02-06-2023 дата публикации
Номер: CN116198757A
Принадлежит:
The invention provides a 2N + 1-axis aircraft, which relates to the technical field of spaceflight, and comprises a fuselage, an even number of middle rotors and 2N small rotors, a main shaft is arranged on the fuselage, and the even number of middle rotors are coaxially arranged on the main shaft; and the 2N small rotors are connected to the fuselage and are regularly distributed around the main shaft. The aircraft has the beneficial effects that the aircraft comprises the aircraft body, the even number of middle rotor wings and the 2N small rotor wings, the rotation of the middle rotor wings and the small rotor wings provides lift force, and the even number of middle rotor wings are coaxially arranged on the main shaft, so that the length size of the middle rotor wings can be properly lengthened, and the lift force generated when the middle rotor wings rotate is stronger; the stability is better, and the wind resistance is good; the main shaft is provided with the autorotation rotor wing ...
Подробнее