| 摘要 |
A turbomachine includes at least one rotor ( 6 ), at least one stator ( 7 ), and a casing ( 1 ), with the rotor ( 6 ) comprising several rotor blades ( 8 ) attached to a rotating shaft, and with the stator ( 7 ) being provided with stationary stator blades ( 9 ), the casing ( 1 ) being passed by a fluid flowing through the rotor ( 6 ) and stator ( 7 ). Provision is made for the removal of fluid on at least one blade ( 8, 9 ) of a blade row of the rotor ( 6 ) and/or the stator ( 7 ) on non-axially symmetrical, aerodynamically critical locations on blade tip and annulus surfaces (SRO).
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