| Patent application number | Description | Published |
|---|
| 20090061530 | METHOD FOR DESIGNATING A COMPONENT HAVING A HEAT INSULATION LAYER AND FOR DETERMINING ITS OPERATING TIME - A method for designating a component, coated with a heat insulation layer including zirconium dioxide (ZrO | 03-05-2009 |
| 20090324989 | MULTILAYER THERMAL BARRIER COATING - Components ( | 12-31-2009 |
| 20100124502 | ROTOR BLADE ARRANGEMENT AND GAS TURBINE - A rotor blade arrangement ( | 05-20-2010 |
| 20100150727 | ROTOR BLADE FOR A GAS TURBINE - A rotor blade ( | 06-17-2010 |
| 20100247953 | MULTILAYER THERMAL PROTECTION SYSTEM AND METHOD FOR MAKING SAME - A multilayer thermal protection system includes a metallic substrate; a first ceramic layer; a bond coat layer attaching the first ceramic layer to the metallic substrate, wherein the first ceramic layer is applied by plasma spraying; at least one second ceramic layer attached to the first ceramic layer, wherein the at least one second ceramic layer includes monolithic ceramic elements adhesively attached to the first ceramic layer; and a ceramic adhesive layer attaching the at least one second ceramic layer to the first ceramic layer. | 09-30-2010 |
| 20110058953 | TURBINE BLADE - A turbine blade is provided having an airfoil and a platform manufactured in two separate pieces, which are joined together. The blade includes a seal, which is a mechanically decoupled seal, interposed between the airfoil and platform in a position closer to a hot gases path than a joint. | 03-10-2011 |
