Method for realizing flight control of A-wing aircraft

• 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 a method for realizing flight control of an A-wing aircraft, and belongs to the technical field of aviation. The A-wing aircraft is provided with a large-area shell-shaped wide-chord wing, a plurality of rows of driving devices are arranged above and below the shell-shaped wing, and layered driving airflow is generated on the surface of the wing; 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 subare