Stator arrangement for compressor of fluid conveying arrangement in gas turbine engine, has radial passage conduit formed in part of stator ring segment, where radial passage conduit is arranged adjacent to stator blade passage conduit

摘要

The arrangement has a stator ring passage conduit formed in a part of a radial inner surface of a housing, and a stator ring segment (154) inserted into a part of the stator ring passage conduit. A stator blade passage conduit (156) is formed in a part of the stator ring segment, and a radial passage conduit (200) is formed in the part of the segment, where the radial passage conduit is arranged adjacent to the stator blade passage conduit. The radial passage conduit is formed in the segment at a position, which is preset in an axial direction and a peripheral direction.