Refractory tile with reinforcing members embedded therein, as liner for gas turbine combustion chamber

摘要

Heat shield element (26), especially for the inner lining of a combustion chamber of a gas turbine, comprises a base body (28) made of a strengthened cast ceramic material containing a number of reinforcing elements (30). Independent claims are also included for: (1) Combustion chamber with an inner lining comprising heat shield elements; and (2) Gas turbine comprising the above combustion chamber. Preferred Features: Each reinforcing element is made of a ceramic composite material.