Vertical take-off and landing seaplane

Abstract

The invention relates to a vertical take-off and landing seaplane, belonging to the technical field of aircraft, comprising a fuselage, a wing, a reversing lifting device, a vertical lifting device, atail rotor and a buoy. A main control is arranged in that fuselage, and the main control is connected with a reversing lifting device, a vertical lifting device and a tail rotor. The wing adopts forward swept wing. The reversing lifting device is located at the leading edge of the wing and can be steered 90 degrees under the control of the master controller to provide vertical lift or forward pull for the aircraft. The vertical lifting device is arranged at the rear end of the fuselage, and the vertical lifting device provides the upward lifting force for the aircraft in the form of rotatingthe paddle blades driven by an electric motor. The tail rotor is located below the vertical lift. The invention can carry out vertical take-off and landing, has long sailing time, stable flight process, has two lifting modes, has high safety coefficient, and is suitable for logistics transportation, air fire extinguishing, post-disaster rescue and the like.

Description

technical field [0001] A water vertical lift aircraft belongs to the technical field of aircraft, and in particular relates to an aircraft. Background technique [0002] Although the fixed-wing aircraft has a fast flight speed and a long flight time, it cannot hover at a fixed point; although a multi-rotor aircraft can hover in the air, its flight time is short and the flight speed is slow. Although there are currently some aircrafts that combine multi-rotor aircraft and fixed-wing aircraft, they all have certain defects. When flying in fixed-wing mode, the power of the multi-rotor part must be stopped, and this part becomes a burden on the aircraft. Virtually increased the burden on the aircraft. Contents of the invention [0003] In view of this, the present invention provides a water convertiplane, which can perform vertical lift, hover in the air, and cruise for a long time and a long distance. [0004] A vertical lift aircraft on water, comprising a fuselage, wings,...

AI Technical Summary

Problems solved by technology

[0002] Although the fixed-wing aircraft has a fast flight speed and a long flight time, it cannot hover at a fixed point; although a multi-rotor aircraft can hover in the air, its flight time is short and the flight speed is slow.

Although there are currently some aircrafts that combine multi-rotor aircraft and fixed-wing aircraft, they all have certain defects. When flying in fixed-wing mode, the power of the multi-rotor part must be stopped, and this part becomes a burden on the aircraft. Invisibly increases the burden on the aircraft

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