GAS TURBINE ENGINE COMPONENT AND CORRESPONDING WALL

摘要

A gas turbine engine component (60) includes a wall having an inner surface and an outer surface (72). At least one non-rectangular slot (84) extends through the outer wall surface and is in communication with a passage (94). The passages (94) extend through the wall and include an inlet portion (96) located at the inner surface and an outlet portion (100) located at the outer surface. An intermediate portion (98) fluidly connects the inlet portion (96) and the outlet portion (100).