This invention belongs to the field of variable wing technology and discloses a lightweight integrated aerodynamic drive
system and a deformable wing. The aerodynamic drive
system includes: a double-acting cylinder integrated with the valve bodies of a normally open and normally closed electromagnetic
directional valve via a
cylinder head; a combined valve comprising an inflation valve and a pressure reducing valve; the inflation valve is located above the pressure reducing valve, with its valve body integrated with the pressure reducing valve's valve body, and its outlet flow channel directly connected to the pressure reducing valve's
inlet flow channel; the pressure reducing valve is located on the top of the front
cylinder head of the double-acting cylinder, and is connected to the normally open electromagnetic
directional valve via a gas-sealed connection, directly docking with a
gas cylinder. This
system combines optimized gas
path design and hardware integration, integrating energy and drive functions, resulting in a compact and lightweight structure. It can adapt well to the requirements of limited installation space, significantly improving the system's adaptability to various operating conditions, thereby enhancing the aircraft's flight performance.