A-wing aircraft capable of realizing vertical take-off and landing and horizontal flight

• Main Author: YANG WEIHUA
• Format: Patent
• Language: Chinese; English
• Published: 02.08.2022
• Subjects: AEROPLANES; AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; HELICOPTERS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

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-