CN212243807U - High-stability unmanned aerial vehicle - Google Patents
High-stability unmanned aerial vehicle Download PDFInfo
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- CN212243807U CN212243807U CN202021061955.5U CN202021061955U CN212243807U CN 212243807 U CN212243807 U CN 212243807U CN 202021061955 U CN202021061955 U CN 202021061955U CN 212243807 U CN212243807 U CN 212243807U
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Abstract
The utility model provides a high stable unmanned aerial vehicle, it includes the fuselage, the horn, including a motor, an end cap, a controller, and a cover plate, screw and undercarriage, a plurality of horns set up on the fuselage, the fuselage is kept away from to one end, is to disperse all around and appears, keeps away from the terminal top of fuselage and is provided with the motor cabinet, and the motor sets up on the motor cabinet, is used for providing power, including the motor shaft, motor shaft extension part up, the screw, detachable connects on the motor shaft, and follow the motor shaft and rotate, the undercarriage is buckled and is set up the end of keeping away from the fuselage on the horn, a support for when unmanned aerial vehicle rises and falls, horn below middle part position is provided with the lamp shade, the lamp shade. The utility model discloses a high stable unmanned aerial vehicle is a whole through setting up fuselage, horn and undercarriage, is provided with the motor cabinet on the horn, sets up the louvre on the undercarriage, and the screw is not foldable to screw up on the motor through the screw, thereby make unmanned aerial vehicle more stable when flying.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field, in particular to high stable unmanned aerial vehicle.
Background
Currently, drones are unmanned aircraft that are operated by radio remote control devices and self-contained program control devices, or can be operated autonomously, either completely or intermittently, by an on-board computer. Through the accumulation of technologies for many years and the rapid development of economy, the application scenarios of the existing unmanned aerial vehicle are more and more, for example: aerial photography, crop monitoring, vegetation protection, self-timer, express transportation, disaster relief, wildlife observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, movie and television photography, and the like. The connection of each part of the existing unmanned aerial vehicle is not stable enough.
The problem needs to be solved by providing a high-stability unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
The utility model provides a high stable unmanned aerial vehicle to solve the unmanned aerial vehicle among the prior art and have each parts to connect stable inadequately, and the distribution of each part is reasonable inadequately problem.
In order to solve the technical problem, the utility model adopts the technical scheme that: a highly stable drone, comprising:
a body;
the plurality of the horn arms are arranged on the machine body, one end of each horn arm is far away from the machine body and is in a peripheral divergent shape, and a motor base is arranged above the tail end of each horn arm far away from the machine body;
the motor is arranged on the motor base and used for providing power and comprises a motor shaft, and the extending part of the motor shaft faces upwards;
the propeller is detachably connected to the motor shaft and rotates along with the motor shaft;
and the undercarriage is bent and arranged at the tail end, far away from the fuselage, of the horn and used for supporting the unmanned aerial vehicle during rising and falling.
High stable unmanned aerial vehicle in, the fuselage upper surface is circular-arc, be provided with the louvre on the undercarriage, it is a plurality of the louvre distributes side by side.
In the high-stability unmanned aerial vehicle of the present invention, the horn comprises a front horn and a rear horn, two of the front horns are located on both sides of the vehicle body and are symmetrical with respect to a central vertical plane where the vehicle body is located in the length direction, and two of the rear horns are located on both sides of the vehicle body and are symmetrical with respect to a central vertical plane where the vehicle body is located in the length direction;
the horn is connected the fuselage is close to the upper surface position, preceding horn is connected along length direction's tip on the fuselage, back horn is connected and is kept away from preceding horn one end on the fuselage.
In the high-stability unmanned aerial vehicle, the extending direction of the front horn and the included angle of the side surface of the body are 60 degrees to 90 degrees, and the extending direction of the rear horn and the included angle of the side surface of the body are 30 degrees to 60 degrees, and the extending direction of the front horn and the extending direction of the rear horn are 30 degrees to 90 degrees.
In the high-stability unmanned aerial vehicle, the width of the horn is gradually reduced along the extending direction far away from the body, and a first rotating direction mark is arranged at the position of the horn close to the motor;
the propeller is provided with a second turning mark, and the first turning mark and the second turning mark are used for indicating the disassembly and assembly of the propeller.
High stable unmanned aerial vehicle in, the fuselage is provided with the opening along length direction's one end, the opening is provided with the module of making a video recording down in the opening, the module of making a video recording is used for making a video recording.
