The invention relates to a vertical take-off and landing (VTOL) efficient and high-speed aircraft. A composite tilting wing longitudinal variable-wing reverse-speed rotor aircraft is characterized inthat a main lift rotor set 5 is longitudinally arranged on the upper portion of an aircraft body 1, two pairs of convertible blades 9 are arranged on the main lift rotor set 5, a fixed wing 2 is arranged in the middle of the aircraft body 1, a power stub wing 4 is arranged on the fixed wing 2, and an aileron 8 is arranged on the power stub wing 4; a horizontal tail 3, a vertical tail 6 and an undercarriage 7 are arranged on the aircraft body 1. The power stub 4 tilts, and the rotor-wing conversion enables the composite tilting wing tandem variable-wing reverse-speed rotor aircraft to truly become a high-speed helicopter capable of vertically taking off, landing and hovering, and the composite tilting wing tandem variable-wing reverse-speed rotor aircraft has great significance in nationaleconomy and national defense construction.
本发明涉及一种垂直起降(VTOL)高效、高速飞行器。复合式倾转机翼纵列变翼逆速旋翼飞行器,其特征在于机体1上部纵列布置主升力旋翼组5,主升力旋翼组5上布置有两副可转换桨叶9,机体1中部布置有固定机翼2,固定机翼2上布置有动力短翼4,动力短翼4上布置有副翼8,机体1上布置有水平尾翼3、垂直尾翼6、起落架7。动力短翼4倾转、旋翼—机翼转换使复合式倾转机翼纵列变翼逆速旋翼飞行器真正成为一款可垂直起降、悬停的高速直升飞机,在国民经济及国防建设中具有重大意义。
Composite tilting wing tandem variable-wing reverse-speed rotor aircraft
复合式倾转机翼纵列变翼逆速旋翼飞行器
2020-12-04
Patent
Electronic Resource
Chinese
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