|
US2014060077A1
|
|
Combustor
|
|
US2014020389A1
|
|
Combustor cap assembly
|
|
US2014013756A1
|
|
Combustor
|
|
US2014013723A1
|
|
System and method of supplying fuel to a gas turbine
|
|
US2014000267A1
|
|
Transition duct for a gas turbine
|
|
US2013318976A1
|
|
Turbomachine combustor nozzle and method of forming the same
|
|
US2013298560A1
|
|
System for supplying a working fluid to a combustor
|
|
US2013247581A1
|
|
Systems and methods for dampening combustor dynamics in a micromixer
|
|
US2013213046A1
|
|
Late lean injection system
|
|
US2013122437A1
|
|
Combustor and method for supplying fuel to a combustor
|
|
US2013115561A1
|
|
Combustor and method for supplying fuel to a combustor
|
|
US2013084534A1
|
|
Combustor and method for supplying fuel to a combustor
|
|
US2012304657A1
|
|
Lock leaf hula seal
|
|
US2012306166A1
|
|
Seal assembly for gas turbine
|
|
US2012308947A1
|
|
Combustor having a pressure feed
|
|
US2012304656A1
|
|
Combustion liner and transition piece
|
|
US2012304654A1
|
|
Combustion liner having turbulators
|
|
US2012308948A1
|
|
Combustor nozzle and method for modifying the combustor nozzle
|
|
US2012297784A1
|
|
System and method for flow control in gas turbine engine
|
|
US2012297783A1
|
|
System and method for flow control in gas turbine engine
|
