An improved combustor for a gas turbine is operable to provide high combustion efficiency in a compact combustion chamber. The combustor includes a counter swirl doublet for improved fuel/air mixing. The enhanced combustor assembly and method of operation improves operation of the turbine.
申请公布号
WO2014149081(A1)
申请公布日期
2014.09.25
申请号
WO2013US68704
申请日期
2013.11.06
申请人
ROLLS-ROYCE CORPORATION
发明人
GRAVES, CHARLES, B.;WICKSALL, DONALD, MCKINLEY;RICHARDSON, THOMAS, FRED, JR.
