Gas turbine combustion control, for vibration reduction of large gas turbines, uses a tin granule filled surface reactor for fuel doping with organo-tin compounds in a temperature-dependent concentration

摘要

Gas turbine combustion control, uses a tin granule filled surface reactor for fuel doping with organo-tin compounds in a concentration dependent on the reactor temperature. Gas turbine combustion control, for vibration reduction of combustion noise caused by turbulent flame acceleration in the turbine combustion chamber, comprises passing the fuel through a surface reactor filled with tin granules to effect fuel doping with organo-tin compounds in a concentration dependent on the reactor temperature.