CN216817242U

CN216817242U - Be used for autopilot unmanned aerial vehicle

Info

Publication number: CN216817242U
Application number: CN202122188005.XU
Authority: CN
Inventors: 张兰
Original assignee: Yixian Intelligent Technology Co ltd
Current assignee: Yixian Intelligent Technology Co ltd
Priority date: 2021-09-10
Filing date: 2021-09-10
Publication date: 2022-06-24
Anticipated expiration: 2031-09-10

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a robot for automatic driving, which comprises an unmanned aerial vehicle main body, a servo motor, a camera, a storage battery, a current sensor, a GPS navigator, an ultrasonic sensor and a controller, wherein supporting legs are fixedly connected to the periphery of the unmanned aerial vehicle main body, pulleys are fixedly connected to the bottom ends of the supporting legs, energy absorption pads are fixedly connected to the periphery of the unmanned aerial vehicle main body, the energy absorption pads are fixedly connected to one ends of springs, and the other ends of the springs are fixedly connected to the inner portion of one side, close to the center of the unmanned aerial vehicle main body, of a protective shell. The unmanned aerial vehicle collision protection device is provided with the height, position and direction control device, so that the height, position and electric quantity of the unmanned aerial vehicle main body can be monitored, the unmanned aerial vehicle main body can be controlled to fly safely, the direction of the camera can be adjusted, accurate camera shooting is facilitated, the collision performance of the unmanned aerial vehicle is enhanced, the damage to the unmanned aerial vehicle is reduced, and the service life of the unmanned aerial vehicle is prolonged.

Description

Be used for autopilot unmanned aerial vehicle

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle for automatic driving.

Background

Unmanned aerial vehicle is unmanned aircraft, is fit for those dangerous operations, and unmanned aerial vehicle can be divided into for military use and civilian according to the application, and for military use aspect, unmanned aerial vehicle divide can be reconnaissance aircraft and target drone, and civilian aspect, unmanned aerial vehicle is comparatively extensive in the application in fields such as aerial photography, agriculture, miniature autodyne, express delivery transportation, disaster relief, electric power are patrolled and examined, the movie & TV is shot, at present.

The current unmanned aerial vehicle that is used for automatic pilot, inconvenient simultaneous control unmanned aerial vehicle height, position, electric quantity and the angle of making a video recording can not guarantee that unmanned aerial vehicle stably flies, and anticollision effect is poor, damages unmanned aerial vehicle easily, therefore needs to design one kind and is used for automatic pilot unmanned aerial vehicle urgently.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide an unmanned aerial vehicle for automatic driving, and aims to solve the problems that the existing unmanned aerial vehicle for automatic driving proposed in the background technology is inconvenient to control the height, the position, the electric quantity and the camera angle of the unmanned aerial vehicle at the same time, cannot ensure the stable flight of the unmanned aerial vehicle, has poor anti-collision effect, and is easy to damage the unmanned aerial vehicle.

In order to achieve the purpose, the utility model provides the following technical scheme: the unmanned aerial vehicle comprises an unmanned aerial vehicle main body, a servo motor, a camera, a storage battery, a current sensor, a GPS navigator, an ultrasonic sensor and a controller, wherein supporting legs are fixedly connected to the periphery of the unmanned aerial vehicle main body, the bottom ends of the supporting legs are fixedly connected with pulleys, energy absorption pads are fixedly connected to the periphery of the unmanned aerial vehicle main body, the energy absorption pads are fixedly connected to one ends of springs, the other ends of the springs are fixedly connected to the inner portion of one side, close to the center of the unmanned aerial vehicle main body, of a protective shell, and cushion pads are fixedly connected to one side, far away from the center of the unmanned aerial vehicle main body, of the protective shell;

unmanned aerial vehicle main part bottom has linked firmly the mount pad, and the mount pad right side has linked firmly servo motor, servo motor pivot is inserted and is established the mount pad and has linked firmly carousel one, and a carousel tooth connects carousel two, carousel two rotates to be connected in the mount pad rear end, two bottoms of carousel have linked firmly camera one end, and the camera other end passes the through-hole setting in the mount pad bottom, the inside rear end of unmanned aerial vehicle main part links firmly battery, current sensor and GPS navigator, the battery links firmly on the current sensor right side, and has linked firmly the GPS navigator on the battery right side.

Preferably, the supporting legs are provided with four groups, and four groups of supporting legs are evenly arranged around the unmanned aerial vehicle main body in an annular shape.

Preferably, four rows of springs are arranged on the outer surface of the energy absorption pad, three groups of springs are arranged on each row, and the three groups of springs are uniformly arranged inside the protective shell.

Preferably, protective housing and blotter all are the arc setting, and protective housing radian size equals blotter radian size.

Preferably, the inside left side of unmanned aerial vehicle main part has linked firmly ultrasonic sensor, the inside right side of unmanned aerial vehicle main part has linked firmly the controller.