High stable unmanned aerial vehicle in, the module of making a video recording includes:
the camera shooting base is connected to the body and used for connection;
the rotating platform is of a plate-shaped structure, one end of the rotating platform is connected to the camera base, and a rotating motor is arranged at one end of the rotating platform, which is far away from the camera base, and is used for expanding the visual field;
the connecting seat is of a U-shaped structure, one end of the connecting seat is opened, and the other end of the connecting seat is connected to the rotating motor and used for connection;
the camera is connected in the opening of the connecting seat and used for shooting.
High stable unmanned aerial vehicle in, be provided with the battery case on the fuselage, the battery case sets up the fuselage downside, the battery case is used for the power supply.
In the high-stability unmanned aerial vehicle, a clamping part is arranged on one side of the battery box, which is close to the vehicle body, and a buckle bulge is arranged at the tail end of the clamping part;
the connection part of the machine body and the battery box is provided with a buckle groove corresponding to the buckle bulge, and the buckle bulge is clamped in the buckle groove.
High stable unmanned aerial vehicle in, horn below middle part position is provided with the lamp shade, the lamp shade is the convex closure form, the inside corresponding lamp shade position of horn is provided with the pilot lamp.
The utility model discloses compare in prior art, its beneficial effect is: the utility model discloses a high stable unmanned aerial vehicle is a whole through setting up fuselage, horn and undercarriage, is provided with the motor cabinet on the horn, sets up the louvre on the undercarriage, and the screw is not foldable to screw up on the motor through the screw, thereby make unmanned aerial vehicle more stable when flying.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required to be used in the embodiments are briefly introduced below, and the drawings in the following description are only corresponding drawings of some embodiments of the present invention.
Fig. 1 and fig. 2 are schematic structural diagrams of the high-stability unmanned aerial vehicle of the present invention.
Fig. 3 is the utility model discloses a high stable unmanned aerial vehicle's explosion structure schematic diagram.
Fig. 4 is the utility model discloses a high stable unmanned aerial vehicle's the explosion structure schematic diagram of the module of making a video recording.
The camera comprises a main body 1, a main body 2, a machine arm 3, a motor 4, a propeller 5, an undercarriage 6, a camera module 7, a battery box 21, a motor base 22, a lampshade 23, a first rotating mark 24, a front machine arm 25, a rear machine arm 41, a second rotating mark 51, a heat dissipation hole 61, a rotating base 62, a rotating table 63, a connecting seat 64, a camera 71 and a clamping part.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by the skilled in the art without creative work belong to the protection scope of the present invention.
In the present invention, the directional terms, such as "up", "down", "front", "back", "left", "right", "inner", "outer", "side", "top" and "bottom", refer to the orientation of the drawings, and the directional terms are used for illustration and understanding, but not for limiting the present invention.
The terms "first," "second," and the like in the terms of the present invention are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, nor should they be construed as limiting in any way.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
Each part of the unmanned aerial vehicle in the prior art is not stable enough.
Following do the utility model provides a pair of can solve above technical problem's high stable unmanned aerial vehicle's preferred embodiment.
Please refer to fig. 1, fig. 2, fig. 3 and fig. 4, wherein fig. 1 and fig. 2 are schematic structural diagrams of the high-stability unmanned aerial vehicle of the present invention, fig. 3 is a schematic structural diagram of the high-stability unmanned aerial vehicle of the present invention, and fig. 4 is a schematic structural diagram of the camera module of the high-stability unmanned aerial vehicle of the present invention.
In the drawings, elements having similar structures are denoted by the same reference numerals.
