COMPRESSOR OF GAS TURBINE SYSTEM

摘要

PROBLEM TO BE SOLVED: To provide a compressor of a gas turbine system.SOLUTION: A compressor 12 includes at least one inlet row 24 having a plurality of inlet guide vanes. Also included is at least one stator row 14 having a plurality of stator vanes. Further included is a first actuation mechanism 32 operably connected to the at least one stator row, wherein the first actuation mechanism is configured to positionally manipulate the at least one stator row. Yet further included is a second actuation mechanism 34 operably connected to the at least one stator row, wherein the second actuation mechanism is configured to positionally manipulate the at least one stator row.