CN216674445U

CN216674445U - High-endurance bird-repelling unmanned aerial vehicle based on solar energy

Info

Publication number: CN216674445U
Application number: CN202123253209.3U
Authority: CN
Inventors: 赵鹏宇
Original assignee: Shijiazhuang Second Experimental Middle School
Current assignee: Shijiazhuang Second Experimental Middle School
Priority date: 2021-12-22
Filing date: 2021-12-22
Publication date: 2022-06-07
Anticipated expiration: 2031-12-22

Abstract

The utility model discloses a high-endurance bird-repelling unmanned aerial vehicle based on solar energy, which relates to the field of bird repelling of unmanned aerial vehicles and comprises a machine body, a connecting plate and a main shaft, wherein the connecting plate is in an Contraband-type structural mode, the connecting plate is arranged below the machine body, the main shaft is movably connected to the connecting plate, four corners of the side edge of the machine body are provided with fixedly connected wings, the bottom end of the machine body is provided with a disc, the machine body and the disc are connected through screw locking, the top end of the machine body is symmetrically provided with vertical plates, the top ends of the vertical plates are provided with solar panels, an inclined angle is formed between each solar panel and the machine body, a limiting groove is arranged inside the disc, the limiting groove is arranged at the central part of the disc, and the limiting groove is in a countersunk head mode in the disc. The bird repellent device can repel birds, does not need power supply, and is more environment-friendly.

Description

High-endurance bird-repelling unmanned aerial vehicle based on solar energy

Technical Field

The utility model relates to the field of bird repelling of unmanned aerial vehicles, in particular to a high-endurance bird repelling unmanned aerial vehicle based on solar energy.

Background

Bird repelling is also called bird repelling, and in a broad sense, all means for preventing harmful birds from invading the territory of a user, such as farms, orchards, wind power plants, military and civil airports, and the like, so that the work result of the user or the equipment safety is damaged are called bird repelling. Unmanned aerial vehicle now is extensive be used for the agricultural field, can be used for fertilizeing the orchard, water spray etc, when crops or orchard are ripe, probably there are many birds to steal early morning and destroy, the most traditional mode is the form of artifical patrol or placing the dummy, though there is certain effect, but long-term effect is unsatisfactory, the device that has unmanned aerial vehicle to drive the bird now also, but most devices all need the motor to drive, can't accomplish green's mode and carry out the expulsion to birds, and how unmanned aerial vehicle realizes long-time continuation of the journey also needs further improvement.

SUMMERY OF THE UTILITY MODEL

In order to solve the technical problems, the utility model provides the following technical scheme:

a high-endurance bird-repelling unmanned aerial vehicle based on solar energy comprises a machine body, a connecting plate and a main shaft, wherein the connecting plate is in an Contraband-type structural mode and is arranged below the machine body, the main shaft is movably connected to the connecting plate, wings which are fixedly connected are arranged at four corners of the side edge of the machine body, and a disc is arranged at the bottom end of the machine body;

the novel LED lamp is characterized in that transverse plates are symmetrically arranged on the main shaft, spot lamps are arranged at the end portions of the transverse plates, a waist-shaped groove is formed in the bottom end of the connecting plate, a first rotating plate is arranged on the main shaft, an auxiliary rod is arranged in the first rotating plate, and the auxiliary rod is designed in a right angle mode.

Furthermore, the machine body and the disc are connected through screw locking, vertical plates are symmetrically arranged at the top end of the machine body, a solar panel is arranged at the top end of each vertical plate, and an inclined angle is formed between each solar panel and the machine body.

Furthermore, a limiting groove is formed in the disc, the limiting groove is formed in the center of the disc, and the limiting groove is in a countersunk mode in the disc.

Furthermore, the top of main shaft is equipped with movable post, movable post with the main shaft is fixed connection the circumference side of activity post is equipped with a plurality of evenly distributed's ball, the ball activity is inlayed in the activity post, and the ball is in the area of activity post exceeds half.

Furthermore, the other end of the auxiliary rod is provided with a second rotating plate, the auxiliary rod is movably connected with the first rotating plate and the second rotating plate, the diameter of the auxiliary rod is smaller than the inner diameters of the first rotating plate and the second rotating plate, a cross shaft is arranged on the second rotating plate, and the cross shaft is fixedly connected with the second rotating plate.