The utility model provides a high stable unmanned aerial vehicle, it includes fuselage 1, horn 2, motor 3, screw 4 and undercarriage 5, fuselage 1 is the square form, it is smooth and mellow all around, fuselage 1 upper surface is circular-arc, a plurality of horns 2 set up on fuselage 1, fuselage 1 is kept away from to one end, it is all around to disperse the shape, it is provided with motor cabinet 21 to keep away from the terminal top of fuselage 1, electrode cabinet 21 is cylindric, one end opening, the inside wall is linked together with horn 2, the wire that extends in horn 2 connects motor 3 in motor cabinet 21, it can also form the air current passageway to link together, convenient heat dissipation; the width of the machine arm 2 is gradually reduced along the extension direction far away from the machine body 1, a first turning mark 23 is arranged at the position, close to the motor 3, of the machine arm 2, and the first turning mark 23 is used for indicating the disassembly and assembly of the propeller 4; the horn 2 comprises front horns 24 and rear horns 25, the two front horns 24 are positioned on two sides of the body 1 and are symmetrical about a central vertical plane where the length direction of the body 1 is positioned, and the two rear horns 25 are positioned on two sides of the body 1 and are symmetrical about the central vertical plane where the length direction of the body 1 is positioned; the included angle between the extending direction of the front horn 24 and the side surface of the machine body 1 is 60 degrees to 90 degrees, and the included angle between the extending direction of the rear horn 25 and the side surface of the machine body 1 is 30 degrees to 60 degrees, and the included angle between the extending direction of the front horn 24 on the same side surface and the extending direction of the rear horn 25 is 30 degrees to 90 degrees. The horn 2 is connected and is being close to the upper surface position at fuselage 1, and screw 4 rotates the process and can not touch fuselage 1, and preceding horn 24 is connected and is followed length direction's tip on fuselage 1, and preceding horn 24 one end is kept away from on fuselage 1 to back horn 25 connection. The spacing distance between four horn 2 each other is great, and four motor cabinet 21 intervals are great, and screw 4 be provided with sufficient space, can not mutual interference, and unmanned aerial vehicle flight is stable.
The motor 3 is arranged on the motor base 21 and used for providing power and comprises a motor shaft, and the extending part of the motor shaft faces upwards; the propeller 4 is detachably connected to the motor shaft and rotates along with the motor shaft; screw 4 designs as an organic whole, and stable in structure is provided with second rotation direction mark 41 on screw 4, and second rotation direction mark 41 is used for instructing the dismouting of screw 4, corresponds on screw 4 and is provided with the dedicated screw of screw 4, looks at first rotation direction mark 23 and second rotation direction mark 41 and just can screw up or loosen the screw, carries out the dismouting to screw 4.
The undercarriage 5 is bent and arranged at the tail end, far away from the airframe 1, of the aircraft arm 2 and is used for supporting the unmanned aerial vehicle during rising and falling. Be provided with louvre 51 on the undercarriage 5, a plurality of louvres 51 distribute side by side, inside louvre 51 intercommunication horn 2, intercommunication motor cabinet 21 for the heat dissipation, undercarriage 5, horn 2 and fuselage 1 set up to a whole, and overall structure is firm.
Referring to fig. 4, the camera module 6 includes a camera base 61, a rotary table 62, a connecting base 63 and a camera 64, the camera base 61 is connected to the body 1 for connection; the rotating platform 62 is of a plate-shaped structure, one end of the rotating platform is connected to the camera base 61, and one end of the rotating platform, which is far away from the camera base 61, is provided with a rotating motor for expanding the visual field; the connecting seat 63 is in a U-shaped structure, one end of the connecting seat is open, and the other end of the connecting seat is connected to the rotating motor and used for connection; a camera 64 is attached in the opening of the attachment base 63 for taking a picture.
The utility model discloses a theory of operation: take out unmanned aerial vehicle, fix battery case 7 on fuselage 1, screw 4 is loaded on, screws up 4 special screws of screw, and motor 3 power supply is given to battery case 7, and motor 3 drives screw 4 and rotates, and then drives unmanned aerial vehicle flight, uses the remote controller that matches with unmanned aerial vehicle to control unmanned aerial vehicle's flight.
This completes the use of the high-stability drone of the preferred embodiment.
In summary, although the present invention has been described with reference to the preferred embodiments, the above-described preferred embodiments are not intended to limit the present invention, and those skilled in the art can make various changes and modifications without departing from the spirit and scope of the present invention, so that the scope of the present invention shall be determined by the scope of the appended claims.
Claims (10)
1. A high stable unmanned aerial vehicle, comprising:
a body;
the plurality of the horn arms are arranged on the machine body, one end of each horn arm is far away from the machine body and is in a peripheral divergent shape, and a motor base is arranged above the tail end of each horn arm far away from the machine body;
the motor is arranged on the motor base and used for providing power and comprises a motor shaft, and the extending part of the motor shaft faces upwards;
the propeller is detachably connected to the motor shaft and rotates along with the motor shaft;
and the undercarriage is bent and arranged at the tail end, far away from the fuselage, of the horn and used for supporting the unmanned aerial vehicle during rising and falling.
