CN220884825U - Multi-mode large-load modularized multipurpose unmanned aerial vehicle - Google Patents
Multi-mode large-load modularized multipurpose unmanned aerial vehicle Download PDFInfo
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- CN220884825U CN220884825U CN202322353490.0U CN202322353490U CN220884825U CN 220884825 U CN220884825 U CN 220884825U CN 202322353490 U CN202322353490 U CN 202322353490U CN 220884825 U CN220884825 U CN 220884825U
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a multi-mode large-load modularized multipurpose unmanned aerial vehicle which comprises an unmanned aerial vehicle and supporting legs, wherein the left side and the right side of the bottom of the unmanned aerial vehicle are respectively fixedly connected with the tops of the supporting legs, the bottom of the unmanned aerial vehicle is connected with a control structure, the bottom of the control structure is connected with a bottom plate, the front side and the rear side of the top of the bottom plate are respectively connected with a limiting structure, the top of the bottom plate is fixedly connected with a protection pad, a handle is matched in the control structure to drive a screw to rotate outwards, the inner side of the outer wall of the screw is separated from a corresponding round opening, then a vertical cylinder moves downwards on the outer wall of a vertical rod, the bottom plate is driven to move downwards, the distance between the bottom plate and the bottom of the unmanned aerial vehicle is adjusted, then the handle is matched to drive the screw to rotate inwards, the inner side of the outer wall of the screw is spliced with the inner wall of the corresponding round opening, the load of the unmanned aerial vehicle is increased, and the working efficiency of the unmanned aerial vehicle is improved.
Description
Technical Field
The utility model relates to the technical field of multi-purpose unmanned aerial vehicles, in particular to a multi-mode large-load modularized multi-purpose unmanned aerial vehicle.
Background
The drone is an unmanned aircraft that is maneuvered using a radio remote control device and a self-contained programming device, or is operated autonomously, either entirely or intermittently, by an on-board computer.
For example, the utility model discloses a multipurpose unmanned aerial vehicle of "CN207157512U" is authorized, can carry out long-range detection through the camera, be applicable to various dangerous occasions, realize the jetting of cargo in end storehouse through the cooperation of two stripper and electric telescopic handle, and control is simple, and is fast, can be used to rescue the aerial throwing of goods and materials, also can place the medicine spraying ware in the end storehouse, the external branch pipe of cooperation and shower nozzle can carry out the spraying of liquid, can be used to the agricultural medicine operation of spouting and water spray, a tractor serves several purposes, the cost of design research and development has been reduced, satisfy multiple demand simultaneously, but in the unmanned aerial vehicle use, goods and materials and camera equipment are placed to unmanned aerial vehicle's below, can increase unmanned aerial vehicle's whole weight like this, unmanned aerial vehicle goods and materials places the space is limited, lead to unmanned aerial vehicle can't reach user's demand, many times carry goods and materials, lead to unmanned aerial vehicle's load volume is less, unmanned aerial vehicle's work efficiency has been reduced.
Disclosure of utility model
The utility model aims to solve the problems that the load capacity of an unmanned aerial vehicle is small and the working efficiency of the unmanned aerial vehicle is reduced, and provides a multi-mode large-load modularized multipurpose unmanned aerial vehicle.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
The utility model provides a multi-mode big load modularization multipurpose unmanned aerial vehicle, includes unmanned aerial vehicle and landing leg, unmanned aerial vehicle's bottom left and right sides is the top looks rigid coupling with the landing leg respectively, unmanned aerial vehicle's bottom is connected with control structure, control structure's bottom is connected with the bottom plate, both sides are connected with limit structure respectively around the top of bottom plate, the top rigid coupling of bottom plate has the protection pad.
Preferably, the control structure comprises a vertical rod and round openings, the top of the vertical rod is fixedly connected with the bottom of the unmanned aerial vehicle, a plurality of round openings are formed in the outer side of the vertical rod, a vertical barrel is slidably clamped on the outer wall of the vertical rod, a screw is connected above the outer wall of the vertical barrel in a threaded manner, and a grip is fixedly connected on the outer side of the screw.
Preferably, the inner side of the outer wall of the screw is spliced with the inner wall of the round opening.
Preferably, the bottom of the screw rod is fixedly connected with the top of the bottom plate.
Preferably, the limiting structure comprises a vertical plate and a square plate, the bottom of the outer wall of the vertical plate is spliced with the notch at the top of the bottom plate, the lower part of the outer side of the vertical plate is fixedly connected with the inner side of the square plate, and the inner wall of the square plate is connected with a bolt in a threaded manner.
Preferably, the bottom of the outer wall of the bolt is in threaded connection with the top of the bottom plate.
