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Inventor: Hans-Peter Bossmann


Address: Lauchringen, DE
No. of applications: 8
Last application issue date: 12/08/2011

Application No.Application TitleIssue Date
20110300357THERMAL BARRIER COATING SYSTEM, COMPONENTS COATED THEREWITH AND METHOD FOR APPLYING A THERMAL BARRIER COATING SYSTEM TO COMPONENTS
A thermal barrier coating system on a base material includes a bond coat layer with a lower face in direct contact with the base material and an upper face, a first ceramic layer in direct contact with the upper face of the bond coating layer and a second ceramic layer ...
12/08/2011
20110058953TURBINE 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 gase...
03/10/2011
20100247953MULTILAYER 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 a...
09/30/2010
20100150727ROTOR BLADE FOR A GAS TURBINE
A rotor blade (10) for a gas turbine includes a blade airfoil (11), a blade tip (15), a blade root (14), and a platform (12) which is formed between the blade tip (15) and the blade root (14), and is assembled from a plur...
06/17/2010
20100124502ROTOR BLADE ARRANGEMENT AND GAS TURBINE
A rotor blade arrangement (20), especially for a gas turbine, which can be fastened on a blade carrier (19) and includes in each case a blade aerofoil element (10) and a platform element (14), wherein the platform elements (14) of a bl...
05/20/2010
20090324989MULTILAYER THERMAL BARRIER COATING
Components (1) have a thermal barrier coating (2-6) on the surface thereof, wherein the thermal barrier coating includes at least one layer (3) having chemically stabilized zirconia, and wherein at least indirectly adjacent to the layer (3...
12/31/2009
20090061530METHOD 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 (ZrO2) stabilized with yttrium oxide (Y2O3) [YSZ], and for determining its operating time or operating temperature is provided. The met...
03/05/2009
20050042474High-temperature protection layer
A high-temperature protection layer contains (% by weight) 23 to 27% Cr, 4 to 7% Al, 0.1 to 3% Si, 0.1 to 3% Ta, 0.2 to 2% Y, 0.001 to 0.01% B, 0.001 to 0.01% Mg and 0.001 to 0.01% Ca, remainder Ni and inevitable impurities. Optionally, the Al content is in a range from...
02/24/2005
 
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