Aircraft wing

A wing and aircraft technology, applied in the field of aircraft wings, to achieve a wide range of effects

Inactive Publication Date: 2020-04-21
王世宝
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Since the invention of fixed-wing aircraft, its wings have been fixed on both sides of the aircraft fuselage. This design allow

Method used

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Embodiment Construction

[0010] specific implementation plan

[0011] The wing of the fixed-wing aircraft that can take off and land vertically according to the present invention is mainly composed of a wing shell, a main power motor, a propeller, a main shaft, a main shaft gear, an electric motor, and an electric motor gear. The wings can be divided into two shapes according to needs, one is The left and right wings of the fuselage are combined into one integral wing and cross the fuselage. The other is that the left and right wings of the fuselage are independent, and each independent wing is divided into two parts as required (two parts The size depends on the need), that is, the fixed wing part of the wing (the part of the wing fixed on the fuselage) and the movable wing part of the wing. Now the left and right wings are independently installed on both sides of the fuselage and each independent wing is divided into two parts, namely the fixed wing part (the part of the wing fixed on the fuselage) ...

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Abstract

The invention provides a fixed-wing aircraft wing, which mainly comprises a wing shell, a main power motor, a propeller, a main shaft, a main shaft gear, an electric motor and an electric motor gear,and is invented to solve the problem of singleness of a take-off mode of the fixed-wing aircrafts. The fixed-wing aircraft wing can be two shapes, wherein one left and right wing is in an integral wing shape, the other left and right wing independently exists, each independent wing is divided into two parts as required, namely a fixed wing part (a part fixed on a fuselage) and a movable wing part,and the main power motor and the electric motor are mounted on the movable wing part. When an aircraft does not take off, the wing of the fixed wing part and the wing of the movable wing part are located at the same horizontal position. The electric motor is started, the electric motor gear rotates around the main shaft gear, when the electric motor gear rotates to the position below the main shaft gear, namely the perpendicular position, the electric motor stops rotating, at the moment, the movable wing part is perpendicular to the fixed wing part, the main power motor is started, and vertical take-off and landing of the airplane are achieved.

Description

[0001] Technical field [0002] The invention relates to an aircraft wing, which is a fixed-wing aircraft wing capable of vertical take-off and landing. Background technique [0003] Since the invention of fixed-wing aircraft, its wings have been fixed on both sides of the aircraft fuselage. This design allows fixed-wing aircraft to take off only by taxiing, so that fixed-wing aircraft are used because of the fixed wings. limitations. Contents of the invention [0004] In order to enable the fixed-wing aircraft to play more roles, the present invention provides a variable fixed-wing aircraft wing, which mainly includes a wing shell, a main power motor, a propeller, a main shaft, a main shaft gear, an electric motor, and an electric motor gear. The wing of the fixed-wing aircraft is cut off at a position close to the fuselage (the specific position depends on the need), that is, the wing is divided into two parts-the fixed wing part wing (the part of the wing fixed on the fu...

Claims

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Application Information

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IPC IPC(8): B64C27/28
CPCB64C27/28
Inventor 王世宝
Owner 王世宝
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