Preferably, the storage battery is electrically connected with a servo motor, a camera, a current sensor, a GPS navigator, an ultrasonic sensor and a controller, and the controller is electrically connected with the servo motor, the camera, the current sensor, the GPS navigator and the ultrasonic sensor.

Compared with the prior art, the utility model has the beneficial effects that:

1. through being provided with the height, the position, direction control device, unmanned aerial vehicle main part takes off during the use, ultrasonic sensor transmits altitude information and gives the controller, current sensor transmits electric quantity information and gives the controller, GPS navigator transmits positional information and gives the controller, then the controller transmits information transfer for remote control equipment, the flight of remote control equipment instruction, servo motor makes the camera redirecting at last is opened to the controller, the camera carries out the accuracy and makes a video recording, set up the height that is favorable to monitoring the unmanned aerial vehicle main part like this, position and electric quantity, be convenient for control unmanned aerial vehicle main part safety flight, and can adjust the camera direction, be convenient for the accuracy is made a video recording.

2. Through being provided with collision protection device, the blotter tentatively cushions during the use, then the spring provides the bounce-back buffering, and last energy-absorbing pad further cushions, is provided with like this and does benefit to reinforcing unmanned aerial vehicle collision performance, alleviates the harm that unmanned aerial vehicle received, extension unmanned aerial vehicle life.

Drawings

FIG. 1 is a schematic front view of the structure of the present invention;

FIG. 2 is a schematic top view of the structure of the present invention;

FIG. 3 is a schematic sectional elevation view of the structure of the present invention;

FIG. 4 is a schematic top view of the structure of the present invention.

In the figure: 1. an unmanned aerial vehicle main body; 2. supporting legs; 3. a pulley; 4. an energy absorbing pad; 5. a spring; 6. a protective housing; 7. a cushion pad; 8. a mounting seat; 9. a servo motor; 10. a first rotating disc; 11. a second rotating disc; 12. a through hole; 13. a camera; 14. a storage battery; 15. a current sensor; 16. a GPS navigator; 17. an ultrasonic sensor; 18. and a controller.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-4, an embodiment of the present invention is shown:

a unmanned aerial vehicle for automatic driving comprises an unmanned aerial vehicle main body 1, a servo motor 9, a camera 13, a storage battery 14, a current sensor 15, a GPS navigator 16, an ultrasonic sensor 17 and a controller 18, wherein supporting legs 2 are fixedly connected around the unmanned aerial vehicle main body 1, the bottom ends of the supporting legs 2 are fixedly connected with pulleys 3, energy absorption pads 4 are fixedly connected around the unmanned aerial vehicle main body 1, the energy absorption pads 4 are fixedly connected with one ends of springs 5, the other ends of the springs 5 are fixedly connected to the inner portion of one side, close to the center of the unmanned aerial vehicle main body 1, of a protective shell 6, and cushion pads 7 are fixedly connected to one side, far away from the center of the unmanned aerial vehicle main body 1, of the protective shell 6;

1 bottom of unmanned aerial vehicle main part has linked firmly mount pad 8, and the 8 right sides of mount pad have linked firmly servo motor 9, servo motor 9 pivot is inserted and is established mount pad 8 and linked firmly carousel one 10, and carousel one 10 joggle carousel two 11, carousel two 11 rotate to be connected in the 8 rear ends of mount pad, carousel two 11 bottoms have linked firmly camera 13 one end, and the camera 13 other end passes through-hole 12 and sets up in 8 bottoms of mount pad, 1 inside rear end of unmanned aerial vehicle main part has linked firmly battery 14, current sensor 15 and GPS navigator 16, battery 14 links firmly on current sensor 15 right sides, and has linked firmly GPS navigator 16 on the battery 14 right side.

Further, supporting legs 2 are provided with four groups, and four groups of supporting legs 2 are that the annular evenly sets up around unmanned aerial vehicle main part 1, are favorable to providing stable support for unmanned aerial vehicle main part 1, and unmanned aerial vehicle main part 1 of being convenient for takes off and descends.

Further, the outer surface of the energy absorption pad 4 is provided with four rows of springs 5, each row is provided with three groups of springs 5, and the three groups of springs 5 are uniformly arranged inside the protective shell 6, so that stable support for the protective shell 6 is facilitated, and rebound acting force is provided for the protective shell 6.

Further, protecting sheathing 6 and cushion 7 all are the arc setting, and protecting sheathing 6 radian size equals 7 radian sizes of cushion, is favorable to following each angle protection, alleviates unmanned aerial vehicle main part 1 and receives effort intensity.

Further, 1 inside left sides of unmanned aerial vehicle main part have linked firmly

ultrasonic sensor

17, and 1 inside right sides of unmanned aerial vehicle main part have linked firmly controller 18, are favorable to just can realizing altitude control near ground, realize that unmanned aerial vehicle no matter can both steadily fly at high altitude or low latitude.

