CN211919016U

CN211919016U - Miniature four-rotor aircraft capable of automatically hiding birds

Info

Publication number: CN211919016U
Application number: CN201922270016.5U
Authority: CN
Inventors: 杨志雄
Original assignee: Guangdong Yinrun Industrial Co ltd
Current assignee: Guangdong Yinrun Industrial Co ltd
Priority date: 2019-12-17
Filing date: 2019-12-17
Publication date: 2020-11-13
Anticipated expiration: 2029-12-17

Abstract

The utility model discloses a miniature four-rotor aircraft capable of automatically hiding birds, which comprises an aircraft body; the utility model drives the sector gear to rotate directionally on the two fixed seats through the motor driving gear, thereby the mounting plate can effectively drive the two bird hiding devices to swing back and forth on the aircraft body through the connecting piece, meanwhile, two universal balls are arranged on the aircraft body, and two electric push rods are respectively in rotary connection with the aircraft body and the bird hiding device through a lifting lug and a pin shaft, thereby leading the two bird hiding devices to swing back and forth on the aircraft body and simultaneously realizing the driving of the upper and lower positions, and through the LED lamp area that is equipped with in bird ware periphery of hiding can make the aircraft body realize when the sky flight to the warning effect of bird crowd can also implement the effect of driving and then the effectual condition of avoiding the damage of bird crowd of avoiding through the bird ware of hiding under the swing state to the bird crowd thereby effectually compensatied not enough among the prior art.

Description

Miniature four-rotor aircraft capable of automatically hiding birds

Technical Field

The utility model relates to an aircraft technical field specifically is a but four miniature rotor crafts of automatic bird of hiding.

Background

The quadcopter (Quadrotor) is a multi-rotor aircraft, four propellers of the quadcopter are all simple mechanisms with direct connection of motors, the cross-shaped layout allows the quadcopter to obtain the force of a rotating fuselage by changing the rotating speed of the motors so as to adjust the self posture, and the specific technical details are described in the basic motion principle, because of the inherent complexity, the quadcopter has never been large-sized commercial quadcopter historically, in recent years, micro-electro-mechanical systems benefit from the development of the control technology, the stable quadcopter gets extensive attention, the application prospect is very considerable, and the quadcopter in the prior art has certain defects in the practical application, such as:

the miniature four-rotor aircraft in the prior art is difficult to effectively realize the effect of avoiding and driving when encountering a bird group in the sky flight, so that a user is very easy to collide with the aircraft under the condition of careless control to cause damage, thereby failing to meet the requirements of the prior art.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a can hide miniature four rotor crafts of bird automatically to solve the problem that provides among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: a miniature four-rotor aircraft capable of automatically hiding birds comprises an aircraft body, wherein a motor is fixedly connected to one side in the aircraft body through a bolt, a gear is rotatably connected to the middle of the upper surface of the aircraft body through a pin shaft, a power output end of the motor is fixedly connected with the gear through a bolt, fixing seats are fixedly connected to the upper surface of the aircraft body on two sides of the gear through bolts, a sector gear is rotatably connected to the middle of the adjacent surface of the two fixing seats close to the top end through a pin shaft and is meshed with the gear, a mounting plate is fixedly connected to the top end of the sector gear through a bolt, a connecting piece is fixedly connected to the middle of the upper surface of the mounting plate through a bolt, bird hiding devices are rotatably connected to the middle of the two sides of the connecting piece close to the top end through a pin shaft, and universal balls are fixedly connected to, the top ends of the two universal balls are rotatably connected with electric push rods through lifting lugs and pin shafts, one ends of the electric push rods are rotatably connected with the lifting lugs and the bird hiding device through the pin shafts, and the motors and the electric push rods are both in electric signal connection with the aircraft body.

Preferably, the gear is rotatably connected with the aircraft body, and the top end of the periphery of the gear is positioned above the aircraft body.

Preferably, the connecting piece is the I shape structure, the fixing base is the right trapezoid structure, sector gear thickness size is not more than gear thickness size.

Preferably, the aircraft body specifically is four rotor crafts, and connecting piece upper surface height dimension is not less than four rotor height dimensions of aircraft body.

Preferably, the mounting panel is arc structure, the mounting panel is used for being as connecting piece and sector gear's connecting device, and is used for being as the stop device of hiding bird ware on the aircraft body.

