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A multi-axis low altitude manned aircraft

An aircraft, low-altitude technology, applied in the field of aircraft, can solve the problems of poor safety performance of manned aircraft and the inability to fully open the parachute, and achieve the effect of alleviating urban traffic congestion, good flight performance and safety performance, and simple mechanical structure

Inactive Publication Date: 2019-01-22
FOSHAN SHENFENG AVIATION SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Since most of the existing manned aircraft fly at low altitudes, the parachute cannot be fully opened to play a role when a fault occurs, so the safety performance of the current manned aircraft is poor, so it is particularly important to improve the safety performance of the manned aircraft

Method used

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  • A multi-axis low altitude manned aircraft
  • A multi-axis low altitude manned aircraft
  • A multi-axis low altitude manned aircraft

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Embodiment Construction

[0025] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0026] The embodiment of the present invention discloses a multi-axis low-altitude manned aircraft, which has excellent comprehensive performance, good flight performance and safety performance; it can alleviate urban traffic congestion, reduce carbon emissions, and can quickly deliver passengers; In the event of a collision, the induction airbag will automatically inflate and expand to maximize the safety of the occupants in the cockpit. Due to the airbag stru...

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PUM

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Abstract

The invention discloses a multi-axis low-altitude manned aircraft including an airframe and a cockpit. An airbag is arranged on that airframe, the airframe has four arms. A motor is provided on each arm. A motor is bolted to the head end of the arm; a rotating shaft is arranged in the center of the motor. A rotor is mounted on each shaft; the rotor is fixed on the motor by bolts and rotated by thecorresponding motor, and the cockpit is arranged in the center of the body, the cockpit is provided with a manned seat and an operation screen, the operation screen controls the movement of the wholeaircraft, a landing bracket is arranged at the bottom of the cockpit, and a battery and a standby battery are arranged between the body and the cockpit. The invention has excellent comprehensive performance and good flight performance and safety performance at the same time and can alleviate urban traffic congestion, reduce carbon emissions, and can achieve rapid delivery of passengers; In the event of a collision, the inductive airbag inflates automatically to maximize the safety of cockpit personnel.

Description

technical field [0001] The invention relates to the technical field of aircraft, and more specifically relates to a multi-axis low-altitude manned aircraft. Background technique [0002] In real life, people mostly rely on transportation for travel, but most cities are currently heavily congested. For short-distance travel, especially when the road conditions are poor, conventional transportation is very inconvenient. At the same time, a large number of vehicle exhaust emissions cause serious air polltion. [0003] The low-altitude manned aircraft is a four-axis manned flight device controlled by wireless remote control equipment and its own program. to the specified location. In recent years, thanks to the development of micro-electromechanical control technology, stable quadcopters have received widespread attention, and their application prospects are very promising. [0004] Since most of the existing manned aircrafts fly at low altitudes, the parachute cannot be full...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C27/14B64D45/00B64C25/56B64D43/00B64D17/80
CPCB64C27/08B64C25/56B64C27/14B64D17/80B64D43/00B64D45/00
Inventor 王志成肖凤兰
Owner FOSHAN SHENFENG AVIATION SCI & TECH
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