. a rotating lever; 403. pressing the plate; 404. a gear; 405. a spring; 5. a bracket; 6. a locking groove.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1 to 5, in an embodiment of the present utility model, an unmanned frame wire structure for an electric iron tower includes a frame 1, a frame 2, and a bracket 5, wherein the frame 2 is used for supporting an unmanned aerial vehicle propeller and is rotatably connected to an edge of the frame 1, the bracket 5 is fixedly connected to an upper surface of the frame 1, a limit mechanism 3 is provided on the upper surface of the frame 1, the limit mechanism 3 is used for locking an unfolding state and a storage state of the frame 2, and the limit mechanism 3 includes a locking plate 301, a sliding rod 302, a sliding rail 303, and a connecting frame 304;
the sliding rail 303 is fixedly connected to the outer wall of the bracket 5 in a surrounding manner, the sliding rod 302 is slidably connected to the inner wall of the sliding rail 303, and the sliding rail 303 is used for guiding and limiting the sliding of the sliding rod 302;
the locking plate 301 is fixedly connected below one end of the sliding rod 302, the locking plate 301 is used for locking the rotation of the frame 2, and the connecting frame 304 is fixedly connected to the upper end of the sliding rail 303;
a locking component 4 is arranged above the bracket 5, and the locking component 4 comprises tooth sockets 401, a rotating rod 402, a pressing plate 403, a gear 404 and a spring 405;
the rotating rod 402 is rotatably connected to the upper surface of the machine body 1 and penetrates through the upper side of the bracket 5, one end of the connecting frame 304 is fixedly connected with the rotating rod 402, and the rotating rod 402 drives the locking plate 301 to rotate through the connecting frame 304 so as to release the limit of the machine frame 2;
the tooth slot 401 is arranged on the upper surface of the top end of the bracket 5 and is positioned at the outer side of the rotating rod 402, the pressing plate 403 and the gear 404 are connected to the outer wall of the rotating rod 402 in a sliding way, and the gear 404 is meshed with the tooth slot 401 and is used for locking the rotation of the rotating rod 402;
the spring 405 is sleeved on the outer wall of the rotating rod 402, the spring 405 is located between the gear 404 and the machine body 1, and the spring 405 is used for providing upward moving force for the gear 404 after downward moving;
a locking groove 6 is formed in one side of the frame 2, the thickness of the locking groove 6 is matched with that of the locking plate 301, and when the frame 2 rotates to a vertical state, the horizontal height of the locking groove 6 is matched with that of the locking plate 301;
the pressing plate 403 is provided in a circular ring structure, and the pressing plate 403 is connected with the gear 404 through a connecting block, and the gear 404 can be pushed down by pressing the pressing plate 403.
In this embodiment: when unmanned aerial vehicle needs to be folded and transported, press the clamp plate 403 with the hand, press the in-process that the clamp plate 403 was pressing down through connecting block drive gear 404 and move in step, at this moment, gear 404 and tooth's socket 401 separation, rotate dwang 402, dwang 402 drives link 304 and slide bar 302 and moves under the orbit of slide rail 303, lock plate 301 is also driven and moves this moment, it is that lock plate 301 is laminated with frame 2 under the initial condition to need to say, lock plate 301 carries out spacingly to the upward rotation of frame 2, lock plate 301 displacement to one side with frame 2, upset frame 2 makes frame 2 fold, again with lock plate 301 to the direction of being close to frame 2 after the upset remove, make lock plate 301 insert the inside of lock groove 6, will press the hand of pressing down at clamp plate 403 again, utilize the restoring force of spring 405, make gear 404 upwards shift, make gear 404 and tooth's socket 401 mesh, make dwang 402 obtain fixedly, thereby make lock plate 301 obtain locking folding under the state, make frame 2 obtain locking folding through setting up more convenient.
Referring to fig. 1 to 4, a plurality of frames 2, locking plates 301, sliding rods 302, and connecting frames 304 are provided, and are distributed at equal intervals along the circumference, and the numbers of the frames are matched.
In this embodiment: by the above arrangement, the plurality of locking plates 301 can lock the plurality of racks 2, and the problem that the plurality of racks 2 cannot be locked due to the number of the locking plates 301 does not occur.
Referring to fig. 3, a bottom end of the machine body 1 is located at a lower side of the frame 2 and is fixedly connected with a limiting plate for limiting downward rotation of the frame 2.
In this embodiment: through the arrangement, the downward overturning direction of the stand 2 is limited, and the stand 2 cannot be overturned downwards in the using process.
