Stator splitter blades with single-stage transonic axial compressor

摘要

A single-stage transonic axial-flow compressor with a stator splitter blade is disclosed. The single stage transonic axial compressor includes a casing having an internal space formed therein; A rotating shaft that rotates inside the casing; A rotor hub fixedly coupled to the rotating shaft and rotated together with the rotating shaft; A plurality of rotor blades spaced apart in a circumferential direction of the rotor hub; A stator blade coupled to the casing and disposed alternately with the rotor blade; And a splitter blade spaced apart from the stator blade at an angle with respect to the rotation axis.