Stefan Irmisch

Cooled turbine blade or vane for a gas turbine, and use of a turbine blade or vane of this type

Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ring

Method for producing a gas turbine component which is to be coated, with exposed holes, device for carrying out the method, and coatable turbine blade with film cooling holes

Method to produce a coated gas turbine component having opening holes, apparatus to perform the method and coated turbine blade having cooling holes

Gas turbine with a gap blocking device

Cooled turbine blade for a gas turbine and use of such a turbine blade

Clearance blocking device and use of such a clearance blocking device

Method for recording microstructural changes in a component

Gas turbine blade and platform element for a gas-turbine blade ring, supporting structure for fastening it, gas-turbine blade ring and its use

Non destructive monitoring of microstructure changes of a component ( layer system, turbine blades, liners of a combustion chamber )