Furthermore, be equipped with square piece on the cross axle, square piece is fixed on the connecting plate, be equipped with fixed connection's jib on the cross axle, and the jib is in the waist type groove, the bottom of jib is equipped with the balancing weight.

The utility model has the beneficial effects that:

1: through the connecting plate of this practical setting, the jib, parts such as balancing weight, when using, unmanned aerial vehicle can make the balancing weight produce the motion at other factors such as production speed difference or external wind-force, balancing weight itself has certain weight, make the back and forth swing that the shot-light can be ceaselessly in the air through the imitation pendulum clock motion mode, carry out the expulsion to birds, not only do not need the participation of electricity through this mode, and have certain weight through the balancing weight to have inertia, can swing very long time, when the energy saving, the efficiency of driving the bird has been improved.

2: through parts such as solar panel of this practical setting, when using, solar panel can absorb light, changes solar light into the electric energy, provides electric power for the device, when having realized energy-concerving and environment-protective, has prolonged the flight time of device.

Drawings

The accompanying drawings, which are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate embodiments of the utility model and together with the description serve to explain the principles of the utility model and not to limit the utility model. In the drawings:

fig. 1 is an isometric view of an integral apparatus in a solar-based high-endurance bird-repelling drone of the present invention;

fig. 2 is an isometric view of a connecting plate and other components of a high-endurance bird-repelling unmanned aerial vehicle based on solar energy according to the present invention;

fig. 3 is an isometric view of a disc component in a solar-based high endurance bird repellent drone of the present invention;

fig. 4 is an isometric view of the components such as the auxiliary rod in the high-endurance bird-repelling unmanned aerial vehicle based on solar energy.

In the figure: 1. a body; 2. a connecting plate; 3. a main shaft; 4. an airfoil; 5. a disc; 6. a vertical plate; 7. a solar panel; 8. a limiting groove; 9. a movable post; 10. a ball; 11. a transverse plate; 12. sending light; 13. a waist-shaped groove; 14. rotating the first plate; 15. an auxiliary lever; 16. a second rotating plate; 17. a horizontal axis; 18. a square block; 19. a boom; 20. and a balancing weight.

Detailed Description

The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are described herein for the purpose of illustration and explanation and not limitation.

Examples

As shown in fig. 1 to 4:

the utility model provides a high-endurance bird-repelling unmanned aerial vehicle based on solar energy, wherein,

including organism 1, connecting plate 2, main shaft 3, connecting plate 2 is the structural style of Contraband type, and connecting plate 2 is in the below of organism 1, main shaft 3 swing joint is in on connecting plate 2, be equipped with fixed connection's wing 4 on the side four corners of organism 1, the bottom of organism 1 is equipped with disc 5, organism 1 with disc 5 pays for the screw and connects, the top symmetry of organism 1 is equipped with perpendicular template 6, the top of perpendicular template 6 is equipped with solar panel 7, and solar panel 7 with there is the angle of slope between the organism 1, the inside of disc 5 is equipped with spacing groove 8.

Spacing groove 8 is in the central point of disc 5, and spacing groove 8 is in shape in the disc 5 is the countersunk head mode, the top of main shaft 3 is equipped with movable post 9, movable post 9 with main shaft 3 is fixed connection the circumference side of activity post 9 is equipped with a plurality of evenly distributed's ball 10, ball 10 activity is inlayed in the activity post 9, and ball 10 is in the area of activity post 9 exceeds half, the symmetry is equipped with diaphragm 11 on the main shaft 3, the tip of diaphragm 11 is provided with shot-light 12, the bottom of connecting plate 2 is equipped with waist type groove 13, be equipped with rotor plate 14 on the main shaft 3 be equipped with auxiliary rod 15 in the rotor plate 14, auxiliary rod 15 is the right angle design.

The other end of auxiliary rod 15 is equipped with rotor plate two 16, auxiliary rod 15 swing joint be in rotor plate one 14 with in rotor plate two 16, and the diameter of auxiliary rod 15 is less than rotor plate one 14 with the internal diameter of rotor plate two 16, be equipped with cross axle 17 on the rotor plate two 16, cross axle 17 with rotor plate two 16 is fixed connection, be equipped with square piece 18 on the cross axle 17, square piece 18 is fixed on the connecting plate 2, be equipped with fixed connection's jib 19 on the cross axle 17, and jib 19 is in among the waist type groove 13, the bottom of jib 19 is equipped with balancing weight 20.

