US2013269350A1
|
|
Turbine combustor system having aerodynamic feed cap
|
US2013115566A1
|
|
Combustor having wake air injection
|
US2013111909A1
|
|
Combustion system having a venturi for reducing wakes in an airflow
|
US2013086910A1
|
|
System for fuel injection in a fuel nozzle
|
US2013074471A1
|
|
Turbine combustor and method for temperature control and damping a portion of a combustor
|
US2012186266A1
|
|
Reformed multi-fuel premixed low emission combustor and related method
|
US2012096866A1
|
|
Fuel nozzle for combustor
|
US2012085834A1
|
|
Flame Tolerant Primary Nozzle Design
|
US2012011854A1
|
|
Flame tolerant secondary fuel nozzle
|
US2011289929A1
|
|
Turbomachine fuel nozzle
|
US2011240769A1
|
|
Variable area fuel nozzle
|
US2011162371A1
|
|
Fuel nozzle with integrated passages and method of operation
|
US2011094234A1
|
|
Fuel flexible combustor systems and methods
|
US2011083442A1
|
|
Apparatus and method for cooling nozzles
|
US2010281876A1
|
|
Fuel blanketing by inert gas or less reactive fuel layer to prevent flame holding in premixers
|
US2010269507A1
|
|
Radial lean direct injection burner
|