Variable-mode cross-type single-propeller dual-rotor aircraft and working method thereof

Abstract

The invention discloses a variable-mode cross type single-propeller double-rotor aircraft and a working method thereof. According to the technical scheme, the variable-mode cross type single-propeller double-rotor aircraft is characterized by comprising an aircraft body and an undercarriage arranged on the aircraft body, wings are further arranged on the side portion of the aircraft body, rotor cases are symmetrically installed on the aircraft body, a transmission device is arranged in any rotor receiver, a power source is arranged in the aircraft body, the power source is used for driving the transmission device to rotate, the transmission device is connected with a single-propeller rotor mechanism, the rotor cases drive the single-propeller rotor mechanism to rotate through transmission of the transmission device, the single-propeller rotors symmetrically arranged along the fuselage are arranged in a crossed mode, rotating shaft of the single-propeller rotor mechanism and the rotor case are coaxially arranged, a three-blade propeller is arranged at the wingtip of the single-propeller rotor mechanism, a brake limiting component is further arranged in the rotor case, and the brake limiting component is used for braking rotation of the single-propeller rotor mechanism and controlling the single-propeller rotor mechanism to keep parallel to the fuselage; and the variable-mode cross type single-propeller double-rotor aircraft has the effects of improving the cruising speed and the voyage during flight work.

Description

technical field [0001] The present invention relates to the technical field of aircraft, and more specifically relates to a variable-mode intersecting single-blade dual-rotor aircraft and a working method thereof. Background technique [0002] With the rapid development of industry and aviation, many new configurations of aircraft have been proposed and put into use, prompting continuous innovation in the types and functions of aircraft, and many different types of aircraft have been derived, among which helicopters have vertical take-off and landing , the function of hovering in the air, but the flight speed is low, and it is difficult to improve the range and flight time. The fixed-wing aircraft can cruise at high speed, but it needs to take off and land with the help of running to taxiing. The tilt-rotor aircraft combines the functions of the rotor aircraft and the fixed-wing aircraft. Advantages, with the advantages of vertical takeoff and landing, air hovering, long ran...

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Problems solved by technology

[0002] With the rapid development of industry and aviation, many new configurations of aircraft have been proposed and put into use, prompting continuous innovation in the types and functions of aircraft, and many different types of aircraft have been derived, among which helicopters have vertical take-off and landing , the function of hovering in the air, but the flight speed is low, and it is difficult to improve the range and flight time. The fixed-wing aircraft can cruise at high speed, but it needs to take off and land with the help of running to taxiing. The tilt-rotor aircraft combines the functions of the rotor aircraft and the fixed-wing aircraft. Advantages, with the advantages of vertical takeoff and landing, air hovering, long range and long endurance. At present, most innovative aircraft are aimed at combining fixed-wing aircraft and rotary-wing aircraft, and few programs are based on helicopters. Innovate and optimize

[0003] Existing comparatively new type of helicopter is double-rotor cross-rotor helicopter. The rotating shafts of the two rotors are not parallel, and the blades are arranged crosswise on the top of the fuselage. The direction of rotation of the blades is opposite. It is not easy to collide and interfere with each other, and has high stability of the whole machine, and can perform large lifting tasks, but it still has the effect of vertical take-off and landing and hovering in the air, and it still has a cruising speed when cruising. The common problems of low speed and short range, so a new model can solve the problems of low cruising speed and short range of existing helicopters

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