SYSTEM AND A METHOD FOR AUTOMATICALLY TUNING A GAS TURBINE COMBUSTION SYSTEM, CAPABLE OF AUTOMATICALLY LEARNING CONTROL DATA THROUGH DYNAMIC CONTROLS WITHOUT USER'S INTERVENTION

摘要

PURPOSE: A system and a method for automatically tuning a gas turbine combustion system are provided to improve the performance and efficiency of a gas turbine because historical archive of information on a state, setting and gas emission is automatically generated.;CONSTITUTION: A method for automatically tuning a gas turbine combustion system comprises the following steps. A first tuning curve is selected from a tuning curve set(700). One or more operation parameters are corrected based on a pre-defined recipe, and the stable operation point of a gas turbine is unbalanced(702). A tuning parameter is determined and stored while the present operation point of the gas turbine returns to the first tuning curve(704). The backup of the tuning parameter is generated to recover the stable operation point(706).;COPYRIGHT KIPO 2013;[Reference numerals] (700) Step of selecting a first tuning curve from a tuning curve set regarding a gas turbine; (702) Step of unbalancing a stable operation point by correcting one or more operation parameters based on a pre-defined recipe; (704) Step of determining and storing a tuning parameter while the present operation point of the gas turbine returns to the first tuning curve; (706) Step of generating backup of the tuning parameter to recover the stable tuning point