A vertical take-off and landing aircraft with multiple axes combined with fixed wings

Abstract

The invention relates to a vertical take-off and landing aircraft with multiple axes combined fixed wings, belonging to the technical field of aircraft, comprising a fuselage, a wing, a tail wing, a transmission rod, an operation rod, a cross beam, a multi-rotor device and a landing gear. The wing is provided with an aileron, the left section and the right section of the wing are symmetrically provided with notches, and the notches are parallel to the central axis of the fuselage. The tail includes a horizontal tail and a vertical tail, which are located at the end of the fuselage. The transmission rod is located at the position of the lift point of the wing, and is arranged on the left and right sections of the wing through bearings. The operating lever is arranged in the fuselage, and isconnected with the transmission lever through a gear set for controlling the rotation angle of the transmission lever. The invention relates to a multi-axis vertical take-off and landing fixed-wing aircraft, which combines the advantages of a multi-rotor device and a fixed-wing aircraft, can carry out vertical take-off and landing, hovering in the air, long sailing time, stable flight process, high safety factor, and is suitable for logistics transportation, air fire extinguishing, post-disaster rescue and the like.

Description

technical field [0001] A vertical take-off and landing aircraft combined with multi-axis and fixed wings belongs to the technical field of aircraft, in particular to a vertical take-off and landing fixed-wing aircraft. Background technique [0002] Although the aircraft flies fast and has a long flight time, it cannot hover at a fixed point, nor can it take off and land vertically; although a multi-rotor aircraft, also known as a multi-axis aircraft, can hover in the air and take off and land vertically, its navigation The time is short and the flight speed is slow. Although there are also some aircrafts that combine multi-rotor aircraft and aircraft at present, they have certain defects. When flying in fixed-wing mode, the power of the multi-rotor part must be stopped, and this part has become a burden on the aircraft. Increased aircraft load. Contents of the invention [0003] In order to overcome the deficiencies of the above-mentioned prior art, the present invention...

AI Technical Summary

Problems solved by technology

[0002] Although the aircraft flies fast and has a long flight time, it cannot hover at a fixed point, nor can it take off and land vertically; although a multi-rotor aircraft, also known as a multi-axis aircraft, can hover in the air and take off and land vertically, its navigation Time is short, flight speed is slow

Although there are also some aircrafts that combine multi-rotor aircraft and aircraft at present, they have certain defects. When flying in fixed-wing mode, the power of the multi-rotor part must be stopped, and this part has become a burden on the aircraft. Increased aircraft load

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