Wings of the aircraft comprise an inner wing fixedly connected with a fuselage and an outer wing connected with the inner wing, the outer wing is divided into two parts, each part of the outer wing is connected with a power system, the power systems are connected with propellers, and the propellers are connected with the inner wing. Aerodynamic layout configuration conversion is carried out through rotation, separation or splicing combination conversion of each part of outer wings, so that the aircraft is converted between a vertical take-off and landing mode and a fixed wing cruising mode. The defects of a traditional composite wing vertical take-off and landing aircraft are overcome, and meanwhile the multi-rotor-wing vertical take-off and landing aircraft has the multi-rotor-wing high hovering efficiency and the fixed wing high-speed cruise flight aerodynamic efficiency.
本发明提供了一种变构型垂直起降飞行器,飞行器的机翼包括与机身固连的内机翼和与内机翼连接的外翼,所述外翼分割为2部分,每部分外翼连接有动力系统,动力系统连接螺旋桨,通过每部分外翼的旋转、分离或拼接组合变换进行气动布局构型转换,使飞行器在垂直起降模式和固定翼巡航模式之间转换。本发明避免了传统复合翼垂直起降飞行器的缺点,同时具备多旋翼高悬停效率和固定翼的高速巡航飞行气动效率。
Variable-configuration vertical take-off and landing aircraft
一种变构型垂直起降飞行器
2023-03-24
Patent
Elektronische Ressource
Chinesisch
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