|
US2005235649A1
|
|
Method for operating a gas turbine
|
|
US2006283920A1
|
|
Vibration stress relief of superalloy components
|
|
US2006283660A1
|
|
Acoustic termination for a pressure monitoring system
|
|
US2006283921A1
|
|
Method of diffusion bonding of nickel based superalloy substrates
|
|
US2005277721A1
|
|
High thermal conductivity materials aligned within resins
|
|
US2005277349A1
|
|
High thermal conductivity materials incorporated into resins
|
|
US2006275553A1
|
|
Electrically conductive thermal barrier coatings capable for use in electrode discharge machining
|
|
US2006254280A1
|
|
Combined cycle power plant using compressor air extraction
|
|
US2005198967A1
|
|
Smart component for use in an operating environment
|
|
US2006252308A1
|
|
Hazard boundary termination box
|
|
US2006219758A1
|
|
Welding of gamma'-strengthened superalloys
|
|
US2006213274A1
|
|
Nondestructive inspection heads for components having limited surrounding space
|
|
US2006188357A1
|
|
Nut cap and method of securing a nut on a bolt
|
|
US2006182649A1
|
|
High strength oxidation resistant superalloy with enhanced coating compatibility
|
|
US2006156734A1
|
|
Gas turbine combustor
|
|
US6930434B1
|
|
Generator rotor pole crossover
|
|
US2006088793A1
|
|
Optical viewing system for monitoring a wide angle area of interest exposed to high temperature
|
|
US7035763B2
|
|
Systems and methods for selecting training data and generating fault models for use in use sensor-based monitoring
|
|
CA2477486A1
|
|
System and method for processing inspection data for evaluating degradation of coatings on components
|
|
US2005038817A1
|
|
System and method for processing inspection data for evaluating degradation of coating on components
|
