WO2007008238A2
|
|
Turbine component fixture for manufacture or repair
|
US7146990B1
|
|
Process for repairing sulfidation damaged turbine components
|
KR20060127005A
|
|
Durable thermal barrier coating having low thermal conductivity
|
WO2005045198A2
|
|
A turbine blade and a method of manufacturing and repairing a turbine blade
|
US6872912B1
|
|
Welding single crystal articles
|
US7041383B2
|
|
Durable thermal barrier coating having low thermal conductivity
|
US6764779B1
|
|
Thermal barrier coating having low thermal conductivity
|
US6803135B2
|
|
Thermal barrier coating having low thermal conductivity
|
US6380512B1
|
|
Method for removing coating material from a cooling hole of a gas turbine engine component
|
US6537021B2
|
|
Abradeable seal system
|
US6502303B2
|
|
Method of repairing a turbine blade tip
|
US6420677B1
|
|
Laser machining cooling holes in gas turbine components
|
US6573474B1
|
|
Process for drilling holes through a thermal barrier coating
|
US6333484B1
|
|
Welding superalloy articles
|
US6154959A
|
|
Laser cladding a turbine engine vane platform
|
US6173491B1
|
|
Method for replacing a turbine vane airfoil
|
US6107598A
|
|
Maskant for use during laser welding or drilling
|
US6206081B1
|
|
Withdrawal elevator mechanism for withdrawal furnace with a center cooling spool to produce DS/SC turbine airfoils
|
US6209618B1
|
|
Spool shields for producing variable thermal gradients in an investment casting withdrawal furnace
|
US6037563A
|
|
Protective gas shroud for welding
|