Compressor for a gas turbine engine with radially divided cooling air bleed manifold

摘要

The compressor (10) has a flow path (14) defined radially outward from an outer wall (26). A compressor casing (32) encompasses the wall under formation of a collecting space (44) that is arranged between the wall and the casing. A removal opening (40) is present in the wall for releasing a portion of a medium (18) in the space. An opening (64) is arranged with the casing for discharging the released portion of the medium from the casing. A separative element (46) is provided in the space for separating the space into a radially inner subspace (48) and a radially outer subspace (50).