Patent ID: 6276142
Filing Date: 2001-08-21
Classification: F05B,F23M,F23R

Abstract:
A gas turbine, comprising:a combustion chamber with an inner wall acting as a supporting structure; anda heat-shield configuration including a plurality of heat-shield components disposed next to one another for attachment to said supporting structure, each of said heat-shield components having:an outer hollow body to be attached to the supporting structure, said outer hollow body having side walls and a first base side to be exposed to a hot gas;an insert to be attached to the supporting structure, said insert enclosed by said outer hollow body and defining an intermediate space between said outer hollow body and said insert, said insert having side walls and a second base side with a plurality of openings for passage of cooling fluid into said intermediate space; anda hot gas directing component wall to be exposed to a hot gas, said wall formed by said first and second base sides of said heat-shield component.