Referring to fig. 2, the locking plate 301 is configured in an arc shape, and in an initial state, the locking plate 301 is attached to the frame 2.
In this embodiment: through the above setting, make locking plate 301 laminate mutually with frame 2, make unmanned aerial vehicle lock frame 2 at the in-process of flight, the condition of frame 2 upset can not appear.
The foregoing description is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical solution of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.
Claims (7)
1. The utility model provides an unmanned aerial vehicle frame line structure for electric power iron tower, includes fuselage (1), frame (2), support (5), its characterized in that, frame (2) are used for supporting unmanned aerial vehicle screw, and rotate connect in the edge of fuselage (1), support (5) fixed connection in the upper surface of fuselage (1), the upper surface of fuselage (1) is provided with stop gear (3), stop gear (3) are used for carrying out the locking operation to the expansion state and the state of accomodating of frame (2), stop gear (3) include locking plate (301), slide bar (302), slide rail (303), link (304);
the sliding rail (303) is fixedly connected to the outer wall of the bracket (5) in a surrounding mode, the sliding rod (302) is connected to the inner wall of the sliding rail (303) in a sliding mode, and the sliding rail (303) is used for guiding and limiting the sliding of the sliding rod (302);
the locking plate (301) is fixedly connected to the lower portion of one end of the sliding rod (302), the locking plate (301) is used for locking rotation of the frame (2), and the connecting frame (304) is fixedly connected to the upper end of the sliding rail (303).
2. The unmanned aerial vehicle frame line structure for the electric power iron tower according to claim 1, wherein a locking component (4) is arranged above the bracket (5), and the locking component (4) comprises a tooth slot (401), a rotating rod (402), a pressing plate (403), a gear (404) and a spring (405);
the rotating rod (402) is rotatably connected to the upper surface of the machine body (1) and penetrates through the upper portion of the bracket (5), one end of the connecting frame (304) is fixedly connected with the rotating rod (402), and the rotating rod (402) drives the locking plate (301) to rotate through the connecting frame (304) so as to release the limit of the machine frame (2);
the tooth groove (401) is formed in the upper surface of the top end of the support (5) and is positioned on the outer side of the rotating rod (402), the pressing plate (403) and the gear (404) are connected to the outer wall of the rotating rod (402) in a sliding mode, and the gear (404) is meshed with the tooth groove (401) and used for locking the rotation of the rotating rod (402);
the spring (405) is sleeved on the outer wall of the rotating rod (402), the spring (405) is located between the gear (404) and the machine body (1), and the spring (405) is used for providing upward moving force for the gear (404) after downward moving.
3. An unmanned aerial vehicle frame line structure for a power pylon according to claim 1, wherein a locking groove (6) is provided on one side of the frame (2), the thickness of the locking groove (6) matches the thickness of the locking plate (301), and when the frame (2) is rotated to a vertical state, the horizontal height of the locking groove (6) matches the horizontal height of the locking plate (301).
4. An unmanned aerial vehicle frame line structure for a power pylon according to claim 2, wherein the pressing plate (403) is provided in a circular ring structure, and the pressing plate (403) is connected with the gear (404) through a connecting block, and the gear (404) can be pushed down by pressing the pressing plate (403).
5. An unmanned frame line structure for electric power towers according to claim 1, characterized in that the frame (2), locking plate (301), sliding rod (302), connecting frame (304) are provided in plurality and equally distributed circumferentially and in number.
6. An unmanned frame line structure for an electric iron tower according to claim 1, wherein the bottom end of the frame (1) is located at the lower side of the frame (2) and is fixedly connected with a limiting plate for limiting the downward rotation of the frame (2).
7. An unmanned aerial vehicle frame line structure for a power pylon according to claim 1, wherein the locking plate (301) is arranged in the shape of an arc, and in the initial state the locking plate (301) is in abutment with the frame (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321297267.2U CN220076699U (en) | 2023-05-26 | 2023-05-26 | Unmanned aerial vehicle frame line structure for electric power iron tower |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321297267.2U CN220076699U (en) | 2023-05-26 | 2023-05-26 | Unmanned aerial vehicle frame line structure for electric power iron tower |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220076699U true CN220076699U (en) | 2023-11-24 |
Family
ID=88832803
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321297267.2U Active CN220076699U (en) | 2023-05-26 | 2023-05-26 | Unmanned aerial vehicle frame line structure for electric power iron tower |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220076699U (en) |
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2023
- 2023-05-26 CN CN202321297267.2U patent/CN220076699U/en active Active
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