A composite wing aircraft and a flight control method thereof

Abstract

The invention discloses a composite wing aviation aircraft and a flight control method thereof, A composite wing aerocraft includes a fuselage, The left wing and the right wing are symmetrically arranged on the side of the fuselage, the flight controller is arranged inside the fuselage, the integral plastic frame is connected above the fuselage, the top end of the frame is provided with a rotor, the tail part of the fuselage is provided with a propeller connected with the output shaft of the engine, and the rotor is connected with the output shaft of the engine through a clutch transmission mechanism. As that composite-wing aeronautical aircraft comprise a rotor and a fixed wing, the take-off distance is shorten and the flight speed and the flight efficiency are improved through driving control and rotational speed control of different stages of the rotor. The composite-wing aeronautical aircraft comprise a rotor and a fixed wing.

Description

technical field [0001] The invention relates to the field of aviation flight, in particular to a compound wing aircraft and a flight control method thereof. Background technique [0002] Human beings' pursuit of aircraft has never stopped. Since the beginning of the 21st century, with the development of general aviation, there are more and more types of aircraft, and the society's demand for air vehicles is increasing, and the application range is wider and wider. For example: aerial photography, agriculture, forestry and plant protection, police inspection, power inspection, geological exploration, battlefield investigation, special reconnaissance, material transportation, sea and air joint search and other fields. However, the existing general aircrafts generally include several types of aircraft such as fixed-wing, helicopter, multi-rotor and tilt-rotor aircraft, and the emphasis can only be chosen between low speed and high speed, and the flight speed range and flight ra...

AI Technical Summary

Problems solved by technology

However, the existing general aircrafts generally include several types of aircraft such as fixed-wing, helicopter, multi-rotor and tilt-rotor aircraft, and the focus can only be chosen between low speed and high speed, and the flight speed range and flight range are small. , so the scope of application is relatively small

The main disadvantages are as follows: 1. High requirements on the runway, such as fixed-wing; 2. Once the air engine stops, it is easy to crash, such as fixed-wing, helicopter, and multi-rotor; 3. The cruising speed is low, such as helicopter, multi-rotor , Autogyro; 4. High technical requirements for pilots, such as fixed-wing, helicopters, etc.

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