Further, the storage battery 14 is electrically connected with the servo motor 9, the camera 13, the current sensor 15, the GPS navigator 16, the ultrasonic sensor 17 and the controller 18, and the controller 18 is electrically connected with the servo motor 9, the camera 13, the current sensor 15, the GPS navigator 16 and the ultrasonic sensor 17, so that the control of each device is facilitated, the flight task is completed cooperatively, and electric power is provided for each device.

The working principle is as follows: when the unmanned aerial vehicle needs to fly and finish a shooting task, firstly, the unmanned aerial vehicle body 1 starts to take off, the ultrasonic sensor 17 senses the height information of the unmanned aerial vehicle body 1 and transmits the information to the controller 18, the current sensor 15 senses the electric quantity information of the storage battery 14 and transmits the information to the controller 18, the GPS navigator 16 senses the position information of the unmanned aerial vehicle body 1 and transmits the information to the controller 18, then the controller 18 transmits the information to the remote control equipment, the remote control equipment controls the controller 18 to instruct the unmanned aerial vehicle body 1 to fly according to the feedback data, finally, the controller 18 controls the servo motor 9 to rotate, the servo motor 9 changes the direction of the camera 13 through the first rotating disc 10 and the second rotating disc 11, so that the camera 13 can conveniently shoot, when the unmanned aerial vehicle needs to be protected in collision, firstly, the collision primarily buffers the impact force through the cushion 7, then the protective shell 6 compresses the spring 5 to provide rebound buffering force, and finally the spring 5 contracts the protective shell 6 to extrude the energy absorption pad 4 to further buffer the impact force, so that the acting force on the unmanned aerial vehicle main body 1 is reduced.

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 invention may be embodied in other specific forms without departing from the spirit or essential attributes 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

1. The utility model provides a be used for autopilot unmanned aerial vehicle, includes unmanned aerial vehicle main part (1), servo motor (9), camera (13), battery (14), current sensor (15), GPS navigator (16), ultrasonic sensor (17) and controller (18), its characterized in that: the unmanned aerial vehicle is characterized in that supporting legs (2) are fixedly connected to the periphery of the unmanned aerial vehicle main body (1), pulleys (3) are fixedly connected to the bottom ends of the supporting legs (2), energy absorption pads (4) are fixedly connected to the periphery of the unmanned aerial vehicle main body (1), the energy absorption pads (4) are fixedly connected to one ends of springs (5), the other ends of the springs (5) are fixedly connected to the inner portion of one side, close to the center of the unmanned aerial vehicle main body (1), of the protective shell (6), and cushion pads (7) are fixedly connected to one side, far away from the center of the unmanned aerial vehicle main body (1), of the protective shell (6);

unmanned aerial vehicle main part (1) bottom has linked firmly mount pad (8), and mount pad (8) right side has linked firmly servo motor (9), servo motor (9) pivot is inserted and is established mount pad (8) and has linked firmly carousel one (10), and carousel one (10) tooth joint carousel two (11), carousel two (11) rotate to be connected in mount pad (8) rear end, carousel two (11) bottom has linked firmly camera (13) one end, and the camera (13) other end passes through-hole (12) and sets up in mount pad (8) bottom, unmanned aerial vehicle main part (1) inside rear end links firmly battery (14), current sensor (15) and GPS navigator (16), battery (14) link firmly on current sensor (15) right side, and battery (14) have linked firmly GPS navigator (16) on the right side.

2. A drone for automatic piloting according to claim 1, characterized in that: the unmanned aerial vehicle is characterized in that four groups of supporting legs (2) are arranged, and the four groups of supporting legs (2) are uniformly arranged around the unmanned aerial vehicle main body (1) in an annular shape.

3. A drone for automatic piloting according to claim 1, characterized in that: the energy-absorbing pad (4) surface is provided with four rows of springs (5), and every row is provided with three group of springs (5), three group of springs (5) evenly set up inside protecting sheathing (6).

4. A drone for automatic piloting according to claim 1, characterized in that: protective housing (6) and blotter (7) all are the arc setting, and protective housing (6) radian size equals blotter (7) radian size.

5. A drone for automatic piloting according to claim 1, characterized in that: the inside left side of unmanned aerial vehicle main part (1) has linked firmly ultrasonic sensor (17), the inside right side of unmanned aerial vehicle main part (1) has linked firmly controller (18).

6. A drone for automatic piloting according to claim 1, characterized in that: the intelligent GPS navigation system is characterized in that the storage battery (14) is electrically connected with a servo motor (9), a camera (13), a current sensor (15), a GPS navigator (16), an ultrasonic sensor (17) and a controller (18), and the controller (18) is electrically connected with the servo motor (9), the camera (13), the current sensor (15), the GPS navigator (16) and the ultrasonic sensor (17).