|
WO2005061854A1
|
|
Gas turbine tip shroud rails
|
|
US7013718B2
|
|
Method for monitoring the performance of a turbine
|
|
US6733232B2
|
|
Extended tip turbine blade for heavy duty industrial gas turbine
|
|
US6733237B2
|
|
Method and apparatus for mounting stator blades in axial flow compressors
|
|
US6622490B2
|
|
Turbine power plant having an axially loaded floating brush seal
|
|
US6609888B1
|
|
Method and apparatus for reducing contamination in an axial compressor
|
|
US6390673B1
|
|
Method and apparatus for extending the life of a hot gas duct thermowell tube
|
|
US6398518B1
|
|
Method and apparatus for increasing the efficiency of a multi-stage compressor
|
|
US7059827B1
|
|
Turbine power plant having minimal-contact brush seal augmented labyrinth seal
|
|
AU7242998A
|
|
Turbine power plant having minimal-contact brush seal augmented labyrinth seal
|
