The invention discloses an A-wing aircraft capable of realizing vertical take-off and landing and horizontal flight, and belongs to the technical field of aviation. Comprising a fuselage, wings, driving devices, undercarriages and a control mechanism, the A-wing aircraft is provided with large-area shell-shaped wide-chord wings, multiple rows of driving devices are arranged on the upper portions and the lower portions of the shell-shaped wings, and layered driving airflow is generated on the surfaces of the wings; the wing and the driving devices are divided into a plurality of subareas by taking the pneumatic center of the large-area shell-shaped wide-chord wing as an original point; by adjusting the power of the upper driving device and/or the power of the lower driving device of the shell-shaped wing in a certain subarea, namely adjusting the pressure intensity of the layered driving airflow on the upper surface and/or the pressure intensity of the layered driving airflow on the lower surface of the shell-shaped wing in the subarea, the stress of the upper wing surface and/or the stress of the lower wing surface of the shell-shaped wing in the subarea are/is changed. The flight attitude of the large-area shell-shaped wide-chord wing is adjusted by changing the upper and lower stress of each subarea wing surface of the wing, so that vertical take-off and landing and horizontal flight are realized.
本发明公开一种实现垂直起降和水平飞行的甲翼机,属于航空技术领域。包括机身、机翼、驱动装置、起落架和操控机构,甲翼机具有大面积壳状宽弦机翼,壳状机翼的上下部设有多排驱动装置,在机翼表面产生层状驱动气流;将众多的驱动装置以大面积壳状宽弦机翼的气动中心为原点将机翼和驱动装置分为若干分区;通过调节某个分区的壳状机翼上部驱动装置的功率和/或下部驱动装置的功率,即调整该分区的壳状机翼上表面层状驱动气流的压强和/或下表面层状驱动气流的压强,从而改变该分区的壳状机翼上翼面的受力和/或下翼面的受力,通过改变机翼各个分区翼面上下的受力来调整大面积壳状宽弦机翼的飞行姿态,实现垂直起降和水平飞行。
A-wing aircraft capable of realizing vertical take-off and landing and horizontal flight
一种实现垂直起降和水平飞行的甲翼机
2022-08-02
Patent
Elektronische Ressource
Chinesisch
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