公开(公告)号：US20160177738A1

公开(公告)日：2016-06-23

申请号：US14831997

申请日：2015-08-21

Applicant: United Technologies Corporation

Inventor： Sasha M. Moore ,  Clifford J. Musto ,  Timothy J. Jennings ,  Thomas N. Slavens ,  San Quach ,  Nicholas M LoRicco ,  John McBrien ,  Carey Clum ,  Christopher Whitfield

IPC: F01D5/18 ,  F01D11/08 ,  F01D25/12 ,  F02C7/18 ,  F04D29/54 ,  F04D29/58 ,  F02C3/04 ,  F01D9/04 ,  F04D29/32

Abstract: A gas turbine engine component includes a wall that provides an exterior surface and an interior flow path surface. The wall has a wall thickness. A protrusion is arranged on the wall that extends a height beyond the wall thickness and provides a portion of the interior flow path surface. A film cooling hole that has an inlet is provided on the protrusion and extends to an exit on the exterior surface.

Abstract translation: 燃气涡轮发动机部件包括提供外表面和内部流路表面的壁。 墙壁有壁厚。 突出部设置在壁上，其高度超过壁厚，并提供内部流路表面的一部分。 具有入口的薄膜冷却孔设置在突起上并延伸到外表面上的出口。