2. The high-stability unmanned aerial vehicle according to claim 1, wherein the upper surface of the body is arc-shaped, and the undercarriage is provided with a plurality of heat dissipation holes, and the plurality of heat dissipation holes are distributed in parallel.
3. The high stability unmanned aerial vehicle of claim 1, wherein the arms comprise front arms and rear arms, the front arms are located on two sides of the fuselage and are symmetrical about a central vertical plane of the length direction of the fuselage, and the rear arms are located on two sides of the fuselage and are symmetrical about a central vertical plane of the length direction of the fuselage;
the horn is connected the fuselage is close to the upper surface position, preceding horn is connected along length direction's tip on the fuselage, back horn is connected and is kept away from preceding horn one end on the fuselage.
4. The high-stability unmanned aerial vehicle of claim 3, wherein the angle between the extending direction of the front horn and the side surface of the fuselage is 60 ° -90 °, and the angle between the extending direction of the rear horn and the side surface of the fuselage is 30 ° -60 °, and the angle between the extending direction of the front horn and the extending direction of the rear horn is 30 ° -90 °.
5. The high-stability unmanned aerial vehicle of claim 1, wherein the arm has a width that gradually decreases along an extending direction away from the fuselage, and a first rotation mark is disposed on the arm near the motor;
the propeller is provided with a second turning mark, and the first turning mark and the second turning mark are used for indicating the disassembly and assembly of the propeller.
6. The high-stability unmanned aerial vehicle of claim 1, wherein an opening is formed in one end of the body in the length direction, the opening faces downward, and a camera module is arranged in the opening and used for shooting.
7. The high-stability unmanned aerial vehicle of claim 6, wherein the camera module comprises:
the camera shooting base is connected to the body and used for connection;
the rotating platform is of a plate-shaped structure, one end of the rotating platform is connected to the camera base, and a rotating motor is arranged at one end of the rotating platform, which is far away from the camera base, and is used for expanding the visual field;
the connecting seat is of a U-shaped structure, one end of the connecting seat is opened, and the other end of the connecting seat is connected to the rotating motor and used for connection;
the camera is connected in the opening of the connecting seat and used for shooting.
8. The high stability unmanned aerial vehicle of claim 1, wherein a battery compartment is provided on the fuselage, the battery compartment being provided on a lower side of the fuselage, the battery compartment being used for power supply.
9. The high-stability unmanned aerial vehicle of claim 8, wherein a clamping portion is arranged on one side, close to the body, of the battery box, and a clamping protrusion is arranged at the tail end of the clamping portion;
the connection part of the machine body and the battery box is provided with a buckle groove corresponding to the buckle bulge, and the buckle bulge is clamped in the buckle groove.
10. The high-stability unmanned aerial vehicle of claim 1, wherein a lampshade is arranged at a middle position below the arm, the lampshade is convex, and an indicator lamp is arranged inside the arm corresponding to the lampshade.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021061955.5U CN212243807U (en) | 2020-06-09 | 2020-06-09 | High-stability unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021061955.5U CN212243807U (en) | 2020-06-09 | 2020-06-09 | High-stability unmanned aerial vehicle |
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| CN212243807U true CN212243807U (en) | 2020-12-29 |
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| CN202021061955.5U Active CN212243807U (en) | 2020-06-09 | 2020-06-09 | High-stability unmanned aerial vehicle |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113525666A (en) * | 2021-08-29 | 2021-10-22 | 贵州电网有限责任公司六盘水供电局 | Unmanned aerial vehicle for three-dimensional model scanning based on power transmission and transformation equipment |
| CN114514172A (en) * | 2020-12-31 | 2022-05-17 | 深圳市大疆创新科技有限公司 | Unmanned plane |
-
2020
- 2020-06-09 CN CN202021061955.5U patent/CN212243807U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114514172A (en) * | 2020-12-31 | 2022-05-17 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| CN113525666A (en) * | 2021-08-29 | 2021-10-22 | 贵州电网有限责任公司六盘水供电局 | Unmanned aerial vehicle for three-dimensional model scanning based on power transmission and transformation equipment |
| CN113525666B (en) * | 2021-08-29 | 2023-04-14 | 贵州电网有限责任公司六盘水供电局 | Unmanned aerial vehicle is used in three-dimensional model scanning based on power transmission and transformation equipment |
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