Fast take-off aircraft

An aircraft, fast technology, applied in the field of aircraft, can solve the problems of long runway, low efficiency, long time, etc., to achieve the effect of improving acceleration efficiency, increasing pressure difference, and shortening take-off distance

Inactive Publication Date: 2018-08-10
FOSHAN SHENHANG SCI & TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Traditional aircraft take a long time to land and need a long runway, which is inefficient

Method used

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  • Fast take-off aircraft
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Embodiment Construction

[0010] Now in conjunction with accompanying drawing, the present invention is described in detail: a kind of aircraft that takes off rapidly, comprises fuselage 1, power plant 2, wing 3, lift device 4 and empennage 5; Be equipped with control device and energy equipment in fuselage 1; Empennage 5 is positioned at the afterbody of fuselage, strengthens the flight stability of described aircraft; Power unit 2 is positioned at fuselage 1, provides the thrust or pulling force that advances for described aircraft; Wing 3 is positioned at the left and right sides of fuselage 1; The left wing and the right wing of the wing 3 are respectively provided with a circular groove 6, and the two circular grooves 6 are symmetrically arranged; there are two lift devices 4, which are arranged in the two circular grooves 6 left and right; 8, bracket 9, motor 10 and propeller 11; the fixed ring 7 is annular, and the fixed ring 7 is fixed on the inner wall of the circular groove 6; the controller 8...

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Abstract

A fast take-off aircraft belongs to the technical field of aircrafts, and comprises the fuselage, a power device, an aerofoil, lift devices and emages. An operating device and energy equipment are arranged in the fuselage. The emages are located at the tail of the fuselage. The power device is located on the fuselage. The aerofoil is located on the left and right sides of the fuselage. The left wing and the right wing of the aerofoil are each provided with a circular groove, and the two circular grooves are symmetrically arranged. Two lift devices are arranged in the two circular grooves leftand right. Each lift device comprises a fixed ring, a controller, brackets, motors and propellers, the controllers are located on the fixed ring and connected with the operating device, a driver controls the controllers through the operating device and can control the on / off and rotating speeds of the motors, at least four brackets are arranged and evenly distributed on the inner ring of the fixedring, the motors are mounted on the fixed brackets, and each motor is provided with one propeller. The fast take-off aircraft can increase the pressure difference between the upper and lower surfacesof the aerofoil, shorten the take-off distance of the aircraft, and improve the acceleration efficiency.

Description

technical field [0001] A fast-flying aircraft belongs to the technical field of aircraft, and in particular relates to an aircraft. Background technique [0002] It takes a long time and a long runway for traditional aircraft to land, and the efficiency is low. Contents of the invention [0003] The purpose of the present invention is to overcome the deficiency of above-mentioned traditional aircraft, invent a kind of aircraft that takes off rapidly. [0004] A fast-flying aircraft, comprising a fuselage, a power unit, a wing, a lifting device and an empennage; the fuselage is equipped with control devices and energy devices; the empennage is located at the tail of the fuselage to enhance the flight stability of the aircraft; power The device is located on the fuselage to provide forward thrust or pulling force for the aircraft; the wings are located on the left and right sides of the fuselage; a circular groove is respectively arranged on the left wing and the right wing...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/22B64C27/08B64C27/14B64C3/32
CPCB64C27/22B64C3/32B64C27/08B64C27/14
Inventor 王美航
Owner FOSHAN SHENHANG SCI & TECH CO LTD
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