AUTOMATIC COMBUSTION TUNING DEVICE AND A METHOD FOR A GAS TURBINE, USING MULTIPLE SENSIBILITY ANALYSIS TECHNIQUE

摘要

PURPOSE: An automatic combustion tuning device and a method for a gas turbine, using multiple sensibility analysis technique, are provided to perform a gas turbine combustion tuning with less power in a short time.;CONSTITUTION: An automatic combustion tuning device comprises a compressor(101), a combustor(102), a gas turbine(103), a dynamic measuring sensor, an exhaust gas analyze(105) and a combustion tuning main body(106). The compressor inputs air through an air inlet duct. The combustor inputs the fuel through a fuel conduit. The gas turbine exhausts the combustion gas through an air discharge duct. The dynamic measuring sensor measures the vibration pressure of the combustor.;COPYRIGHT KIPO 2011