Electric coaxial multi-rotor helicopter based on contra-rotating double-rotor motor

A dual-rotor motor and dual-rotor technology, used in rotorcraft, motor vehicles, and transmissions that drive multiple propellers, etc., can solve the problems of no change, mutual interference between rotors, poor endurance, etc. , easy control, the effect of large load capacity

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 electric helicopters generally simply replace the engine with an electric motor as a power source, and the control method has not changed, so there are still defects such as complex structure, high energy consumption, and poor endurance
At the same time, a multi-rotor can also be regarded as a multi-rotor helicopter, but the rotors of the multi-rotor will interfere with each other, resulting in more rotors and lower efficiency

Method used

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  • Electric coaxial multi-rotor helicopter based on contra-rotating double-rotor motor
  • Electric coaxial multi-rotor helicopter based on contra-rotating double-rotor motor
  • Electric coaxial multi-rotor helicopter based on contra-rotating double-rotor motor

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Embodiment

[0052] The following is based on Figure 1-2 Describe in detail an electric coaxial multi-rotor helicopter based on counter-rotating dual-rotor motors according to an embodiment of the present invention.

[0053] Such as Figure 1-2 As shown, the embodiment of the present invention discloses an electric coaxial multi-rotor helicopter based on a counter-rotating dual-rotor motor, which specifically includes:

[0054] fuselage 1;

[0055] The main rotor system 2, the main rotor system 2 is located at the upper center position of the fuselage 1 and is fixed with the fuselage 1 by a fastener 12, the main rotor system 2 includes a coaxial upper rotor 21 and a lower rotor 22, placed on the upper rotor 21 and the lower rotor 22 are used to make the upper rotor 21 and the lower rotor 22 realize the counter-rotating dual-rotor motors that rotate at the same speed in the opposite direction; the main rotor system 2 is used to provide the main flight power for the helicopter;

[0056] ...

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PUM

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Abstract

The invention discloses an electric coaxial multi-rotor helicopter based on a contra-rotating double-rotor motor, which comprises a helicopter body; a main rotor wing system which is located in the center of the upper portion of the fuselage and comprises an upper rotor wing and a lower rotor wing which are coaxial, and a contra-rotating double-rotor motor which is arranged between the upper rotorwing and the lower rotor wing and used for enabling the upper rotor wing and the lower rotor wing to achieve coaxial reverse constant-speed rotation; the main rotor system is used for providing mainflight power for the helicopter; an auxiliary rotor wing system which is located below the main rotor wing system, the auxiliary rotor wing system comprises four control rotor wings, and the four control rotor wings are evenly distributed at the four corners, away from the gravity center of the fuselage by a certain distance, of the fuselage; and the auxiliary rotor system provides attitude control for the helicopter. The electric coaxial multi-rotor helicopter has the advantages of simple structure, strong cruising ability, low power consumption, low manufacturing and using cost and the like.

Description

technical field [0001] The invention relates to the technical field of aircraft design and manufacture, in particular to an electric coaxial multi-rotor helicopter based on counter-rotating double-rotor motors. Background technique [0002] Existing electric helicopters generally directly replace the engine as a power source with an electric motor, and its control mode has not changed, so there are still defects such as complex structure, high energy consumption, and poor endurance. At the same time, a multi-rotor can also be regarded as a multi-rotor helicopter, but the rotors of the multi-rotor will interfere with each other, resulting in more rotors and lower efficiency. [0003] Therefore, how to overcome the above-mentioned technical defects of the existing electric multi-rotor helicopters 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 ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C27/10B64C27/12B64D35/02B64D35/06B64C19/00
CPCB64C19/00B64C27/08B64C27/10B64C27/12B64D35/02B64D35/06
Inventor 虞一扬
Owner 贯月航空技术(杭州)有限公司
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