GAS TURBINE COMBUSTOR, CAPABLE OF IMPROVING THE UNIFORMITY OF COMBUSTION AIR BY UNIFORMLY GUIDING A FLOW OF THE COMBUSTION AIR SUPPLIED TO EACH PART OF A COMBUSTOR

摘要

PURPOSE: A gas turbine combustor is provided to completely burn fuel/air-mixed gas of a combustor by uniformly maintaining a flow of combustion air and to reduce a pressure loss.;CONSTITUTION: A gas turbine combustor comprises a casing(10), a liner(20), and an uniform air flow guiding unit(30). A fuel injection nozzle(40) is joined to one side of the casing and combustion air flows into an air inlet unit(50) in the other side of the casing. The liner is coaxially arranged with the casing. An air flowing space is formed between the liner and casing. The liner forms a combustion chamber(20a) of flame ignited by the fuel and combustion air in the inside. The uniform air flowing guiding unit is installed in the air flowing space and uniformly guides a flow of combustion.;COPYRIGHT KIPO 2012