Three-axis aircraft

A technology of quadrocopter and remote control, applied in the field of aircraft, can solve the problems of poor flight stability, inability to maintain balance, unreasonable structure of aircraft, etc., achieve good stability and reliability, and ensure the effect of stability and reliability

Active Publication Date: 2016-07-06
BEIJING INSTITUTE OF GRAPHIC COMMUNICATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, although there are some aircraft toys with three-axis design, on the one hand, these aircraft have poor flight stability and can only be used as toys
On the other hand, the unreasonable structure of the aircraft makes it impossib

Method used

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Embodiment Construction

[0023] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be described in further detail below in conjunction with specific embodiments and with reference to the accompanying drawings.

[0024] It should be noted that all expressions using "first" and "second" in the embodiments of the present invention are to distinguish two entities with the same name but different parameters or parameters that are not the same, see "first" and "second" It is only for the convenience of expression, and should not be construed as a limitation on the embodiments of the present invention, which will not be described one by one in the subsequent embodiments.

[0025] refer to figure 1 Shown is a schematic structural view of an embodiment of the triaxial aircraft provided by the present invention. The three-axis aircraft belongs to the remote control flying device. This type of flying device is provided with multiple sets o...

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Abstract

The invention discloses a three-axis aircraft.The three-axis aircraft comprises an aircraft body, main wings, auxiliary wings, power rotor wings, balance rotor wings, a drive motor and a remote control unit.Control equipment is arranged in the aircraft body, the three sets of main wings and the three sets of auxiliary wings are evenly distributed around the aircraft body, and the main wings vertically correspond to the corresponding auxiliary wings.The main wings are located under the auxiliary wings, and the ends, close to the aircraft body, of the main wings and the auxiliary wings are fixedly connected.The other ends of the main wings and the other ends of the auxiliary wings are provided with the power rotor wings and the balance rotor wings respectively.The lower portions of the power rotor wings and the lower portions of the balance rotor wings are connected with the drive motor, and the drive motor is connected with the control equipment inside the aircraft body through a wire.The remote control unit is wirelessly connected with the control equipment inside the aircraft body.According to the three-axis aircraft, through the three sets of main wings and the three sets of auxiliary wings, all of which are arranged in a staggered mode, the power rotor wings on the main wings provide main flight power, the balance rotor wings on the auxiliary wings can adjust the posture of the aircraft more precisely, and therefore the aircraft can fly stably and reliably.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a three-axis aircraft. Background technique [0002] At present, multi-rotor aircraft are mainly divided into two categories, even-numbered axes and odd-numbered axes. The even-numbered axis multi-rotor aircraft is characterized by several axes distributed around the fuselage, each axis is directly driven by a motor with a fixed pitch propeller, half of the motors rotate clockwise, and the other half rotates counterclockwise, and the pitch of the aircraft is controlled by coordinating the speed of each motor Balance and anti-torque balance, but the coordination for speed is more difficult to achieve. The structure of the odd-axis multi-rotor aircraft is the same as that of the even-axis multi-rotor. The difference is that the rotating surface of the redundant one-axis propeller can rotate around this axis. Part of the pulling force generated by the rotor is used as lift, and th...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C27/12B64C27/32B64C27/82B64C19/00
CPCB64C19/00B64C27/08B64C27/12B64C27/32B64C27/82
Inventor 巫建王兆华杜艳平高振清
Owner BEIJING INSTITUTE OF GRAPHIC COMMUNICATION
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