CN220315316U - Air-sea dual-purpose unmanned aerial vehicle with anchor chain structure - Google Patents
Air-sea dual-purpose unmanned aerial vehicle with anchor chain structure Download PDFInfo
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- CN220315316U CN220315316U CN202321778485.8U CN202321778485U CN220315316U CN 220315316 U CN220315316 U CN 220315316U CN 202321778485 U CN202321778485 U CN 202321778485U CN 220315316 U CN220315316 U CN 220315316U
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Abstract
The utility model discloses an empty sea dual-purpose unmanned aerial vehicle with an anchor chain structure, and relates to the technical field of unmanned aerial vehicles. According to the utility model, through the mutual matching of the slide bar, the buffer spring, the connecting block, the plate, the limit spring and the lug, when the empty and sea dual-purpose unmanned aerial vehicle with the anchor chain structure is required to be transported, the lug on two sides is pressed and the limit spring is extruded, at the moment, the limit spring is in a contracted state, the lug is contracted inside, and then the lug is pushed to enable the plate to move on the surface of the slide bar and be separated from the buffer spring, so that the tail is contracted inside the sleeve, the problem that the tail is easy to break in the transportation process is solved, and the effect that the tail has a certain protection effect on the phenomenon of contraction is achieved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an air-sea dual-purpose unmanned aerial vehicle with an anchor chain structure.
Background
The anchor chain is a special chain for connecting the anchor and the unmanned aerial vehicle and transmitting the holding power of the anchor, the anchor chain structure can enable the machine body to be stable in a fixed area and not float around along with sea waves, the manufacturing cost is greatly reduced along with the gradual maturation of the development technology of the unmanned aerial vehicle, the unmanned aerial vehicle is widely applied to various fields, and the unmanned aerial vehicle is also applied to agricultural plant protection, electric power inspection, police law enforcement, geological exploration, environmental monitoring, forest fire prevention, film and television aerial photography and the like besides military use. In addition, the unmanned aerial vehicle has huge application prospect in water, can be used for underwater detection and underwater rescue, and the travel route of the unmanned aerial vehicle in the air and the sea is changed into the air, so that the rapid and effective large-scale underwater detection can be realized, and the detection practicability can be effectively increased by converting the unmanned aerial vehicle in the air and the sea water. The following problems exist in the prior art:
the problem that the current anchor chain structure and the air-sea unmanned aerial vehicle are integrated and cannot be detached and replaced; meanwhile, as the tail fin in the air-sea dual-purpose unmanned aerial vehicle with the anchor chain structure is not provided with the telescopic structure, the problem that the tail fin is easy to break in the transportation process is caused.
Disclosure of Invention
The utility model provides an air-sea dual-purpose unmanned aerial vehicle with an anchor chain structure, which aims to solve the problems in the background technology.
In order to solve the technical problems, the utility model adopts the following technical scheme:
the utility model provides an empty sea dual-purpose unmanned aerial vehicle with anchor chain structure, includes the unmanned aerial vehicle body, the bottom fixedly connected with anchor chain device of unmanned aerial vehicle body, the one end fixedly connected with sleeve of unmanned aerial vehicle body, telescopic one end is provided with the fin.
The inside fixedly connected with fixed plate of anchor chain device, the draw-in groove has been seted up to the upper surface of fixed plate, the spout has been seted up to the inside of unmanned aerial vehicle body, the inside sliding connection of spout has the draw-in lever, the lower extreme and the temporal portion joint of draw-in groove of draw-in lever.
The technical scheme of the utility model is further improved as follows: one side fixedly connected with spring of clamping lever, the one end fixedly connected with spring board of spring, one side and the inside fixed connection of unmanned aerial vehicle body of spring board, the lower extreme of spring board extends to the inside of anchor chain device.
By adopting the technical scheme, the clamping grooves are conveniently clamped by the mutual matching of the springs, the clamping rods and the spring plates.
The technical scheme of the utility model is further improved as follows: the inside swing joint of spring board has the screw, the inside swing joint of surface and anchor chain device of screw, the inside sliding connection of spring board has the push rod, the one end of push rod extends to the outside of unmanned aerial vehicle body, the other end of push rod and one side fixed connection of clamping lever, the surface of push rod and the inside swing joint of unmanned aerial vehicle body, the upper surface of push rod is provided with the reinforcing seat, one side of reinforcing seat and one side fixed connection of unmanned aerial vehicle body.
By adopting the technical scheme, the anchor chain device is assembled and disassembled by the method through the mutual matching of the screw, the push rod and the reinforcing seat.
