GAS TURBINE ENGINE COMPONENT WITH FLOW SEPARATING RIB

摘要

A component (60) includes a wall (80) that extends about a cooling cavity (72). The cooling cavity (72) is a dual-fed cavity that is fed from at least two different locations. A rib (82) separates the cooling cavity (72) into a first portion (86) and a second portion that is fluidly isolated from the first portion (84).