CORE GAS PATH BOUNDARY STRUCTURE FOR GAS TURBINE ENGINE
卷宗概要
发明人
Philippe Boyer; Jocelyn Bisson; Jasrobin Grewal
IPC 分类
CPC 分类
A core gas path boundary structure is provided that includes an annular housing panel and a baffle. The annular housing panel has a first end segment and a second end segment. The first end segment of the housing panel (HPFES) has an HPFES outer radial surface and a HPFES support rail extending radially outward from the HPFES outer radial surface. The baffle has a body and a first stiffening ring. The body has a baffle first end segment and a baffle second end segment. The first stiffening ring is attached to an inner radial surface of the baffle first end segment. The first stiffening ring has an edge surface. The baffle is engaged with the annular housing panel such that the baffle first end segment is in contact with the HPFES support rail. The edge surface of the first stiffening ring is radially aligned with the HPFES support rail.
原文（中文）
A core gas path boundary structure is provided that includes an annular housing panel and a baffle. The annular housing panel has a first end segment and a second end segment. The first end segment of the housing panel (HPFES) has an HPFES outer radial surface and a HPFES support rail extending radially outward from the HPFES outer radial surface. The baffle has a body and a first stiffening ring. The body has a baffle first end segment and a baffle second end segment. The first stiffening ring is attached to an inner radial surface of the baffle first end segment. The first stiffening ring has an edge surface. The baffle is engaged with the annular housing panel such that the baffle first end segment is in contact with the HPFES support rail. The edge surface of the first stiffening ring is radially aligned with the HPFES support rail.