The technical scheme of the utility model is further improved as follows: the inside swing joint of strengthening the seat has the gag lever post, the upper end fixedly connected with stopper of gag lever post, the lower extreme of gag lever post alternates in the inside of push rod, the lower extreme of gag lever post extends to the outside of push rod, the surface of gag lever post is provided with the nut, the upper surface overlap joint of nut and the lower surface of push rod.
By adopting the technical scheme, the fixing effect on the push rod is enhanced by the mutual matching of the limiting rod, the limiting block and the screw cap in the scheme.
The technical scheme of the utility model is further improved as follows: the inside fixedly connected with slide bar of telescopic, the one end fixedly connected with buffer spring of slide bar, buffer spring's one end overlap joint has the connecting block, the one end fixedly connected with plate of connecting block, the one end of plate and the one end fixed connection of fin, the surface and the inside swing joint of telescopic of fin.
By adopting the technical scheme, the tail wing is contracted and stretched through the mutual matching of the sliding rod, the buffer spring, the connecting block and the plate.
The technical scheme of the utility model is further improved as follows: the surface fixedly connected with spacing spring of plate, the one end fixedly connected with lug of spacing spring, the one end of lug extends to telescopic outside, the surface and the telescopic inside swing joint of lug.
By adopting the technical scheme, the fixing device has the advantages that the fixing device is matched with the tail wing through the limiting spring and the protruding block, so that the tail wing can be conveniently fixed and clamped.
By adopting the technical scheme, compared with the prior art, the utility model has the following technical progress:
the utility model provides an air-sea dual-purpose unmanned aerial vehicle with an anchor chain structure, which adopts the mutual matching of a fixed plate, a clamping groove, a sliding groove, clamping rods, springs, a spring plate, a push rod, a reinforcing seat and screws, when the anchor chain device is required to be disassembled and replaced, the push rod is loosened by taking out a tool for the screws and then passing through the reinforcing seat, meanwhile, the push rods on two sides are pushed and the springs are extruded, so that the clamping rods slide in the sliding groove and are separated from the position of the clamping groove, and then the anchor chain device is moved downwards to be disassembled, thereby solving the problem that the anchor chain device and the air-sea dual-purpose unmanned aerial vehicle cannot be disassembled, and achieving the effects of being easy and convenient to disassemble and replace different types of anchor chain structures, thereby being suitable for the occurrence of ocean conditions.
The utility model provides an empty-sea dual-purpose unmanned aerial vehicle with an anchor chain structure, which adopts the mutual matching of a slide bar, a buffer spring, a connecting block, a plate, a limit spring and a lug, when the empty-sea dual-purpose unmanned aerial vehicle with the anchor chain structure is required to be transported, the lug on two sides is pressed and the limit spring is extruded, at the moment, the limit spring is in a contracted state, the lug is contracted inside, and then the lug is pushed to enable the plate to move on the surface of the slide bar and be separated from the buffer spring by pushing the tail wing, so that the tail wing is contracted inside a sleeve, the problem that the tail wing is easy to break in the transportation process is solved, and the effect that the tail wing has a certain protection effect due to the contraction phenomenon is achieved.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
fig. 2 is a schematic cross-sectional structure of the unmanned aerial vehicle body and the anchor chain device according to the present utility model;
FIG. 3 is a schematic cross-sectional view of a reinforcing seat and a pushrod according to the present utility model;
fig. 4 is a schematic cross-sectional view of a sleeve and tail of the present utility model.
In the figure: 1. an unmanned aerial vehicle body; 11. a chute; 12. a clamping rod; 13. a spring; 14. a spring plate; 15. a push rod; 16. a reinforcing seat; 161. a limit rod; 162. a limiting block; 163. a screw cap; 17. a screw; 2. a chain anchor device; 21. a fixing plate; 22. a clamping groove; 3. a sleeve; 31. a slide bar; 32. a buffer spring; 33. a connecting block; 34. a plate; 35. a limit spring; 36. a bump; 4. and a tail wing.
