The application relates to the field of aeroengines, in particular to a two-
stroke aero-
piston engine air intake
system and an air intake flow control method. The
system comprises an
air filter, a
throttle body, an oil
injector, a
reed valve and a
fuel supply unit for supplying oil to the oil
injector which are communicated through a connecting pipeline, and further comprises a cooling control subsystem, the cooling control subsystem comprising a cooling
injector which is arranged on the connecting pipeline downstream of the
throttle body and upstream of the oil injector; the inner wall surface of the connecting pipeline is provided with a non-uniform protruding structure to improve the proportion of the air intake along the resistance. The scheme can solve the technical problem that the air intake flow of the two-
stroke aero-
piston engine has large discreteness under
low load, and realizes the technical effect of improving the consistency of the air intake flow under the
low load of the engine.