CN221273565U - Six rotor heavy load unmanned aerial vehicle of high stability - Google Patents
Six rotor heavy load unmanned aerial vehicle of high stability Download PDFInfo
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- CN221273565U CN221273565U CN202323335889.2U CN202323335889U CN221273565U CN 221273565 U CN221273565 U CN 221273565U CN 202323335889 U CN202323335889 U CN 202323335889U CN 221273565 U CN221273565 U CN 221273565U
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- 230000007246 mechanism Effects 0.000 claims abstract description 14
- 239000000872 buffer Substances 0.000 claims abstract description 12
- 239000000725 suspension Substances 0.000 claims abstract description 11
- 230000005540 biological transmission Effects 0.000 claims abstract description 4
- 230000003014 reinforcing effect Effects 0.000 claims description 4
- 238000003032 molecular docking Methods 0.000 claims 2
- 210000001503 joint Anatomy 0.000 description 6
- 230000003139 buffering effect Effects 0.000 description 4
- 238000009434 installation Methods 0.000 description 3
- 230000032258 transport Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, and provides a high-stability six-rotor heavy-duty unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body, a suspension bracket and a plurality of rotor wing mechanisms uniformly distributed in the circumferential direction of the unmanned aerial vehicle main body; each rotor mechanism includes: the device comprises a positioning clamping plate, a telescopic rod, a supporting pallet, a motor and paddles; the positioning clamping plate is arranged on the telescopic rod and is fixedly connected with the unmanned aerial vehicle main body; the telescopic rod is arranged on the unmanned aerial vehicle main body, and one end of the telescopic rod, which is far away from the positioning clamping plate, is provided with a supporting plate; a motor is arranged at the end part of the supporting plate; the motor is in transmission connection with the blade; the bottom of unmanned aerial vehicle main part is provided with the mounted frame that is used for carrying cargo, the bottom four sides angle department of mounted frame is provided with the buffer wheel respectively. The utility model supports goods through the suspension bracket, is suitable for transporting the goods, and is provided with the buffer wheels so as to provide buffer for the suspension bracket and the unmanned aerial vehicle body when the unmanned aerial vehicle body lands, thereby ensuring the landing stability of the unmanned aerial vehicle body.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a six-rotor heavy-duty unmanned aerial vehicle with high stability.
Background
Unmanned plane is called "unmanned plane" for short, is unmanned plane that utilizes radio remote control equipment and self-contained program control device to operate, or by on-vehicle computer completely or intermittently independently operate, unmanned plane can divide into for military use and civilian according to the application. For military purposes, unmanned aerial vehicles are classified into reconnaissance and drones. In civil aspect, the unmanned aerial vehicle and the industrial application are really just needed by the unmanned aerial vehicle; the method 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.
The utility model patent number CN202020289646.7 discloses a large-load unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, wherein the front cantilever group comprises three first cantilevers which extend outwards, the rear cantilever group comprises three second cantilevers which extend outwards, the end parts of the first cantilevers are positioned on the same straight line on a front projection surface, the end parts of the second cantilevers are positioned on the same straight line on the front projection surface, the lengths of the first cantilevers and the second cantilevers are equal, and rotor wing parts are arranged at the end parts of the first cantilevers and the end parts of the second cantilevers.
However, when the structure is used, the ends of the first cantilever and the second cantilever are distributed in a straight line, but the lengths of the first cantilever and the second cantilever of the structure are fixed and cannot be adjusted; and the supporting legs can not hang goods, are not suitable for transporting the goods, are not easy for guiding the goods, and are not easy for supporting and buffering the landing of the unmanned aerial vehicle.
Disclosure of utility model
The utility model mainly solves the problems that the lengths of a first cantilever and a second cantilever of the loading unmanned aerial vehicle in the prior art are fixed and cannot be adjusted; and the supporting leg can not hang the goods, is unsuitable technical problem such as transportation goods, proposes a six rotor heavy load unmanned aerial vehicle of high stability, supports the goods through the mounted frame, is fit for transporting the goods, provides the buffering for mounted frame and unmanned aerial vehicle main part when setting up the buffering wheel and being convenient for unmanned aerial vehicle main part to descend simultaneously, ensures its stability that descends.