Description of the embodiments
The utility model is further illustrated by the following examples:
examples
As shown in fig. 1-4, the utility model provides an air-sea dual-purpose unmanned aerial vehicle with an anchor chain structure, which comprises an unmanned aerial vehicle body 1, wherein the bottom of the unmanned aerial vehicle body 1 is fixedly connected with an anchor chain device 2, one end of the unmanned aerial vehicle body 1 is fixedly connected with a sleeve 3, one end of the sleeve 3 is provided with a tail wing 4, the inside of the anchor chain device 2 is fixedly connected with a fixed plate 21, the upper surface of the fixed plate 21 is provided with a clamping groove 22, the inside of the unmanned aerial vehicle body 1 is provided with a sliding groove 11, the inside of the sliding groove 11 is slidingly connected with a clamping rod 12, the lower end of the clamping rod 12 is clamped with the temporal part of the clamping groove 22, one side of the clamping rod 12 is fixedly connected with a spring 13, one end of the spring 13 is fixedly connected with a spring plate 14, one side of the spring plate 14 is fixedly connected with the inside of the unmanned aerial vehicle body 1, the lower end of the spring plate 14 is extended into the inside of the anchor chain device 2, the inside of the spring plate 14 is movably connected with a screw 17, the surface of the screw 17 is movably connected with the inside of the anchor chain device 2, the inside of the spring plate 14 is slidingly connected with a push rod 15, one end of the push rod 15 is extended into the outside of the unmanned aerial vehicle body 1, one side of the clamping rod 15 is fixedly connected with the surface of the clamping rod 12, and one side of the push rod 16 is fixedly connected with the reinforcing seat 16 of the unmanned aerial vehicle body 1.
In this embodiment, when the remote controller is used, the air-sea dual-purpose unmanned aerial vehicle is controlled, flies to the ocean, and then opens the anchor chain device 2 through the setting of the remote controller, so that the internal anchor chain is put in the ocean, and the machine body is stabilized in a fixed area and does not float around along with sea waves, when the anchor chain device 2 is needed to be replaced according to the actual condition of the ocean, the screw 17 is taken out by a tool, the push rod 15 is loosened through the reinforcing seat 16, meanwhile, the push rods 15 on two sides are pushed and the springs 13 are extruded, the clamping rod 12 is closed towards the middle in the chute 11 and is separated from the clamping groove 22, and then the anchor chain device 2 is removed by being taken down, so that the anchor chain device 2 is convenient to replace.
Examples
As shown in fig. 1-4, on the basis of embodiment 1, the present utility model provides a technical solution: preferably, the inside swing joint of strengthening seat 16 has gag lever post 161, and the upper end fixedly connected with stopper 162 of gag lever post 161, and the lower extreme of gag lever post 161 alternates in the inside of push rod 15, and the lower extreme of gag lever post 161 extends to the outside of push rod 15, and the surface of gag lever post 161 is provided with nut 163, and the upper surface of nut 163 and the lower surface overlap joint of push rod 15.
In this embodiment, when the push rod 15 needs to be loosened before the disassembly, the lower end of the limit rod 161 is provided with threads which rotate the nut 163 in the opposite direction and remove the nut, and then the limit rod 161 is moved upward and pulled out by holding the limit block 162, so that the push rod 15 is loosened.
Examples
As shown in fig. 1-4, on the basis of embodiment 1, the present utility model provides a technical solution: preferably, the inside fixedly connected with slide bar 31 of sleeve 3, the one end fixedly connected with buffer spring 32 of slide bar 31, the one end overlap joint of buffer spring 32 has connecting block 33, the one end fixedly connected with plate 34 of connecting block 33, the one end of plate 34 and the one end fixedly connected with fin 4, the surface of fin 4 and the inside swing joint of sleeve 3, the fixed surface of plate 34 is connected with spacing spring 35, the one end fixedly connected with lug 36 of spacing spring 35, the one end of lug 36 extends to the outside of sleeve 3, the surface of lug 36 and the inside swing joint of sleeve 3.
In this embodiment, when transportation is needed, the bump 36 on two sides is pressed and the limit spring 35 is extruded, so that the limit spring 35 and the bump 36 are contracted inside, then the tail 4 is pushed to enable the connecting block 33 to move rightwards on the surface of the slide rod 31 and separate from the buffer spring 32, so that the tail 4 is contracted inside the sleeve 3, when usage is needed, the tail 4 is pulled forcefully to enable the connecting block 33 to move leftwards on the surface of the slide rod 31 and extrude the buffer spring 32, meanwhile, the bump 36 is pushed to move and extend out of the sleeve 3 due to the elastic action of the limit spring 35, and at the moment, the limit spring 35 is from a contracted state to an jacking state, so that the tail 4 is clamped and fixed.
The working principle of the air-sea dual-purpose unmanned aerial vehicle with the anchor chain structure is specifically described below.
