CN220430532U - Multi-station unmanned aerial vehicle - Google Patents
Multi-station unmanned aerial vehicle Download PDFInfo
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- CN220430532U CN220430532U CN202321800623.8U CN202321800623U CN220430532U CN 220430532 U CN220430532 U CN 220430532U CN 202321800623 U CN202321800623 U CN 202321800623U CN 220430532 U CN220430532 U CN 220430532U
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- aerial vehicle
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- 230000007246 mechanism Effects 0.000 claims abstract description 4
- 230000003014 reinforcing effect Effects 0.000 claims description 8
- 230000001681 protective effect Effects 0.000 claims description 3
- 230000003139 buffering effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
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Abstract
The utility model discloses a multi-position unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body, wherein a plurality of first cameras are fixedly arranged on the outer surface of the top end of the unmanned aerial vehicle main body, a clamping piece is fixedly arranged on the outer surface of the bottom end of the unmanned aerial vehicle main body, a third camera is fixedly arranged on the outer surface of the bottom end of a connecting plate, two groups of buffer mechanisms are fixedly arranged at the bottom end of the unmanned aerial vehicle main body, a plurality of first cameras and a plurality of second cameras and a plurality of third cameras are fixedly arranged on the outer surface of the bottom end of the unmanned aerial vehicle main body, and the first cameras, the second cameras and the third cameras are arranged on the upper and lower sides of the unmanned aerial vehicle main body relatively, so that overlooking and looking-up view angles can be shot, scenes and targets can be more comprehensively captured, more accurate height sensing capability can be provided, and more accurate height control and position positioning can be realized.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a multi-station unmanned aerial vehicle.
Background
The unmanned plane is called as unmanned plane for short, and is a unmanned plane operated by radio remote control equipment and a self-contained program control device.
However, in the prior art, an unmanned aerial vehicle is usually only provided with a camera to shoot, so that the unmanned aerial vehicle has the problems of single visual angle, omission of targets and the like when shooting, and meanwhile, the unmanned aerial vehicle can be influenced by surrounding wind power in the falling process, so that shaking or unstable conditions occur, and when the battery power of the unmanned aerial vehicle is insufficient, the output power of a motor can be unstable, the unmanned aerial vehicle falls down to shake, so that the parts of the unmanned aerial vehicle are easily impacted, and the parts are damaged.
Disclosure of Invention
Object of the utility model
In view of the above, the present utility model is directed to a multi-station unmanned aerial vehicle, which solves the above-mentioned problems.
(II) technical scheme
The utility model provides a multi-station unmanned aerial vehicle, includes the unmanned aerial vehicle main part, unmanned aerial vehicle main part top surface fixed mounting has a plurality of first cameras, and the bottom surface fixed mounting of unmanned aerial vehicle main part has the fastener, the surface of fastener has circular draw-in groove, and fixed mounting has the motor in the circular draw-in groove, the one end of motor is connected with the connecting plate, the surface fixed mounting of connecting plate has four sets of solid fixed ring, and gu fixed ring's inner wall sets up the screw thread, install the pole in gu fixed ring's the inner wall, and the one end of pole is connected with the second camera, the bottom surface fixed mounting of connecting plate has the third camera, the bottom fixed mounting of unmanned aerial vehicle main part has two sets of buffer gear.
Preferably, the two groups of buffer mechanisms comprise connecting rods, the two connecting rods are divided into two groups, the two connecting rods are far away from each other, one ends of the two connecting rods are connected with fixed cross rods, and two fixed loop bars are fixedly arranged on the outer surfaces of the fixed cross rods.
Preferably, the outer surfaces of the two fixed loop bars are fixedly provided with reinforcing bars, and one end of each reinforcing bar is connected with a fixed cross bar.
Preferably, the inner walls of the two fixed loop bars are provided with cavities, springs are arranged in the cavities, and one ends of the springs are connected with telescopic rods.
Preferably, the outer surface of the telescopic rod is fixedly provided with a circular bottom plate.
Preferably, rubber is adhered to the bottom end of the circular bottom plate.
Preferably, the bottom fixed mounting of unmanned aerial vehicle main part has the protective housing.
