A special-shaped aircraft

Abstract

A special-shaped aircraft belongs to the technical field of aircraft, which comprises a fuselage, a wing, a tail wing, a left thrust device, a right thrust device, a front spar, a rear spar, a transmission rod and a landing gear. The wing has a definite angle of attack. The two wings on both sides of the fuselage are divided into an inner wing and an outer wing. The inner wing is connected to thefuselage, the outer wing is connected to the inner wing through a front spar and a rear spar, and there is a certain gap between the inner wing and the outer wing. The front and rear spar penetrate the wings on either side of the fuselage. The transverse arrangement of the transmission rods is at the center of gravity of the aircraft. The left thrust device and the right thrust device have the same structure, and both the left thrust device and the right thrust device provide thrust force in the form that the motor drives the propeller to rotate; a left thrust device and a right thrust deviceare symmetrically arrange on both sides of that fuselage and are connected to drive rods positioned between the inner wing and the out wing through a support frame. The invention combines the advantages of a multi-rotor device and a fixed-wing aircraft, and can carry out vertical take-off and landing, hover in the air, have long flight time, stable flight process and high safety factor.

Description

technical field [0001] A special-shaped aircraft 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 above-mentioned deficiencies in the prior art, the present invention provides a special-shaped aircraft capable of vertical ...

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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