Unlock instant, AI-driven research and patent intelligence for your innovation.

Folding manned aircraft with adjustable rotor postures

An aircraft and rotor technology, applied in the field of manned aircraft, can solve the problems of large pulling force, complicated operation and high cost, and achieve the effect of reducing rigid force, good balance ability and better comfort

Pending Publication Date: 2020-11-13
HENAN UNIV OF SCI & TECH
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For the single-person aircraft with the shape of a helicopter, the mosquito helicopter made in Canada is the smallest at present. This helicopter aircraft mainly relies on the rotation of the huge rotor on its top to drive the airflow to move downward, so that the pulling force generated by it is greater than gravity, and the rotor body is relatively small. It is very inconvenient for daily travel, and you need to find an open space when taking off. Although you don’t need a special pilot’s license, the operation is relatively complicated for most people. In addition, it is expensive and not suitable for public use.
For single-person turbojet aircraft and flying backpacks, they all need to be controlled by remote control or joystick. Although they are powerful, they are expensive for ordinary people and difficult to control and balance.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Folding manned aircraft with adjustable rotor postures
  • Folding manned aircraft with adjustable rotor postures
  • Folding manned aircraft with adjustable rotor postures

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0043] Hereinafter, the present invention will be described in further detail with reference to the accompanying drawings and embodiments, and the present invention includes but is not limited to the following embodiments.

[0044] Such as figure 1 As shown, a folding manned aircraft with adjustable rotor attitude, the aircraft includes a chassis 1, a frame assembly 3, a rotor assembly 4 and a shock absorbing device 7.

[0045] Figure 1 to Figure 3 As shown, the chassis 1 serves as a support for the main body of the aircraft, and the chassis 1 is provided with a manned component 2 and a battery 5 for powering the aircraft. The people-carrying part 2 is preferably an inflatable sofa, and may also be a cabin. The battery 5 includes a common battery and a backup battery, and the total number of the batteries 5 is an even number and symmetrically arranged around the center of flight. The battery 5 is installed inside the battery box 51, and one side of the battery box 51 is pr...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention discloses a folding manned aircraft with adjustable rotor postures, which comprises a chassis, a rack assembly, rotor assemblies and a damping device, wherein the chassis is used as a support of an aircraft main body, and a manned part and a battery for providing power for the aircraft are arranged on the chassis; the rack assembly comprises a rack body and eight machine arms, the machine arms are evenly arranged around the rack body every 45 degrees, the whole is of a structure shaped like a Chinese character'mi', and the extending lengths of the machine arms can be adjusted. The eight rotor assemblies are all installed at the tail ends of the machinearms, and each rotor assembly is controlled by an independent power mechanism to achieve rotation of the rotors in different directions. The damping device is used for buffering and damping when the aircraft lands. The flight mode that the aircraft controls the direction through the rotating speed difference between the rotors is changed, advancing and steering of the aircraft are achieved by adjusting the postures of the rotors, the flight process is more stable, and the safety coefficient is higher; and the lengths ofthe arms can be adjusted as required, so that people can go out more conveniently.

Description

technical field [0001] The invention belongs to the field of manned aircraft, and in particular relates to a folding manned aircraft with adjustable rotor attitude. Background technique [0002] At present, the aircraft industry at home and abroad is booming, ranging from large passenger aircraft, large transport aircraft, and large manned helicopters to various quadrotor drones and single-person aircraft. [0003] Although airplanes have provided human beings with the convenience of air transportation for many years, for short-distance travel, it is still a long-standing dream of people to be able to "fly around" in low-altitude cities in a single-person aircraft. Single-person aircraft are basically used by flying enthusiasts, and have not yet been popularized as a means of transportation. [0004] Today's single-person aircraft mainly contains three types: one is an ultralight aircraft with a helicopter shape, the other is a single-person turbojet aircraft powered by a t...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C27/52B64C1/06B64C1/30B64C25/60B64C25/62B64C25/04B64D17/80B64D11/06B64D25/10
CPCB64C1/06B64C1/30B64C25/04B64C25/60B64C25/62B64C27/08B64C27/52B64D17/80B64D25/10B64D11/0619
Inventor 张森冯振宗周峰吕进锋黄怡航王展庄智强李晓强邵敬平徐兴元
Owner HENAN UNIV OF SCI & TECH