A high-speed long-endurance aircraft
An aircraft, long-endurance technology, applied in the field of flight, can solve the problems of difficult to achieve high-speed range of fixed-wing aircraft, lack of low-altitude and low-speed maneuverability, limited flight speed, etc., to achieve site inclusiveness and improve cruise lift-drag ratio , the effect of increasing the lingering time
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Embodiment 1
[0049] Such as Figure 1-3 , a high-speed long-endurance aircraft, comprising a fuselage 1, wings 2, lift rotor 3, vertical tail 4, horizontal tail 5, propeller 6, rotating rotor system and power system; wherein, the power system is propeller 6, Rotating rotor system and lift rotor 3 provide power. An electronic governor 2 is arranged on the transmission path between the power system and the lift rotor 3 .
[0050] The wing 2 adopts a wing with a large aspect ratio, and is symmetrically arranged on both sides of the fuselage 1; the lift rotor 3 is located above the head of the fuselage 1, and the lift rotor 3 is a coaxial dual rotor, and the upper and lower rotors of the coaxial dual rotor Same speed, opposite direction. Wherein, there are two propulsion paddles 6, which are respectively arranged on the trailing edge of the wing 2, and the propulsion paddles 6 are arranged symmetrically with respect to the fuselage 1; wherein the two propulsion paddles 6 rotate at the same s...
Embodiment 2
[0056] Such as Figure 1-3 , when the aircraft among the present invention is the vertical lift mode: the working principle and the flight method of the aircraft among the present invention are: start the engine of the aircraft among the present invention, and the engine transmits power to the lift rotor 3 by the lift transmission system; The system transmits power to the rotating rotor 11 . Increase the output power of engine now, utilize electronic governor two to control the rotating speed of lift rotor 3; Utilize electronic governor three, control the rotating speed of rotating rotor 11; Make the rotating speed of lifting rotor 3 and rotating rotor 11 increase, further make total When the pulling force increases, when the total pulling force is enough to overcome the weight of the whole machine, the aircraft will rise vertically from the ground; on the contrary, if the output power of the engine is reduced, the aircraft will descend vertically until the aircraft lands in b...
Embodiment 3
[0058] Such as Figure 1-3 , when the aircraft among the present invention was converted into the high-speed level flight mode by the vertical lifting mode, its conversion principle and method were: start the engine of the aircraft among the present invention, and the engine transmits power to the lift rotor 3 through the lift transmission system; The transmission system transmits power to the rotating rotor 11 . Increase the output power of engine now, utilize electronic governor two to control the rotating speed of lift rotor 3; Utilize electronic governor three, control the rotating speed of rotating rotor 11; Make the rotating speed of lifting rotor 3 and rotating rotor 11 increase, further make total The pulling force increases, and when the total pulling force is enough to overcome the weight of the whole machine, the aircraft will rise vertically from the ground. After the aircraft reaches a certain height, start the power supply system, and the battery drives the prop...
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