The utility model provides a six-rotor heavy-duty unmanned aerial vehicle with high stability, which comprises the following components: the unmanned aerial vehicle comprises an unmanned aerial vehicle body, a suspension bracket and a plurality of rotor wing mechanisms which are uniformly distributed in the circumferential direction of the unmanned aerial vehicle body;
Each rotor mechanism comprising: the device comprises a positioning clamping plate, a telescopic rod, a supporting pallet, a motor and paddles;
The positioning clamping plate is arranged on the telescopic rod and is fixedly connected with the unmanned aerial vehicle main body;
The telescopic rod is arranged on the unmanned aerial vehicle main body, and one end of the telescopic rod, which is far away from the positioning clamping plate, is provided with a supporting plate; a motor is arranged at the end part of the supporting plate; the motor is in transmission connection with the blade;
the bottom of unmanned aerial vehicle main part is provided with the mounted frame that is used for carrying cargo, the bottom four sides angle department of mounted frame is provided with the buffer wheel respectively.
Preferably, the end of the supporting pallet is provided with a motor through a placing plate.
Preferably, the output end of the motor is provided with a mounting seat, and the mounting seat is provided with a blade.
Preferably, the unmanned aerial vehicle main body is provided with a reinforced card cover.
Preferably, a controller is arranged on the reinforcing card cover, and a GPS navigation device is arranged on one side of the controller.
Preferably, a reducing cover is arranged on the unmanned aerial vehicle main body;
The reinforced card cover and the controller are positioned in the reduction cover, and the GPS navigation device penetrates through the reduction cover and extends out of the reduction cover.
Preferably, a plurality of butt joint clamping seats are arranged at the top of the suspension bracket;
the butt joint cassette is connected with unmanned aerial vehicle main part bottom.
Preferably, the number of rotor mechanisms is six.
Compared with the prior art, the six-rotor heavy-duty unmanned aerial vehicle with high stability has the following advantages:
1. The utility model has simple overall design, reasonable structure and high stability, supports goods through the corresponding cooperation of each structure and is suitable for transporting the goods, and meanwhile, the buffer wheels are arranged to provide buffer and support for the suspension frame and the unmanned aerial vehicle body when the unmanned aerial vehicle body lands, so that the landing stability of the unmanned aerial vehicle body is ensured.
2. In rotor mechanism, location cardboard, telescopic link, support layer board, place board etc. simultaneously can regard as firm heavy load subassembly, easily the goods guide, can also ensure the stability when this unmanned aerial vehicle transports simultaneously.
3. Through the control telescopic link is flexible, adjusts the interval between each corresponding telescopic link upper structure and the unmanned aerial vehicle main part to reduce the windage, stability when can effectually guaranteeing this unmanned aerial vehicle operation has good practicality in the time of facilitating the use.
Drawings
Fig. 1 is a schematic structural view of a high-stability six-rotor heavy-duty unmanned aerial vehicle provided by the utility model;
fig. 2 is a front view of a high stability six-rotor heavy-duty unmanned aerial vehicle provided by the utility model;
FIG. 3 is a schematic view of a portion of a high stability six-rotor heavy duty unmanned aerial vehicle according to the present utility model;
Fig. 4 is a schematic structural view of an unmanned aerial vehicle main body, a reinforced clamping cover, a positioning clamping plate, a telescopic rod and a hanging frame.
The reference numerals are: 1. an unmanned aerial vehicle main body; 2. positioning a clamping plate; 3. a telescopic rod; 4. a supporting pallet; 5. placing a plate; 6. a motor; 7. a mounting base; 8. a paddle; 9. reinforcing the card cover; 10. a hanging frame; 11. a buffer wheel; 12. a butt joint clamping seat; 13. a controller; 14. a subtractive cap; 15. GPS navigation device.
Detailed Description
In order to make the technical problems solved by the utility model, the technical scheme adopted and the technical effects achieved clearer, the utility model is further described in detail below with reference to the accompanying drawings and the embodiments. It is to be understood that the specific embodiments described herein are merely illustrative of the utility model and are not limiting thereof. It should be further noted that, for convenience of description, only some, but not all of the matters related to the present utility model are shown in the accompanying drawings.