From the above technical scheme, the application has the following beneficial effects:
1. according to the utility model, the first cameras and the second cameras and the third cameras are fixedly arranged on the outer surface of the top end of the unmanned aerial vehicle body and the outer surface of the bottom end connecting plate of the unmanned aerial vehicle body, and the first cameras, the second cameras and the third cameras are arranged up and down relatively through the unmanned aerial vehicle body, so that the viewing angles of overlooking and looking up can be shot, the scenes and the targets can be more comprehensively captured, more accurate height sensing capability can be provided, more accurate height control and position positioning can be realized, the coverage range can be enlarged, more comprehensive data support can be provided, and the connecting plate can rotate through the driving motor, so that the second cameras can shoot in three hundred sixty degrees.
2. According to the utility model, the springs and the telescopic rods in the two groups of buffer mechanisms fixedly arranged at the bottom end of the unmanned aerial vehicle main body are used, so that the buffer force of the unmanned aerial vehicle main body can be reduced in the landing process, and the landing of the unmanned aerial vehicle main body is more stable.
Drawings
FIG. 1 is a schematic view of a first perspective structure of the present utility model;
FIG. 2 is a schematic view of a second perspective structure of the present utility model;
FIG. 3 is a schematic side view of the present utility model;
FIG. 4 is an enlarged schematic view of the utility model at A in FIG. 2;
fig. 5 is an enlarged schematic view of fig. 2B in accordance with the present utility model.
In the figure: 1. an unmanned aerial vehicle main body; 2. a first camera; 3. a connecting rod; 4. fixing the cross bar; 5. fixing the loop bar; 6. a reinforcing rod; 7. a telescopic rod; 8. a circular bottom plate; 9. a second camera; 911. a round bar; 912. a fixing ring; 913. a third camera; 914. a connecting plate; 915. a protective shell; 916. a clamping piece; 917. a motor.
Detailed Description
The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses. It should be understood that throughout the drawings, the same or similar reference numerals indicate the same or similar parts and features. The drawings merely schematically illustrate the concepts and principles of embodiments of the disclosure and do not necessarily illustrate the specific dimensions and proportions of the various embodiments of the disclosure. Specific details or structures may be shown in exaggerated form in particular figures to illustrate related details or structures of embodiments of the present disclosure.
Referring to fig. 1-5, an embodiment of the present utility model is provided:
the utility model provides a multi-station unmanned aerial vehicle, including unmanned aerial vehicle main part 1, unmanned aerial vehicle main part 1 top surface fixed mounting has a plurality of first cameras 2, and the bottom surface fixed mounting of unmanned aerial vehicle main part 1 has the fastener 916, the surface of fastener 916 has circular draw-in groove, and fixed mounting has motor 917 in the circular draw-in groove, the one end of motor 917 is connected with connecting plate 914, the surface fixed mounting of connecting plate 914 has four fixed rings 912 of group, and the inner wall of fixed ring 912 is seted up the screw thread, install round bar 911 in the inner wall of fixed ring 912, and the one end of round bar 911 is connected with second camera 9, the screw thread is seted up to the surface of round bar 911, thereby make the round bar 911 more convenient with the connection of fixed ring 912, the bottom surface fixed mounting of connecting plate 914 has third camera 913, the bottom fixed mounting of unmanned aerial vehicle main part 1 has two sets of buffer gear.
Further, two sets of buffer gear is including connecting rod 3, and connecting rod 3 divide into two, keep away from each other between two connecting rods 3, and the one end of two connecting rods 3 all is connected with fixed horizontal pole 4, the surface fixed mounting of fixed horizontal pole 4 has two fixed loop bars 5, the surface of two fixed loop bars 5 is all fixed mounting has reinforcing rod 6, and the one end of reinforcing rod 6 is connected with fixed horizontal pole 4, be the triangle between reinforcing rod 6 and fixed horizontal pole 4, fixed loop bar 5, triangle structure has very high stability, can bear great weight and strength, triangle structure's structure is very firm simultaneously, because its each part can bear certain pressure and pulling force for unmanned aerial vehicle main part 1 is more stable at the in-process of descending.
Further, the cavity has all been seted up to the inner wall of two fixed loop bar 5, and installs the spring in the cavity, and the one end of spring is connected with telescopic link 7, through the effect of spring for telescopic link 7 can reciprocate in the inner wall cavity of fixed loop bar 5, thereby makes unmanned aerial vehicle main part 1 at the in-process that descends, can reduce unmanned aerial vehicle main part 1's buffering power, makes unmanned aerial vehicle main part 1 more stable at the in-process that descends.
