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Miniature shaftless ducted rotor aircraft and flight control method thereof

A technology for a rotorcraft and an aircraft, applied in the field of rotorcraft, can solve the problems of complex control mechanism, larger size of the aircraft, low control efficiency of the control mechanism, etc., and achieves the effects of high control efficiency, reduced thermal radiation, and improved energy utilization rate

Pending Publication Date: 2020-04-03
南京华航翼飞行器技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, at present, micro-rotor aircraft generally have the disadvantages of complex control mechanisms, which lead to larger aircraft volume and low operating efficiency of the control mechanisms.

Method used

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  • Miniature shaftless ducted rotor aircraft and flight control method thereof
  • Miniature shaftless ducted rotor aircraft and flight control method thereof
  • Miniature shaftless ducted rotor aircraft and flight control method thereof

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Embodiment Construction

[0037] The present invention will be further described below in conjunction with accompanying drawing.

[0038] The overall structure of the present invention is as figure 1 shown, from figure 1 It can be seen from the figure that the rotor is composed of four blades 6, the blades 6 are connected with the rotating ring 7, and there is no air gap between the rotor and the duct 1.

[0039] figure 2 It is a cross-sectional view of a shaftless ducted rotor lift device, and its main feature is that the stator 3, the rotor 5 and the blade 6 are installed between the upper fixed bearing 2 and the lower fixed bearing 8, and the upper fixed bearing 2 and the lower fixed bearing 8 play a role in fixing and The position-limiting function can transmit the thrust generated by the rotation of the paddle 6 at the same time. An air gap 6 is formed between the stator 3 and the rotor 5, and the blade 6 is connected with the rotating ring 7 to be connected with the stator 3 as a whole, and t...

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Abstract

The invention provides a miniature shaftless ducted rotor aircraft and a flight control method thereof. The miniature shaftless ducted rotor aircraft comprises a duct as well as a plurality of paddlewing structures and self-adaptive control surface structures which are mounted in the duct; each paddle wing structure comprises an upper fixed bearing and a lower fixed bearing which are fixed on theinner wall of the duct, a motor, a stator, a rotor, paddles and a rotating ring are arranged between the upper fixed bearing and the lower fixed bearing, an air gap is formed between the stator and the rotor, and the paddles are connected with the rotating ring so as to be connected with the stator into a whole; and the self-adaptive control surface structure is distributed below the paddle wingstructure. Compared with a traditional ducted rotor wing, the miniature shaftless ducted rotor aircraft generates larger lift force; the motor-duct-rotor integrated design enables no gap to exist between the blades and the motor, the influence of small deformation of the duct body on the overall aerodynamic efficiency and safety is reduced, and meanwhile, the control mechanism is simple, light inweight, easy to control and more suitable for micro aircrafts.

Description

technical field [0001] The invention relates to the field of rotorcraft, in particular to a miniature shaftless ducted rotorcraft and a flight control method thereof. Background technique [0002] Micro air vehicle has attracted much attention because of its special purpose. An important application is military reconnaissance, which can be equipped to soldier squads for enemy reconnaissance and surveillance. It can also be used for war risk estimation, target search, communication relay, monitoring of chemical, nuclear or biological weapons, and reconnaissance of the interior of buildings. It can be applied to various war environments such as cities and jungles. Because of its portability, simple operation, and good safety, it can be equipped in large quantities in the army. In the non-military field, MAVs equipped with corresponding sensors can be used to search for disaster survivors, sources of toxic gases or chemicals, and eliminate crop pests. [0003] There are thr...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C11/20B64C9/00B64C27/14G05D1/08
CPCG05D1/0808B64C11/20B64C9/00B64C27/14
Inventor 申遂愿朱清华李宜恒
Owner 南京华航翼飞行器技术有限公司
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