As shown in fig. 1 to 4, the six-rotor heavy-duty unmanned aerial vehicle with high stability provided by the embodiment of the utility model comprises: unmanned aerial vehicle main part 1, mounted frame 10 and a plurality of rotor mechanisms of evenly distributed in the circumferencial direction of unmanned aerial vehicle main part 1. In the utility model, the number of the rotor wing mechanisms is six, so that six-rotor-wing heavy-load unmanned flying is realized.
Each rotor mechanism comprising: the positioning clamping plate 2, the telescopic rod 3, the supporting plate 4, the motor 6 and the blade 8. The positioning clamping plate 2 is arranged on the telescopic rod 3, and the positioning clamping plate 2 is fixedly connected with the unmanned aerial vehicle main body 1; the telescopic rod 3 is arranged on the unmanned aerial vehicle main body 1, and a supporting plate 4 is arranged at one end of the telescopic rod 3 far away from the positioning clamping plate 2; a motor 6 is arranged at the end part of the supporting plate 4; the motor 6 is in transmission connection with the blade 8. Specifically, the end of the supporting pallet 4 is provided with a motor 6 through a placing plate 5. The output end of the motor 6 is provided with a mounting seat 7, and a blade 8 is arranged on the mounting seat 7.
In rotor mechanism, location cardboard 2, telescopic link 3, support layer board 4, place board 5 etc. can regard as firm heavy load subassembly simultaneously, can also ensure the stability when this unmanned aerial vehicle transports simultaneously. The telescopic rods 3 can be telescopic and adjustable according to the requirements, so that the length of the rotor wing mechanism can be adjusted, and the distance between the structure on each telescopic rod 3 and the unmanned aerial vehicle main body 1 can be adjusted, thereby reducing wind resistance and effectively ensuring the stability of the unmanned aerial vehicle during operation; and can adapt to more working conditions.
The bottom of unmanned aerial vehicle main part 1 is provided with the mounted frame 10 that is used for carrying cargo, the bottom four sides angle department of mounted frame 10 is provided with buffer wheel 11 respectively. A plurality of butt joint clamping seats 12 are arranged at the top of the suspension bracket 10; the butt joint cassette 12 is connected with the bottom of the unmanned aerial vehicle main body 1, and the butt joint cassette 12 guarantees the stability of mounted frame 10 installation.
When the unmanned aerial vehicle is used, a worker places goods to be transported at the bottom of the unmanned aerial vehicle body 1, supports the goods through the hanging frame 10, supports and buffers the hanging frame 10 and the unmanned aerial vehicle body 1 through the buffer wheel 11, and is convenient for buffering the hanging frame 10 and the unmanned aerial vehicle body 1 when the following unmanned aerial vehicle body 1 lands, so that the landing stability of the unmanned aerial vehicle body 1 is ensured.
In addition, a reinforcing card cover 9 is provided on the unmanned aerial vehicle body 1. The reinforced card cover 9 is provided with a controller 13, and one side of the controller 13 is provided with a GPS navigation device 15. The unmanned aerial vehicle main body 1 is provided with a reducing cover 14; the reinforcement card housing 9 and the controller 13 are positioned in the reduction housing 14, and the GPS navigation device 15 penetrates the reduction housing 14 and protrudes from the reduction housing 14.
When the unmanned aerial vehicle is used, the motor 6 is controlled to be started through the controller 13, the installation seat 7 is driven to rotate, the paddle 8 is driven to rotate when the installation seat 7 rotates, so that the unmanned aerial vehicle can move, and meanwhile, navigation and positioning can be carried out through the GPS navigation device 15. The controller 13 and the GPS navigation device 15 are already well known in the art for performing flight control and line location navigation of a drone, and conventional drones are covered by this technical means, so the present utility model does not describe the controller 13 and the GPS navigation device 15 too much.