Preferably, the upper surface of the bird hiding device is provided with a through hole, the through hole is in a honeycomb hole shape, and the peripheral edge of the bird hiding device is fixedly connected with the LED lamp belt through bolts.

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

the utility model drives the sector gear to rotate directionally on the two fixed seats through the motor driving gear, thereby the mounting plate can effectively drive the two bird hiding devices to swing back and forth on the aircraft body through the connecting piece, meanwhile, two universal balls are arranged on the aircraft body, and two electric push rods are respectively in rotary connection with the aircraft body and the bird hiding device through a lifting lug and a pin shaft, thereby leading the two bird hiding devices to swing back and forth on the aircraft body and simultaneously realizing the driving of the upper and lower positions, and through the LED lamp area that is equipped with in bird ware periphery of hiding can make the aircraft body realize when the sky flight to the warning effect of bird crowd can also implement the effect of driving and then the effectual condition of avoiding the damage of bird crowd of avoiding through the bird ware of hiding under the swing state to the bird crowd thereby effectually compensatied not enough among the prior art.

Drawings

Fig. 1 is a schematic top view of the present invention;

FIG. 2 is a schematic view of a partial half-section structure of the present invention;

FIG. 3 is an enlarged view of the structure at A in FIG. 2;

fig. 4 is a schematic view of the bird shelter according to the present invention.

In the figure: 1. an aircraft body; 11. a motor; 12. a gear; 13. a fixed seat; 14. a sector gear; 15. mounting a plate; 16. a connecting member; 17. a bird hiding device; 18. a universal ball; 19. an electric push rod.

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 a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-4, the present invention provides a technical solution: a miniature four-rotor aircraft capable of automatically hiding birds comprises an aircraft body 1, wherein the aircraft body 1 is specifically a four-rotor aircraft, a motor 11 is fixedly connected to one side inside the aircraft body 1 through a bolt, the model of the motor 11 is GA12 and N20 deceleration motors, the motor 11 is in electric signal connection with the aircraft body 1, a gear 12 is rotatably connected to the middle of the upper surface of the aircraft body 1 through a pin shaft, the gear 12 is rotatably connected with the aircraft body 1, the peripheral top end of the gear 12 is located above the aircraft body 1, the power output end of the motor 11 is fixedly connected with the gear 12 through a bolt, the gear 12 can be effectively driven to rotate in the aircraft body 1 through the motor 11, fixing seats 13 are fixedly connected to the upper surface of the aircraft body 1 on two sides of the gear 12 through bolts, and the fixing seats 13 are in a right trapezoid structure, the middle parts of the adjacent surfaces of the two fixing seats 13 are rotatably connected with a sector gear 14 through a pin shaft, the sector gear 14 is meshed with the gear 12, the thickness of the sector gear 14 is not more than that of the gear 12, the sector gear 14 can be effectively driven to rotate through the gear 12, the top end of the sector gear 14 is fixedly connected with a mounting plate 15 through a bolt, the mounting plate 15 is of an arc structure, the mounting plate 15 is used as a connecting device of a connecting piece 16 and the sector gear 14 and is used as a limiting device of a bird shelter 17 on the aircraft body 1, the middle part of the upper surface of the mounting plate 15 is fixedly connected with the connecting piece 16 through the bolt, the connecting piece 16 is of an I-shaped structure, the height of the upper surface of the connecting piece 16 is not lower than the height of four rotors of the aircraft body 1, and therefore the effect, and the aircraft body 1 at the edge of the four rotors is fixedly provided with a guardrail through bolts, the middle parts of the two sides of the connecting piece 16, which are close to the top ends, are respectively and rotatably connected with a bird hiding device 17 through pin shafts, the bird hiding device 17 is a long plate with a rectangular strip structure, the upper surfaces of the aircraft body 1 at the adjacent surfaces of the two fixing seats 13 are respectively and fixedly connected with universal balls 18 through bolts, the top ends of the two universal balls 18 are respectively and rotatably connected with an electric push rod 19 through a lifting lug and a pin shaft, one end of the electric push rod 19 is rotatably connected with the lifting lug and the bird hiding device 17 through a pin shaft, the electric push rod 19 is XC758, the deflection position of the bird hiding device 17 can be effectively driven and adjusted through the electric push rod 19, the motor 11 and the electric push rod 19 are both in electric signal connection with the aircraft body 1, the upper surface of the bird hiding device, and then effectual realization reduces the windage effect, the peripheral edge of bird ware of dodging 17 has LED lamp area through bolt fixedly connected with convenience of customers to obtain the position of driving the bird ware at night and conveniently watches and improve the aesthetic property, and the specific model in LED lamp area is the lamp area of hardcover, 5050, 60, LED lamp area and aircraft body 1 electricity signal connection.

