The invention provides an aircraft with a double-row wheel counter-rotating aerodynamic effect. The aircraft comprises a wing plate, a rotating assembly and an undercarriage, the wing plate is connected to the position over the rotating assembly. The upper projection area of the wing plate is larger than the area of the rotating assembly. The middle of the outer side face of each wing plate is provided with a first protruding end face. The number of the rotating assemblies is two, the two rotating assemblies are connected to the left side and the right side of the inner side face of the wing plate correspondingly, the two rotating assemblies rotate in the direction of the same inner side face a, and a gap is formed between the two rotating assemblies. The rotating assembly comprises a driver, a propeller and a rotating wheel; the propellers and the rotating wheels are connected with the power output end of the driver; the undercarriage is connected with the bottoms of the two rotating wheels of the two rotating assemblies. Airflow is driven to rotate by rotating the blades, upward airflow impacts the inner sides of the wing plates, lift force is provided, the structural design is reasonable, design is novel, consumed energy is low, manufacturing cost is low, and application and popularization prospects are achieved.
本发明提供了一种双排轮对旋气动效应的飞行器,包括翼板、转动组件和起落架;翼板连接在转动组件的正上方位置;翼板的上投影面积大于转动组件的面积;翼板的外侧面中间位置具有第一凸起端面;转动组件的数量为两个,两个转动组件分别连接在翼板内侧面的左右两侧,两个转动组件均向相同的内侧面a方向转动,两个转动组件之间具有间隙;转动组件包括驱动器、螺旋桨和转动轮;螺旋桨、转动轮均与驱动器的动力输出端连接;起落架连接两个转动组件的两个转动轮底部。本发明通过转动叶片带动气流旋转,向上的气流冲击翼板内侧,提供升力,结构设计合理,设计新颖,耗费能量低,制造成本低,具有推广的应用前景。
Aircraft with double-row wheel counter-rotating aerodynamic effect
一种双排轮对旋气动效应的飞行器
2022-04-15
Patent
Elektronische Ressource
Chinesisch
AIRCRAFT HAVING DOUBLE-ROW WHEEL COUNTER-ROTATING PNEUMATIC EFFECT
Europäisches Patentamt | 2023
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