Further, the outer surface fixed mounting of telescopic link 7 has circular bottom plate 8, and circular bottom plate 8 can increase the area of contact of unmanned aerial vehicle main part 1 with ground to stability when having increased unmanned aerial vehicle main part 1 and having fallen.
Further, the bottom end of the circular bottom plate 8 is stuck with rubber, the rubber has high elasticity, and the rubber can quickly recover after being stressed, so that the buffering force of the unmanned aerial vehicle main body 1 during landing can be reduced again.
Further, the bottom end fixed mounting of the unmanned aerial vehicle body 1 has a casing 915, and the casing 915 plays the effect of protecting the motor 917.
Working principle: the second camera 9 and the third camera 913 that are arranged through the top surface fixed mounting of the unmanned aerial vehicle main body 1 and the bottom connecting plate 914 surface of the unmanned aerial vehicle main body 1, the first camera 2, the second camera 9 and the third camera 913 are relatively arranged up and down through the unmanned aerial vehicle main body 1, the view angles of overlooking and looking up can be shot, thereby the scene and the target are more comprehensively captured, and the connecting plate 917 is driven to rotate, the second camera 9 can be subjected to three hundred sixty degrees of position adjustment, and simultaneously, the telescopic rod 7 can move up and down through the spring in the cavity of the inner wall of the fixed sleeve rod 5 in the falling process of the unmanned aerial vehicle main body 1, thereby the buffer force brought when the unmanned aerial vehicle main body 1 is lowered is reduced, and the unmanned aerial vehicle main body 1 is enabled to fall more stably.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (7)
1. The multi-station unmanned aerial vehicle comprises an unmanned aerial vehicle main body (1), and is characterized in that; the utility model discloses a unmanned aerial vehicle, unmanned aerial vehicle main part (1) top surface fixed mounting has a plurality of first cameras (2), and the bottom surface fixed mounting of unmanned aerial vehicle main part (1) has fastener (916), the surface of fastener (916) has circular draw-in groove, and fixed mounting has motor (917) in the circular draw-in groove, the one end of motor (917) is connected with connecting plate (914), the surface fixed mounting of connecting plate (914) has four fixed rings (912) of group, and the inner wall of fixed ring (912) has offered the screw thread, install round bar (911) in the inner wall of fixed ring (912), and the one end of round bar (911) is connected with second camera (9), the bottom surface fixed mounting of connecting plate (914) has third camera (913), the bottom fixed mounting of unmanned aerial vehicle main part (1) has two sets of buffer gear.
2. The multi-station drone of claim 1, wherein: the two groups of buffer mechanisms comprise connecting rods (3), the connecting rods (3) are divided into two groups, the two connecting rods (3) are far away from each other, one ends of the two connecting rods (3) are connected with a fixed cross rod (4), and two fixed loop bars (5) are fixedly arranged on the outer surface of the fixed cross rod (4).
3. The multi-station drone of claim 2, wherein: the outer surfaces of the two fixed loop bars (5) are fixedly provided with reinforcing bars (6), and one end of each reinforcing bar (6) is connected with a fixed cross bar (4).
4. A multi-station drone as claimed in claim 3, wherein: the inner walls of the two fixed loop bars (5) are provided with cavities, springs are arranged in the cavities, and one ends of the springs are connected with telescopic bars (7).
5. The multi-station drone of claim 4, wherein: the outer surface of the telescopic rod (7) is fixedly provided with a circular bottom plate (8).
6. The multi-station drone of claim 5, wherein: rubber is adhered to the bottom end of the round bottom plate (8).
7. The multi-station drone of claim 1, wherein: the bottom fixed mounting of unmanned aerial vehicle main part (1) has protective housing (915).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202321800623.8U CN220430532U (en) | 2023-07-10 | 2023-07-10 | Multi-station unmanned aerial vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202321800623.8U CN220430532U (en) | 2023-07-10 | 2023-07-10 | Multi-station unmanned aerial vehicle |
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Publication Number | Publication Date |
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CN220430532U true CN220430532U (en) | 2024-02-02 |
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CN202321800623.8U Active CN220430532U (en) | 2023-07-10 | 2023-07-10 | Multi-station unmanned aerial vehicle |
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CN (1) | CN220430532U (en) |
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2023
- 2023-07-10 CN CN202321800623.8U patent/CN220430532U/en active Active
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