Multi-rotor manned helicopter

A helicopter and multi-rotor technology, applied in the field of aircraft, can solve the problems of high price, complex design, and high requirements for take-off and landing sites

Pending Publication Date: 2020-10-30
叶殊钨
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

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 requi...

Method used

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  • Multi-rotor manned helicopter
  • Multi-rotor manned helicopter
  • Multi-rotor manned helicopter

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0034] Such as figure 1 , figure 2 and image 3 As shown, a multi-rotor manned helicopter includes a manned cabin 1, a lifting rotor 5, an equipment compartment 8 and a steering rudder 10;

[0035] The upper part of the manned cabin 1 has a viewing window 7, the bottom edge is provided with a sliding wheel 9, the rear wall is provided with a hatch 4, and the outer walls of both sides are respectively provided with two side-thrusting rotors 2, and the two side-thrusting rotors on the same side 2 are located on the same axis, and the rear end of the side-thrusting rotor 2 is provided with a first power device 3 that drives the side-thrusting rotor 2 to run; wherein, the manned cabin 1 is a capsule-shaped structure with a boat-shaped cross section To accommodate multiple people;

[0036] There are twelve lift rotors 5 arranged side by side on both sides of the manned cabin 1, and the lower end of each lift rotor 5 is respectively provided with a second power to drive the lift...

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PUM

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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...

Claims

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Application Information

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IPC IPC(8): B64C1/22B64C1/14B64C27/08B64C9/00B64C7/00B64D17/00
CPCB64C1/22B64C1/1484B64C27/08B64C9/00B64C7/00B64D17/00
Inventor 叶殊钨
Owner 叶殊钨
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