The invention relates to multistage axial flow
air compressor treatment casings, and discloses a self-circulation treatment casing for simultaneously improving
stator corner region flowing. The self-circulation treatment casing comprises a target rotor blade, a downstream
stator blade, a casing body and an air guide
pipe structure located in the casing body. A flow guide cavity structure penetrating the whole circumferential direction is arranged at the position, on the
front edge of a target rotor blade tip, in the casing body. Flow guide cavity outlet front guide vanes used for adjusting the
jet flow direction are circumferentially and evenly arranged on the
front edge of a flow guide cavity outlet, and the outlet directions of the guide vanes are consistent with the pre-rotating direction of the target rotor blade tip. According to the characteristic of stage-by-stage pressurization of a multistage
air compressor, self-adaptive suction and
jet flow are formed under the action of
differential pressure of a downstream
stator blade combined suction groove and the flow guide cavity outlet of the target rotor blade tip; separated flowing of a stator three-dimensional corner region of the
air compressor is effectively restrained, and meanwhile moving blade rotating stall is prevented from happening too early through circumferentially-even
jet flow with the pre-rotating direction consistent with that of the rotor blade tip; the rotor blade rotating stability and margin are increased; and the stable work condition range of the air compressor is widened.