a single-axis aircraft

A kind of aircraft and single-axis technology, which is applied in the direction of aircraft, unmanned aircraft, remote control aircraft, etc., can solve the problems of difficult control of propeller angle, monotonous appearance and complex structure, etc., and achieve simple and convenient operation mode, beautiful appearance and easy operation Achieved effect

Active Publication Date: 2017-07-21
GEER TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In view of the above problems, the present invention provides a single-axis aircraft to solve the problems of the existing single-axis multi-blade aircraft with complex structure, difficulty in controlling the propeller angle, and monotonous appearance and shape

Method used

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Embodiment Construction

[0042] In order to make the object, technical solution and advantages of the present invention clearer, the implementation manner of the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0043] Overall design idea of ​​the present invention is: reference figure 1 , using the principle that the wings change the wind resistance, the wing drive device is introduced into the main body of the single-axis aircraft, such as figure 1 As shown in the left figure in the figure, under normal circumstances, the wind resistance area of ​​the part where the wings protrude from the main body of the monocopter is the same in all directions. At this time, although the wings will cause wind resistance, the downward propulsion force of the monocopter is uniform due to the small and equal wind resistance area. ;Such as figure 1 As shown in the right figure in the figure, when the wings move in a certain direction, they are received in th...

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Abstract

The invention discloses a uniaxial aircraft. The uniaxial aircraft comprises: a propeller (1), an aircraft main body (2) and a wing driving device (3) constituting a part of the aircraft main body (2). The aircraft main body (2) is streamlined, The central position of the wing driving device (3) is provided with an annular wing (4) extending out of the wing driving device, and the annular wing (4) can move horizontally under the drive of the wing driving device (3); When the wind resistance area in all directions of the outer circumference of the wing drive device (3) is the same, the uniaxial aircraft maintains the current flight posture; when the annular wing (4) moves in a certain direction, the wind resistance of the drive device (3) extending out of the wing in this direction is increased. area, and when the relative direction is received in the wing drive device (3) to reduce the windage area of ​​the relative direction, the single-axis aircraft changes the current flying attitude. The uniaxial aircraft of the invention has the characteristics of simple structure, convenient manipulation and beautiful appearance.

Description

technical field [0001] The invention relates to the technical field of aircraft design, in particular to a single-axis aircraft. Background technique [0002] The existing consumer-type aircraft that can take off and land in a straight line can be mainly divided into two types: multi-axis multi-blade aircraft and single-axis multi-blade aircraft. The single-axis multi-blade aircraft realizes the control of the aircraft's flight posture through the following two methods : [0003] 1. Set multiple sets of propellers, change the angle of the propellers, so that the angles of each set of propellers are different, and control the flight posture of the aircraft by changing the downward wind direction generated by each set of propellers; the single-axis multi-blade aircraft with this structure has a complex structure , and it is not easy to control the propeller angle, which is relatively rare in consumer products. [0004] 2. The tail structure is set, and the flight posture is ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C9/00
CPCB64C9/00B64U10/10B64U20/70B64U40/00B64U30/24B64C9/02B64C13/50B64C39/062B64C27/467B64C27/82B64C27/10B64C39/024B64U30/20B64C2027/8272B64D27/24
Inventor 蔡忠育
Owner GEER TECH CO LTD
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