COMPONENT FOR A COMBUSTION CHAMBER OF A GAS TURBINE
The invention relates to a component for a combustion chamber of a gas turbine, which component has a multi-layer structure in the form of ceramic films and/or paper made of pre-ceramic material, the inner and outer structure of the component being matched to the dimensions and conditions in the gas turbine combustion chamber. The invention further relates to a gas turbine combustion chamber having the component and to a method for producing the component.