|
2020
|
Invention
|
Nozzle and fuel system for operation on gas with varying heating value. A fuel nozzle assembly (3... |
|
2019
|
Invention
|
Nozzle and fuel system for operation on gas with varying heating value. A fuel nozzle assembly fo... |
|
2014
|
Invention
|
Low calorific fuel combustor for gas turbine. A low calorific value fuel-fired can combustor for ... |
|
2011
|
Invention
|
Low calorific fuel combustor for gas turbine. A low calorific value fuel -fired can combustor for... |
|
|
Invention
|
Ultra low emissions gas turbine combustor. The gaseous fuel-fired can combustor for a gas turbine... |
|
|
Invention
|
Apparatus and method for reducing air mass flow for extended range low emissions combustion for s... |
|
|
Invention
|
Turbine inlet nozzle guide vane mounting structure for radial gas turbine engine. Apparatus for c... |
|
2010
|
Invention
|
Low calorific fuel combustor for gas turbine. 3) to heat energy flow rate Q (MJ/sec) in the range... |
|
|
Invention
|
High speed gear coupler. The coupling apparatus includes a gear shaft (30), including a sun gear ... |
|
2009
|
Invention
|
High speed gear coupler. The coupling apparatus includes a gear shaft, including a sun gear at on... |
|
2008
|
Invention
|
Impingement cooled can combustor. A can combustor includes a generally cylindrical housing having... |
|
|
Invention
|
Adjustable compressor bleed system and method. An adjustable bleed apparatus and method for bleed... |
|
|
Invention
|
Single stage dual-entry centriafugal compressor, radial turbine gas generator. A compact, single ... |
|
|
Invention
|
Dual fuel can combustor with automatic liquid fuel purge.
A lean, low NOx gas-fired can combusto... |
|
2004
|
Invention
|
Apparatus and method for gas turbine engine fuel/air premixer exit velocity control. A gas turbin... |