COMPRESSOR

摘要

A discharge port 340a of a compression element 2 is positioned inside an outer circumferential surface of a stator 5, as seen looking in a direction of a rotation axis 12a of a shaft 12, and overlaps the stator 5, as seen looking in a direction orthogonal to the rotation axis 12a of the shaft 12. Accordingly, refrigerant gas discharged from the compression element 2 can be made to flow mainly into spaces inside the outer circumferential surface of the stator 5.