Multi-rotor manned helicopter

Abstract

The invention discloses a multi-rotor manned helicopter which comprises a manned cabin, lifting rotors, an equipment cabin and a steering rudder. The upper portion of the manned cabin is provided witha window, the bottom edge of the manned cabin is provided with sliding wheels, the rear wall of the manned cabin is provided with a cabin door, the outer walls of the two sides of the manned cabin are each provided with a side pushing rotor wing, and the rear ends of the side pushing rotor wings are provided with first power equipment for driving the side pushing rotor wings to operate. There areat least two lifting rotors, the lifting rotors are distributed on the two sides of the manned cabin side by side, and the lower end of each lifting rotor is provided with second power equipment fordriving the corresponding lifting rotor to operate. The equipment cabin is arranged at the bottom of the manned cabin, and a power source for the first power equipment and the second power equipment to operate is arranged in the equipment cabin; and the steering rudder is arranged at the top of the manned cabin. The flight and take-off and landing device is similar to an unmanned aerial vehicle, and has the advantages of small size, flexibility, low altitude, low speed, vertical take-off and landing, economy and practicability.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a multi-rotor manned helicopter. Background technique [0002] Throughout the world, there are almost no manned helicopters that are suitable for ordinary people to own and drive. The personal manned helicopters currently developed at home and abroad generally have the following problems: 1. The operation is difficult and requires professionals to operate; 2. It flies high and fast, so it is not suitable as a means of transportation for ordinary people in cities and villages; 3. It has a large wingspan and takes up a lot of space, and has high requirements for take-off and landing sites; 4. The design is complicated and expensive. Therefore, small and flexible, low-altitude and low-speed, vertical lift, economical and practical smart helicopters will be the development direction of the future era of personal manned aircraft. Contents of the invention [0003] Aiming at the de...

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Problems solved by technology

[0002] Throughout the world, there are almost no manned helicopters that are suitable for ordinary people to own and drive. The personal manned helicopters currently developed at home and abroad generally have the following problems: 1. The operation is difficult and requires professionals to operate; 2. Flying high and fast, it is not suitable as a means of transportation for ordinary people in urban and rural areas; 3. The large wingspan occupies a large space and requires high take-off and landing sites; 4. The design is complex and expensive

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