Disc type rotor craft

Abstract

The invention relates to a disc type rotor craft. The disc type rotor craft. The disc type rotor craft comprises a body, a rotor system, a landing gear and a control system, wherein the rotor system comprises a disc type rotor and n movable control surfaces, control surface openings are evenly formed in the upper surface of the disc type rotor, the middle of the lower bottom surface of the disc type rotor is connected with an engine transmission system through a central shaft, the movable control surfaces are embedded into the control surface openings, the middle of each movable control surface is movably connected with the disc type rotor through a rotary shaft, and the movable control surfaces can be driven by the rotary shafts to rotate relative to the disc type rotor; the control system comprises an automatic inclinator for controlling the pitching angle of the disc type rotor and a control surface control mechanism for controlling the rotating angles of the movable control surfaces, and the control surface control mechanism comprises a control surface control disc and a control surface drive motor. The rotor craft further comprises a balance propeller and a duct type propeller. The disc type rotor craft which utilizes the aerodynamics feature of the disc type rotor is good in stability, low in power consumption, high in interference resistance, high in cruising ability, convenient to control, high in operability and high in safety.

Description

technical field

[0001] The invention relates to the technical field of aviation aircraft, in particular to a dish rotor aircraft. Background technique

[0002] There are many types of existing aircraft, including airplanes, helicopters, disc aircraft, rotorcraft, etc., which can be widely used in transportation, patrol, tourism, rescue and other fields, but the aircraft currently in use:

[0003] 1. The structure of the propeller aircraft is complex and difficult to control;

[0004] 2. Due to the high force requirements of the propeller, the manufacturing materials and processes of the helicopter are complicated, the manufacturing cost is high, and the aerodynamic stability and controllability are poor, and the endurance is weak, resulting in frequent accidents;

[0005] 3. The multi-rotor UAV has a complex structure and poor anti-interference ability. Due to the turbulent flow and wingtip stall generated during the propeller movement, it is easy to cause a drop in lift...

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