The multi-mode large-load modularized multipurpose unmanned aerial vehicle provided by the utility model has the beneficial effects that: the screw is driven to rotate outwards through the cooperation handle in the control structure, so that the inner side of the outer wall of the screw is separated from a corresponding round opening, then the vertical cylinder moves downwards on the outer wall of the vertical rod, and then the bottom plate is driven to move downwards, so that the distance between the bottom plate and the bottom of the unmanned aerial vehicle is adjusted, and then the cooperation handle drives the screw to rotate inwards, so that the inner side of the outer wall of the screw is spliced with the inner wall of the corresponding round opening, the load of the unmanned aerial vehicle is increased, and the working efficiency of the unmanned aerial vehicle is improved.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic diagram of the structure of FIG. 1A;
FIG. 3 is a schematic diagram of the structure of FIG. 1B;
Fig. 4 is a schematic structural diagram of the connection relationship among the straight rod, the transverse plate and the disc in fig. 1.
In the figure: 1. unmanned aerial vehicle, 2, control structure, 201, montant, 202, circle mouth, 203, vertical tube, 204, screw rod, 205, handle, 3, limit structure, 301, riser, 302, square board, 303, bolt, 4, bottom plate, 5, protection pad, 6, landing leg, 7, straight-bar, 8, diaphragm, 9, disc.
Detailed Description
The utility model is further described below with reference to the accompanying drawings:
Example 1:
Please refer to fig. 1-4: in this embodiment, a multimode big load modularization multipurpose unmanned aerial vehicle, including unmanned aerial vehicle 1 and landing leg 6, the bottom left and right sides of unmanned aerial vehicle 1 respectively with the top looks rigid coupling of landing leg 6, how unmanned aerial vehicle 1 operates the use has been prior art, do not set forth the model too much and select according to the user demand, the bottom of unmanned aerial vehicle 1 is connected with control structure 2, control structure 2's bottom is connected with bottom plate 4, both sides are connected with limit structure 3 respectively around the top of bottom plate 4, the top rigid coupling of bottom plate 4 has protection pad 5, protection pad 5 material is rubber.
The control structure 2 comprises a vertical rod 201 and round openings 202, wherein the top of the vertical rod 201 is fixedly connected with the bottom of the unmanned aerial vehicle 1, a plurality of round openings 202 are formed in the outer side of the vertical rod 201, a vertical cylinder 203 is slidably clamped on the outer wall of the vertical rod 201, the vertical cylinder 203 is stressed to slide up and down through the outer wall of the vertical rod 201, a screw 204 is connected above the outer wall of the vertical cylinder 203 in a threaded manner, a handle 205 is fixedly connected on the outer side of the screw 204, the handle 205 is convenient for driving the screw 204 to rotate, the inner side of the outer wall of the screw 204 is spliced with the inner wall of the round opening 202, and the bottom of the screw 204 is fixedly connected with the top of the bottom plate 4;
The screw 204 is driven to rotate outwards through the cooperation of the grip 205 in the control structure 2, so that the inner side of the outer wall of the screw 204 is separated from the corresponding round opening 202, then the vertical barrel 202 moves downwards on the outer wall of the vertical rod 201, further the bottom plate 4 is driven to move downwards, the distance between the bottom plate 4 and the bottom of the unmanned aerial vehicle 1 is adjusted, then the screw 204 is driven to rotate inwards through the cooperation of the grip 205, the inner side of the outer wall of the screw 204 is spliced with the inner wall of the corresponding round opening 202, the load of the unmanned aerial vehicle is increased, and the working efficiency of the unmanned aerial vehicle is improved.
The restriction structure 3 includes riser 301 and square board 302, and the outer wall bottom of riser 301 is pegged graft mutually with the top notch of bottom plate 4, and riser 301 atress upwards pulls the notch that can break away from bottom plate 4 top, and riser 301's length can be adjusted according to the interval between bottom plate 4 and unmanned aerial vehicle 1, and the outside below of riser 301 and the inboard looks rigid coupling of square board 302, and square board 302's inner wall threaded connection has bolt 303, and bolt 303 plays the fixed action to square board 302 and riser 301, and the outer wall bottom of bolt 303 and the top threaded connection of bottom plate 4.
