Hans-Thomas Bolms

Gap control system for turbine engines

Seal element for sealing a gap and combustion turbine having a seal element

Impingement cooled wall

Construction element for use in a thermal machine

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

Layer structure and method for producing such a layer structure

Layered structure and method to produce such a layered structure

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

Turbine blade and gas turbine equipped with a turbine blade

Heat shield element