阅读说明：本技术 一种双翼飞行器 (Double-wing aircraft ) 是由 汪皖豫 于 2020-12-28 设计创作，主要内容包括：本发明提供一种双翼飞行器,包括固定连接的左右两个旋翼,两个旋翼之间具有连接架。连接架设有两个转盘电机,每个转盘电机上均铰接有一伸缩电机,伸缩电机上安装有伸缩杆,所述的旋翼包括框架,底部支撑架的中心设有电机座,电机座上安装有电机,电机连接螺旋桨,通过电机带动螺旋桨转动,电机座与电机为球铰接,电机能够绕电机座转动,电机还设有主控杆,所述的主控杆,与对应的伸缩电机上的伸缩杆铰连接。(The invention provides a double-wing aircraft which comprises a left rotor wing and a right rotor wing which are fixedly connected, wherein a connecting frame is arranged between the two rotor wings. The link is equipped with two carousel motors, and all articulated on every carousel motor have a flexible motor, installs the telescopic link on the flexible motor, the rotor include the frame, the center of bottom sprag frame is equipped with the motor cabinet, installs the motor on the motor cabinet, the screw is connected to the motor, drives the screw through the motor and rotates, the motor cabinet is ball-hinged with the motor, the motor can rotate around the motor cabinet, the motor still is equipped with the master control pole, with the telescopic link on the flexible motor that corresponds hinge and connect.)

1. The double-wing aircraft is characterized by comprising a left rotor wing and a right rotor wing which are fixedly connected, and a connecting frame is arranged between the two rotor wings.

2. The twin wing aircraft of claim 1, wherein: the connecting frame is provided with two turntable motors, each turntable motor is hinged with a telescopic motor, the telescopic motor is provided with a telescopic rod,

the rotor wing comprises a frame, a motor base is arranged at the center of the bottom support frame, a motor is arranged on the motor base, the motor is connected with a propeller and drives the propeller to rotate through the motor, the motor base is in spherical hinge connection with the motor, the motor can rotate around the motor base,

the motor is also provided with a main control rod which is hinged with the corresponding telescopic rod on the telescopic motor.

Technical Field

The invention relates to a double-wing aircraft.

Background

The existing unmanned aerial vehicle aircraft is mostly provided with four rotors, is large in size and cannot meet special flight in narrow space.

Disclosure of Invention

Technical problem to be solved

In view of the problems in the prior art, the present invention is directed to a two-wing aircraft, which has a smaller size than a four-rotor aircraft and can freely shuttle in a narrow space.

A double-wing aircraft comprises a left rotor wing and a right rotor wing which are fixedly connected, and a connecting frame is arranged between the two rotor wings.

The connecting frame is provided with two turntable motors, each turntable motor is hinged with a telescopic motor, the telescopic motor is provided with a telescopic rod,

the rotor wing comprises a frame, a motor base is arranged at the center of the bottom support frame, a motor is arranged on the motor base, the motor is connected with a propeller and drives the propeller to rotate through the motor, the motor base is in spherical hinge connection with the motor, the motor can rotate around the motor base,

the motor is also provided with a main control rod which is hinged with the corresponding telescopic rod on the telescopic motor.

The invention aims to provide a double-wing aircraft, wherein a motor and a propeller are connected with a rack in a ball hinge mode, the direction of a main shaft of the propeller is controlled through a turntable motor and a telescopic motor, power transfer is realized, and the double-wing aircraft is smaller than a four-rotor aircraft in size and can freely shuttle in a narrow space.

Drawings

FIG. 1 is a schematic structural view of the present invention

FIG. 2 is a schematic view of the present invention in a top view (in this state, vertically ascending and descending)

FIG. 3 is a schematic left-side view of the present invention

FIG. 4 is a schematic view of the full section A-A of FIG. 2

FIG. 5 is a schematic view of the side of the working shaft of the present invention (two turntable motors rotating in opposite directions to reverse the direction of the propeller and achieve self-rotation of the aircraft)

FIG. 6 is a schematic top view of the present invention

FIG. 7 is a schematic view of the two-axis side of the inventive operation

FIG. 8 is a schematic top view of the present invention in operation;

the reference numbers in the figures illustrate:

1. connecting frame

2. Left side frame

3. Right side frame

4. Left side support frame

5. Right supporting frame (the other end of the main control rod is connected with the supporting frame through a ball joint, and when the main control rod is swung, the other end is fixed at a point to rotate)

6. Left side telescopic motor

7. Right side telescopic motor

8. Left side propeller

9. Right side propeller

10. Left side telescopic rod

11. Right telescopic rod (Telescopic motor, i.e. linear motor, the telescopic rod is the output shaft of the telescopic motor)

12. Left turntable motor (turntable motor output shaft and telescopic motor rotating link)

13. Right turntable motor

14. Left side support frame

15. Right side support frame

16. Left main control rod

17. Right main control rod (end and telescopic rod ball joint connection)

18. An electric motor.

Detailed Description

The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention; it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and all other embodiments obtained by those skilled in the art without any inventive work are within the scope of the present invention.

Comprises a left rotor wing and a right rotor wing which are fixedly connected, a connecting frame 1 is arranged between the two rotor wings,

the connecting frame is provided with two turntable motors, namely a left turntable motor 12 and a right turntable motor 13,

each turntable motor is hinged with a telescopic motor, a left side turntable motor 12 is provided with a left side telescopic rod 10, the same as the right side,

as shown in the drawing, taking the left side as an example,

the rotor wing comprises a left side frame 2, a motor base is arranged at the center of the bottom support frame, a motor 18 is arranged on the motor base, the motor is connected with a left side propeller 9 and drives the propeller to rotate through the motor, the motor base is in spherical hinge connection with the motor, the motor can rotate around the motor base,

the motor is also provided with a left main control rod 16, the left main control rod 16 is hinged with the left telescopic rod 10,

the rotation and angle adjustment of the propeller are realized in a ball-hinged mode, and the flight of double wings is realized.