Working principle:
When the unmanned aerial vehicle 1 is used, the handle 205 is matched to drive the screw 204 to rotate outwards, the inner side of the outer wall of the screw 204 is separated from the corresponding round opening 202, then the vertical barrel 202 moves downwards on the outer wall of the vertical rod 201, the bottom plate 4 is driven to move downwards, the distance between the bottom plate 4 and the bottom of the unmanned aerial vehicle 1 is adjusted, then the handle 205 is matched to drive the screw 204 to rotate inwards, the inner side of the outer wall of the screw 204 is spliced with the inner wall of the corresponding round opening 202, load is increased, objects are placed at the top of the bottom plate 4, then the vertical plate 301 is inserted at the front side and the rear side of the top of the bottom plate 4, then the bolt 303 rotates downwards through the square plate 302, the bottom of the outer wall of the bolt 303 is in threaded connection with the top of the bottom plate 4, the vertical plate 301 is used for shielding the objects, the terrain can be monitored when the unmanned aerial vehicle 1 is transported, the unmanned aerial vehicle 1 is in a modularized distribution, and the various structures of the unmanned aerial vehicle 1 are convenient to operate.
Example 2:
Please refer to fig. 1-4: in this embodiment, a multi-mode heavy-load modularization multipurpose unmanned aerial vehicle still includes straight-bar 7, diaphragm 8 and disc 9, and the outer wall inboard of straight-bar 7 is pegged graft mutually with unmanned aerial vehicle 1's outer wall circle mouth, and the outer wall inboard of straight-bar 7 is fixedly connected mutually with the outside of diaphragm 8, and the outer wall of straight-bar 7 is fixedly connected mutually with the inner wall of disc 9.
Working principle:
When unmanned aerial vehicle 1 load increases, can make straight-bar 7 peg graft with unmanned aerial vehicle 1, make the inboard of disc 9 laminate with unmanned aerial vehicle 1's outer wall mutually, the bolt passes disc 9 and unmanned aerial vehicle 1's outer wall threaded connection afterwards, accomplishes the fixed of straight-bar 7 and diaphragm 8, and diaphragm 8 can increase the area of contact with the air current, improves unmanned aerial vehicle 1 in the sky stability.
While the utility model has been shown and described with reference to a preferred embodiment, it will be understood by those of ordinary skill in the art that various changes in form and details may be made therein without departing from the scope of the utility model.
Claims (6)
1. The utility model provides a multi-mode big load modularization multipurpose unmanned aerial vehicle, includes unmanned aerial vehicle (1) and landing leg (6), its characterized in that: the bottom left and right sides of unmanned aerial vehicle (1) are respectively with the top looks rigid coupling of landing leg (6), the bottom of unmanned aerial vehicle (1) is connected with control structure (2), the bottom of control structure (2) is connected with bottom plate (4), both sides are connected with limit structure (3) respectively around the top of bottom plate (4), the top rigid coupling of bottom plate (4) has protection pad (5).
2. A multi-mode, high-load modular multi-purpose unmanned aerial vehicle as claimed in claim 1, wherein: the control structure (2) comprises a vertical rod (201) and a round opening (202), the top of the vertical rod (201) is fixedly connected with the bottom of the unmanned aerial vehicle (1), a plurality of round openings (202) are formed in the outer side of the vertical rod (201), a vertical barrel (203) is slidably clamped on the outer wall of the vertical rod (201), a screw (204) is connected with the upper side of the outer wall of the vertical barrel (203) in a threaded mode, and a grip (205) is fixedly connected with the outer side of the screw (204).
3. A multi-mode high load modular multi-purpose unmanned aerial vehicle as claimed in claim 2, wherein: the inner side of the outer wall of the screw rod (204) is spliced with the inner wall of the round opening (202).
4. A multi-mode high load modular multi-purpose unmanned aerial vehicle as claimed in claim 2, wherein: the bottom of the screw rod (204) is fixedly connected with the top of the bottom plate (4).
5. A multi-mode, high-load modular multi-purpose unmanned aerial vehicle as claimed in claim 1, wherein: the limiting structure (3) comprises a vertical plate (301) and a square plate (302), wherein the bottom of the outer wall of the vertical plate (301) is inserted into a notch at the top of the bottom plate (4), the lower part of the outer side of the vertical plate (301) is fixedly connected with the inner side of the square plate (302), and the inner wall of the square plate (302) is in threaded connection with a bolt (303).
6. The multi-mode, high-load modular multi-purpose unmanned aerial vehicle of claim 5, wherein: the bottom of the outer wall of the bolt (303) is in threaded connection with the top of the bottom plate (4).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202322353490.0U CN220884825U (en) | 2023-08-30 | 2023-08-30 | Multi-mode large-load modularized multipurpose unmanned aerial vehicle |
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CN202322353490.0U CN220884825U (en) | 2023-08-30 | 2023-08-30 | Multi-mode large-load modularized multipurpose unmanned aerial vehicle |
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CN220884825U true CN220884825U (en) | 2024-05-03 |
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CN202322353490.0U Active CN220884825U (en) | 2023-08-30 | 2023-08-30 | Multi-mode large-load modularized multipurpose unmanned aerial vehicle |
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2023
- 2023-08-30 CN CN202322353490.0U patent/CN220884825U/en active Active
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