Tailstock type vector differential biaxial aircraft

Abstract

The invention discloses a tailstock type vector differential biaxial aircraft. The tailstock type vector differential biaxial aircraft comprises a main wing, a vector motor base, a canard and an mwc flight controller. Sweepback wings are adopted as the main wing to provide main lift force. The canard is located at the front end of the main wing and used for increasing the overall stall angle of attack of the aircraft and providing lift force. The vector motor seat is arranged at the tail part of the main wing and is used for overcoming the flight resistance and self-gravity of the aircraft. The flight controller automatically detects the posture during hovering, and automatically changes the direction of the motor base and the rotating speed of the motor when the posture is abnormal, so that the motor base is stable. Characteristics of a rotor aircraft and a fixed-wing aircraft are combined, a vector technology is introduced, and a low-power engine is selected to be fixed to a vector motor base; double engines, a special airfoil profile, a moderate aspect ratio, canard wings and a wing end stabilizing surface are adopted, and the requirements for rapid small-attack-angle flight, hovering, low-speed large-attack-angle flight and rapid steering and attack angle change under a complex site can be met.

Description

technical field [0001] The invention relates to the field of vertical take-off and landing aircraft, in particular to a tailstock type vector differential two-axis aircraft. Background technique [0002] Most of the existing civil small aircraft are rotor-type and fixed-wing aircraft. Rotor-type aircraft can meet the low-speed flight work in various environments. This type of aircraft changes the flight attitude by changing the pitch of the propeller, which has low aerodynamic efficiency. , Low power load, difficult maneuvering, unstable flight, and the flight speed cannot be increased. However, fixed-wing aircraft need to reach a certain speed to take off, which cannot meet the requirements of low-speed flight missions, and have requirements for take-off and landing sites. Vector aircraft are mostly used in the military field, with the characteristics of high efficiency, good flexibility, and high adaptability to flight attitude, but they are rarely involved in civilian in...

AI Technical Summary

Problems solved by technology

[0002] Most of the existing civil small aircraft are rotor-type and fixed-wing aircraft. Rotor-type aircraft can meet the low-speed flight work in various environments. This type of aircraft changes the flight attitude by changing the pitch of the propeller, which has low aerodynamic efficiency. , low power load, difficult maneuvering, unstable flight, and the flight speed cannot be increased

However, fixed-wing aircraft need to reach a certain speed to take off, which cannot meet the requirements of low-speed flight missions, and have requirements for take-off and landing sites

Vector aircraft are mostly used in the military field, with the characteristics of high efficiency, good flexibility, and high adaptability to flight attitude, but they are rarely involved in civilian industries.

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