Airplane capable of performing fixed wing flight and vertical take-off and landing based on three-axle flight control panel

Abstract

An airplane capable of performing fixed wing flight and vertical take-off and landing based on a three-axle flight control panel is characterized in the airplane structure and the airplane control connection manner. In the aspect of structure, the airplane is characterized in that front inclination/rotation power capsules are symmetrically arranged on two sides of each wing of the airplane, a rear inclination/rotation power capsule is arranged at the rear part of an airplane body. In the aspect of airplane control connection manner, the airplane is characterized by adopting an innovative connection manner based on a simple three-axle flight control panel, so that the airplane can complete fixed wing flight and vertical take-off and landing under the control of the three-axle flight control panel. The airplane provided by the invention can complete double flight modes including fixed wing flight and vertical take-off and has good maneuverability and high flight efficiency, which is very important for improving the survival rate of the airplane in a war. In addition, the airplane based on the conventional three-axle control panel is convenient and reliable in the control manner and is suitable for mass production.

Description

technical field [0001] The invention relates to an aircraft that realizes fixed-wing and vertical take-off and landing based on a three-axis flight control board. Background technique [0002] With the development of aerospace science and technology, the development of aviation technology is changing with each passing day. In particular, the aircraft that can realize the dual flight modes of fixed wing and vertical take-off and landing represents the advanced aviation technology. Compared with the existing fixed-wing aircraft, the fixed-wing and vertical take-off and landing The aircraft almost does not need a runway, which makes this type of aircraft better in applicability and versatility. It also has the advantages of high flight efficiency and long range of fixed-wing aircraft; vertical take-off and landing aircraft are completely It is generated by the propeller rotation of the engine or motor, and its thrust-to-weight ratio is often required to be greater than 1. Howev...

AI Technical Summary

Problems solved by technology

[0002] With the development of aerospace science and technology, the development of aviation technology is changing with each passing day. In particular, the aircraft that can realize the dual flight modes of fixed wing and vertical take-off and landing represents the advanced aviation technology. Compared with the existing fixed-wing aircraft, the fixed-wing and vertical take-off and landing The aircraft almost does not need a runway, which makes this type of aircraft better in applicability and versatility. It also has the advantages of high flight efficiency and long range of fixed-wing aircraft; vertical take-off and landing aircraft are completely It is generated by the propeller rotation of the engine or motor, and its thrust-to-weight ratio is often required to be greater than 1. However, fixed-wing and vertical take-off and landing aircraft overcome the above shortcomings, greatly improving flight efficiency, longer range, and both vertical take-off and landing aircraft The advantage of maneuverability; this type of aircraft is especially representative of the tilt-rotor aircraft (US military "Osprey" tilt-rotor aircraft), the YY-1 short-distance / vertical take-off and landing UAV of AVIC Qing'an Group Company, and the Israeli aerospace industry The vertical take-off and landing tilt-rotor UAV "Black Panther" and "Osprey" produced by the company are based on two-axis aircraft, which have very high requirements for flight control. The frequent accidents of "Osprey" make everyone seek easier control and safety design; YY-1 short-range / vertical take-off and landing UAV and tilt-rotor UAV "Black Panther" are based on three-axis aircraft, easy to maneuver, good safety, but when doing fixed-wing flight, the tail propeller It cannot provide forward pulling force; it has a propeller at the rear of the aircraft to control the flight direction and improve the maneuverability of the aircraft in the fixed-wing flight mode; with the needs of economic and social development and military technological innovation, more advanced fixed-wing and vertical take-off and landing aircraft continue to emerge

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