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Dish-shaped five-axis multi-rotor aircraft

A rotorcraft and disc-shaped technology, which is applied in the field of disc-shaped five-axis multi-rotors, can solve the problems of human injury, safety concerns, and propellers occupying a large space, etc., to achieve accurate flight attitude control, improve safety, and individual appearance Effect

Pending Publication Date: 2021-02-09
贯月航空技术(杭州)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Existing multi-rotor aircraft generally use motors to drive propellers to generate power. The propellers occupy a large space, and the propellers are exposed outside the fuselage. If the high-speed rotating propellers touch the human body, it will cause great damage to the human body. safety concerns

Method used

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  • Dish-shaped five-axis multi-rotor aircraft
  • Dish-shaped five-axis multi-rotor aircraft
  • Dish-shaped five-axis multi-rotor aircraft

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Embodiment

[0054] The following is based on Figure 1-4 A dish-shaped five-axis multi-rotor aircraft according to an embodiment of the present invention is described in detail.

[0055] Such as Figure 1-4 As shown, the embodiment of the present invention discloses a disc-shaped five-axis multi-rotor aircraft, which specifically includes: a fuselage 1, a casing 2, a main rotor system, an auxiliary rotor system and a control system, specifically,

[0056] The casing 2 is fixed on the outside of the fuselage 1 and includes an upper cover 21 with a narrow shape and an open top and a lower cover 22 with a wide shape and an open bottom.

[0057] The main rotor system is installed in the upper center position of the fuselage 1 and wrapped by the upper cover 21 of the casing. The main rotor system includes an electric counter-rotating ducted fan 3 that can make the upper and lower fans rotate oppositely at the same speed; The counter-rotating ducted fan 3 is used to provide the main flight po...

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Abstract

The invention discloses a dish-shaped five-axis multi-rotor aircraft which comprises an aircraft body; a machine shell which is fixed to the exterior of the machine body in a covering mode; a main rotor system which comprises an electric contra-rotating ducted fan capable of enabling an upper-stage fan and a lower-stage fan to rotate oppositely at a constant speed; wherein the electric contra-rotating ducted fan is used for providing main flight power for the multi-rotor aircraft; an auxiliary rotor wing system which comprises four control rotor wings, and the four control rotor wings providing attitude control for the multi-rotor-wing aircraft; and a control system which is used for controlling the main rotor wing system and the auxiliary rotor wing system. Compared with an existing multi-rotor-wing aircraft, all rotor wings of the dish-shaped five-axis multi-rotor-wing aircraft are wrapped in the aircraft shell and do not make contact with the human body to injure the human body; meanwhile, the dish is cool in appearance and can be applied to multiple fields of consumption, entertainment and the like.

Description

technical field [0001] The invention relates to the technical field of design and manufacture of a multi-rotor aircraft, in particular to a dish-shaped five-axis multi-rotor aircraft. Background technique [0002] Existing multi-rotor aircraft generally use motors to drive propellers to generate power. The propellers will occupy a large space, and the propellers are exposed outside the fuselage. If the high-speed rotating propellers touch the human body, it will cause great damage to the human body. Safety concerns. [0003] Therefore, how to overcome the above-mentioned technical defects of the existing electric multi-rotor aircraft is a direction that those skilled in the art need to study. Contents of the invention [0004] The present invention aims to solve one of the above-mentioned technical problems in the prior art at least to a certain extent. [0005] For this reason, the object of the present invention is to propose a kind of disc-shaped five-axis multi-rotor...

Claims

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Application Information

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IPC IPC(8): B64C11/48B64C27/08B64C27/32B64D27/24B64C19/00B64D31/00
CPCB64C11/48B64C19/00B64C27/08B64C27/32B64D27/24B64D31/00Y02T50/60
Inventor 虞一扬
Owner 贯月航空技术(杭州)有限公司
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