According to the high-stability six-rotor heavy-duty unmanned aerial vehicle, the suspension frame 10 is used for supporting cargoes, and meanwhile, the buffer wheels 11 are arranged, so that the suspension frame 10 and the unmanned aerial vehicle body 1 can be conveniently buffered when the unmanned aerial vehicle body 1 falls, and the falling stability of the unmanned aerial vehicle is ensured; through control telescopic link 3 flexible, adjust the interval between structure and the unmanned aerial vehicle main part 1 on each telescopic link 3 to reduce windage, stability when can effectively guaranteeing this unmanned aerial vehicle operation.
Finally, it should be noted that: the above embodiments are only for illustrating the technical solution of the present utility model, and not for limiting the same; although the utility model has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments is modified or some or all of the technical features are replaced equivalently, so that the essence of the corresponding technical scheme does not deviate from the scope of the technical scheme of the embodiments of the present utility model.
Claims (8)
1. High-stability six-rotor heavy-duty unmanned aerial vehicle, which is characterized by comprising: the unmanned aerial vehicle comprises an unmanned aerial vehicle main body (1), a suspension bracket (10) and a plurality of rotor wing mechanisms which are uniformly distributed in the circumferential direction of the unmanned aerial vehicle main body (1);
Each rotor mechanism comprising: the device comprises a positioning clamping plate (2), a telescopic rod (3), a supporting pallet (4), a motor (6) and paddles (8);
The positioning clamping plate (2) is arranged on the telescopic rod (3), and the positioning clamping plate (2) is fixedly connected with the unmanned aerial vehicle main body (1);
the telescopic rod (3) is arranged on the unmanned aerial vehicle main body (1), and a supporting plate (4) is arranged at one end of the telescopic rod (3) far away from the positioning clamping plate (2); a motor (6) is arranged at the end part of the supporting plate (4); the motor (6) is in transmission connection with the blade (8);
the bottom of unmanned aerial vehicle main part (1) is provided with mounted frame (10) that are used for carrying cargo, bottom four corners department of mounted frame (10) is provided with buffer wheel (11) respectively.
2. The six-rotor heavy-duty unmanned aerial vehicle with high stability according to claim 1, wherein the end of the supporting pallet (4) is provided with a motor (6) by means of a placement plate (5).
3. The six-rotor heavy-duty unmanned aerial vehicle with high stability according to claim 2, wherein the output end of the motor (6) is provided with a mounting seat (7), and the mounting seat (7) is provided with a blade (8).
4. The six-rotor heavy-duty unmanned aerial vehicle with high stability according to claim 1, wherein the unmanned aerial vehicle body (1) is provided with a reinforcing clamping cover (9).
5. The six-rotor heavy-duty unmanned aerial vehicle with high stability according to claim 4, wherein the reinforced card cover (9) is provided with a controller (13), and one side of the controller (13) is provided with a GPS navigation device (15).
6. The six-rotor heavy-duty unmanned aerial vehicle with high stability according to claim 5, wherein a reducing cover (14) is arranged on the unmanned aerial vehicle main body (1);
The reinforced card cover (9) and the controller (13) are positioned in the reducing cover (14), and the GPS navigation device (15) penetrates through the reducing cover (14) and extends out of the reducing cover (14).
7. The six-rotor heavy-duty unmanned aerial vehicle with high stability according to claim 1, wherein a plurality of docking seats (12) are arranged at the top of the suspension bracket (10);
the docking clamping seat (12) is connected with the bottom of the unmanned aerial vehicle main body (1).
8. The high stability six rotor heavy duty unmanned aerial vehicle of claim 1, wherein the number of rotor mechanisms is six.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323335889.2U CN221273565U (en) | 2023-12-08 | 2023-12-08 | Six rotor heavy load unmanned aerial vehicle of high stability |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323335889.2U CN221273565U (en) | 2023-12-08 | 2023-12-08 | Six rotor heavy load unmanned aerial vehicle of high stability |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221273565U true CN221273565U (en) | 2024-07-05 |
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ID=91708395
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323335889.2U Active CN221273565U (en) | 2023-12-08 | 2023-12-08 | Six rotor heavy load unmanned aerial vehicle of high stability |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221273565U (en) |
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2023
- 2023-12-08 CN CN202323335889.2U patent/CN221273565U/en active Active
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