Detailed methods of use and effects of the above examples: when we need drive the bird, through making wing 4 is rotatory, and the drive arrangement rises aloft, and when unmanned aerial vehicle flies in the sky, when turning round and producing the speed difference, perhaps when windy, under inertial effect, balancing weight 20 has certain weight, can make balancing weight 20 be in connecting plate 2 the motion that makes a round trip is realized in the waist type groove 13. The balance weight block 20 is connected with the suspension rod 19, and the suspension rod 19 is fixedly connected with the transverse shaft 17, so that the second rotating plate 16 can be driven to swing back and forth in a vertical space. Swing joint has in the two 16 rotating plates auxiliary rod 15, auxiliary rod 15 follows when changeing, can be in rotating plate one 14 with the inside round trip motion of two 16 rotating plates, because auxiliary rod 15 designs for the form of right angle, makes rotating plate one 14 realizes periodic swing in the horizontal space, rotating plate one 14 is connected on main shaft 3, pass through on main shaft 3 diaphragm 11 fixed connection shot-light 12 can make a round trip the swing, drives the bird. The round ball 10 on the movable column 9 is rotatably connected in the limiting groove 8 in the disc 5, so that the main shaft 3 is more stable to rotate. Solar panel 7 that the top of organism 1 was equipped with can absorb solar light and change the electric energy, for the device provides electric power, can make the time of device flight more for a long time.

In the description of the present invention, it should be noted that the terms "vertical", "upper", "lower", "horizontal", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of describing the present invention and simplifying the description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention.

In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that changes may be made in the embodiments and/or equivalents thereof without departing from the spirit and scope of the utility model. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The high-endurance bird repelling unmanned aerial vehicle based on solar energy is characterized by comprising a machine body (1), a connecting plate (2) and a main shaft (3), wherein the connecting plate (2) is in an Contraband type structural mode, the connecting plate (2) is arranged below the machine body (1), the main shaft (3) is movably connected onto the connecting plate (2), wings (4) which are fixedly connected are arranged at four corners of the side edge of the machine body (1), and a disc (5) is arranged at the bottom end of the machine body (1);

the symmetry is equipped with diaphragm (11) on main shaft (3), the tip of diaphragm (11) is provided with shot-light (12), the bottom of connecting plate (2) is equipped with waist type groove (13), be equipped with rotor plate (14) on main shaft (3) be equipped with in rotor plate (14) auxiliary rod (15), auxiliary rod (15) are the right angled design.

2. The high-endurance bird-repelling unmanned aerial vehicle based on solar energy according to claim 1, wherein the machine body (1) and the disc (5) are connected in a screw locking manner, vertical plates (6) are symmetrically arranged at the top end of the machine body (1), a solar panel (7) is arranged at the top end of each vertical plate (6), and an inclined angle is formed between each solar panel (7) and the machine body (1).

3. The solar-based high-endurance bird-repelling unmanned aerial vehicle according to claim 1, wherein a limiting groove (8) is formed in the disc (5), the limiting groove (8) is formed in the central portion of the disc (5), and the limiting groove (8) is shaped in a countersunk manner in the disc (5).

4. The high-endurance bird-repelling unmanned aerial vehicle based on solar energy according to claim 1, wherein a movable column (9) is arranged at the top end of the main shaft (3), the movable column (9) and the main shaft (3) are fixedly connected, a plurality of uniformly distributed balls (10) are arranged on the circumferential side of the movable column (9), the balls (10) are movably embedded in the movable column (9), and the area of the balls (10) on the movable column (9) exceeds half.

5. The high-endurance bird-repelling unmanned aerial vehicle based on solar energy according to claim 1, wherein a second rotating plate (16) is arranged at the other end of the auxiliary rod (15), the auxiliary rod (15) is movably connected in the first rotating plate (14) and the second rotating plate (16), the diameter of the auxiliary rod (15) is smaller than the inner diameter of the first rotating plate (14) and the second rotating plate (16), a transverse shaft (17) is arranged on the second rotating plate (16), and the transverse shaft (17) is fixedly connected with the second rotating plate (16).

6. The solar-based high-endurance bird-repelling unmanned aerial vehicle according to claim 5, wherein a square block (18) is arranged on the transverse shaft (17), the square block (18) is fixed on the connecting plate (2), a fixedly-connected suspender (19) is arranged on the transverse shaft (17), the suspender (19) is arranged in the waist-shaped groove (13), and a balancing weight (20) is arranged at the bottom end of the suspender (19).