The invention discloses a two-cycle aviation piston engine drive lubrication cylinder sleeve inner wall laser micro-texturing structure design method. The method comprises the steps that firstly, through analysis modeling on boundary lubrication of the two friction pairs including a piston ring-a cylinder sleeve and a piston skirt-the cylinder sleeve which are abraded most severely, micro texturesfollowing the optimal arranging rules are arranged on the surface of the cylinder sleeve in a targeted mode, pits of the micro textures are filled with various abrasive particles in the up-down strokes of a piston and the piston ring, the cylinder sleeve is prevented from being damaged during pulling, and accordingly, the service lives of the cylinder sleeve and an engine comprising the cylindersleeve are prolonged; and secondly, the micro textures following the optimal arranging rules are utilized for organizing motion of lubricating oil film, the oil film is prevented from being broken, the velocity of motion of the lubricating oil film in the axial direction of an air cylinder is decreased, the component velocity in the circumferential direction of the piston ring is increased, thus,the amount of lubricating oil entering a combusting chamber is decreased, and consumption of the lubricating oil is reduced. Meanwhile, the flow rate of the oil film in the circumferential direction of the piston ring is increased, lubrication is improved, the airtightness of a piston ring set is improved simultaneously, and consumption of the lubricating oil is reduced.