The working principle is as follows: in use, the gear 12 is driven by the motor 11 to drive the sector gear 14 to rotate directionally on the two fixed seats 13, so that the mounting plate 15 can effectively drive the two bird hiding devices 17 to swing back and forth on the aircraft body 1 through the connecting piece 16, meanwhile, two universal balls 18 are arranged on the aircraft body 1, and two electric push rods 19 are respectively in rotary connection with the aircraft body 1 and the bird hiding device 17 through a lifting lug and a pin shaft, thereby driving the two bird-hiding devices 17 to swing back and forth on the aircraft body 1 and to move up and down, and through the LED lamp area that is equipped with in the periphery of bird ware 17 of dodging can make aircraft body 1 realize when the sky flight to the warning effect of birdswarm can also be through the effect that bird ware 17 of dodging under the swing state implements the bird crowd and drives and then the effectual realization avoids the condition of damage to the birdswarm.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. A miniature four-rotor aircraft that can automatically hide birds, comprising:

an aircraft body (1);

the aircraft comprises an aircraft body (1), a motor (11) is fixedly connected to one side inside the aircraft body (1) through a bolt, a gear (12) is rotatably connected to the middle of the upper surface of the aircraft body (1) through a pin shaft, the power output end of the motor (11) is fixedly connected with the gear (12) through a bolt, fixing seats (13) are fixedly connected to the upper surface of the aircraft body (1) on two sides of the gear (12) through bolts, a sector gear (14) is rotatably connected to the middle of the adjacent surface of the two fixing seats (13) close to the top end through a pin shaft, and the sector gear (14) is meshed with the gear (12);

wherein, fan-shaped gear (14) top is through bolt fixedly connected with mounting panel (15), bolt fixedly connected with connecting piece (16) is passed through at mounting panel (15) upper surface middle part, connecting piece (16) both sides middle part is close to top department and all is connected with bird ware (17) of dodging through the round pin axle rotation, two the adjacent face of fixing base (13) aircraft body (1) upper surface all is through bolt fixedly connected with universal ball (18), two universal ball (18) top is rotated through lug and round pin axle and is connected with electric putter (19), and electric putter (19) one end through round pin axle and lug with bird ware (17) of dodging rotate and are connected, motor (11) and electric putter (19) all with aircraft body (1) signal of electricity connection.

2. The miniature quad-rotor vehicle capable of automatically hiding birds as claimed in claim 1, wherein: the gear (12) is rotationally connected with the aircraft body (1), and the top end of the periphery of the gear (12) is located above the aircraft body (1).

3. The miniature quad-rotor vehicle capable of automatically hiding birds as claimed in claim 1, wherein: the connecting piece (16) is of an I-shaped structure, the fixing seat (13) is of a right-angle trapezoidal structure, and the thickness of the sector gear (14) is not larger than that of the gear (12).

4. The miniature quad-rotor vehicle capable of automatically hiding birds as claimed in claim 1, wherein: aircraft body (1) specifically is four rotor crafts, and connecting piece (16) upper surface height dimension is not less than aircraft body (1) four rotor height dimensions.

5. The miniature quad-rotor vehicle capable of automatically hiding birds as claimed in claim 1, wherein: mounting panel (15) are the arc structure, mounting panel (15) are used for as connecting piece (16) and sector gear (14)'s connecting device, and are used for as the stop device of bird dodging ware (17) on aircraft body (1).

6. The miniature quad-rotor vehicle capable of automatically hiding birds as claimed in claim 1, wherein: the bird-hiding device is characterized in that a through hole is formed in the upper surface of the bird-hiding device (17), the through hole is in a honeycomb hole shape, and the edge of the periphery of the bird-hiding device (17) is fixedly connected with an LED lamp belt through bolts.