As shown in fig. 1 to 4, when the unmanned aerial vehicle is required to be used, the unmanned aerial vehicle is controlled by a remote controller and flies to the sea, the anchor chain device 2 is opened by the arrangement of the remote controller, so that the anchor chain device 2 is put in the sea, the fuselage is stabilized in a fixed area and does not float around with sea waves, when the anchor chain device 2 is required to be replaced, the screw 17 is taken out, the push rod 15 is loosened by the reinforcing seat 16, the clamping rod 12 moves in the sliding groove 11 and is separated from the clamping groove 22 by the cooperation of the push rod 15 and the spring 13, so that the disassembly is performed, when the unmanned aerial vehicle is transported, the bump 36 on two sides is pressed and the limit spring 35 is extruded, the limit spring 35 and the bump 36 are contracted in the sea, and then the connecting block 33 is moved rightwards on the surface of the sliding rod 31 and separated from the buffer spring 32 by pushing the tail wing 4, so that the tail wing 4 is contracted in the sleeve 3.
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 an empty marine dual-purpose unmanned aerial vehicle with anchor chain structure, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein an anchor chain device (2) is fixedly connected to the bottom of the unmanned aerial vehicle body (1), a sleeve (3) is fixedly connected to one end of the unmanned aerial vehicle body (1), and a tail wing (4) is arranged at one end of the sleeve (3);
the inside fixedly connected with fixed plate (21) of anchor chain device (2), draw-in groove (22) have been seted up to the upper surface of fixed plate (21), spout (11) have been seted up to the inside of unmanned aerial vehicle body (1), the inside sliding connection of spout (11) has draw-in lever (12), the lower extreme and the temporal joint of draw-in groove (22) of draw-in lever (12).
2. The air-sea dual-purpose unmanned aerial vehicle with an anchor chain structure according to claim 1, wherein: one side fixedly connected with spring (13) of clamping rod (12), the one end fixedly connected with spring board (14) of spring (13), one side and the inside fixed connection of unmanned aerial vehicle body (1) of spring board (14), the lower extreme of spring board (14) extends to the inside of anchor chain device (2).
3. The air-sea dual-purpose unmanned aerial vehicle with an anchor chain structure according to claim 2, wherein: the inside swing joint of spring board (14) has screw (17), the inside swing joint of the surface of screw (17) and anchor chain device (2), the inside sliding connection of spring board (14) has push rod (15), the one end of push rod (15) extends to the outside of unmanned aerial vehicle body (1), the other end of push rod (15) and one side fixed connection of clamping rod (12), the surface of push rod (15) and the inside swing joint of unmanned aerial vehicle body (1), the upper surface of push rod (15) is provided with strengthens seat (16), one side of strengthening seat (16) and one side fixed connection of unmanned aerial vehicle body (1).
4. The air-sea dual-purpose unmanned aerial vehicle with an anchor chain structure according to claim 3, wherein: the inside swing joint of boss (16) has gag lever post (161), the upper end fixedly connected with stopper (162) of gag lever post (161), the lower extreme of gag lever post (161) alternates in the inside of push rod (15), the lower extreme of gag lever post (161) extends to the outside of push rod (15), the surface of gag lever post (161) is provided with nut (163), the upper surface of nut (163) and the lower surface overlap joint of push rod (15).
5. The air-sea dual-purpose unmanned aerial vehicle with an anchor chain structure according to claim 1, wherein: the inside fixedly connected with slide bar (31) of sleeve (3), the one end fixedly connected with buffer spring (32) of slide bar (31), the one end overlap joint of buffer spring (32) has connecting block (33), the one end fixedly connected with plate (34) of connecting block (33), the one end of plate (34) and the one end fixed connection of fin (4), the surface of fin (4) and the inside swing joint of sleeve (3).
6. The air-sea dual-purpose unmanned aerial vehicle with an anchor chain structure according to claim 5, wherein: the surface fixing of plate (34) is connected with spacing spring (35), the one end fixedly connected with lug (36) of spacing spring (35), the one end of lug (36) extends to the outside of sleeve (3), the surface of lug (36) and the inside swing joint of sleeve (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321778485.8U CN220315316U (en) | 2023-07-07 | 2023-07-07 | Air-sea dual-purpose unmanned aerial vehicle with anchor chain structure |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321778485.8U CN220315316U (en) | 2023-07-07 | 2023-07-07 | Air-sea dual-purpose unmanned aerial vehicle with anchor chain structure |
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| Publication Number | Publication Date |
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| CN220315316U true CN220315316U (en) | 2024-01-09 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321778485.8U Active CN220315316U (en) | 2023-07-07 | 2023-07-07 | Air-sea dual-purpose unmanned aerial vehicle with anchor chain structure |
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| Country | Link |
|---|---|
| CN (1) | CN220315316U (en) |
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2023
- 2023-07-07 CN CN202321778485.8U patent/CN220315316U/en active Active
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