The present application belongs to the technical field of
aviation piston engine. The present application discloses a kind of cylinder body structure and connecting method of air-cooled two-
stroke aviation piston engine, to solve the problem of
heat load concentration, aluminum
alloy strength decline, cylinder deformation caused by the contact
thermal resistance of aluminum
alloy cylinder and cylinder cover connection area is too large, in the present application, connecting screw and threaded hole are matched with fine thread to increase contact area, reduce contact
thermal resistance and enhance heat conduction performance;Threaded hole
counterbore is treated to reduce the amount of residual gas in the hole, reduce the obstruction of gas to heat conduction;Connecting anti-loosening strictly prohibits the use of thread glue, to avoid local temperature rise. And using TC4
titanium alloy screw material, threaded hole circumferential uniform arrangement and enough connection depth and other supporting design, systematically make the heat of connection area conduct and dissipate efficiently, avoid the strength decline caused by
heat load concentration, improve the anti-deformation ability of cylinder, ensure that the roundness and cylindricity of cylinder meet the design requirements, the engine performance maintains stable under design condition.