公开(公告)号：US20160230567A1

公开(公告)日：2016-08-11

申请号：US15022622

申请日：2014-09-12

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Scott W. Gayman ,  Brandon W. Spangler

IPC: F01D5/18

CPC classification number: F01D5/187 ,  F05D2240/81 ,  F05D2250/185

Abstract: A gas turbine engine airfoil includes a platform, and spaced apart walls that provide an exterior airfoil surface that extends radially from the platform to an end opposite the platform. A serpentine cooling passage is arranged between the walls and has a first passageway that extends from the platform toward the end and a second passageway fluidly connecting to the first passageway and extending from the end toward the platform to an end. A platform cooling passageway is fluidly connected to the end and extends transversely into the platform. A cooling hole fluidly connects the platform cooling passageway to an exterior surface.

Abstract translation: 燃气涡轮发动机翼型件包括平台和间隔开的壁，其提供从平台径向延伸到与平台相对的端部的外部翼面表面。 蛇形冷却通道布置在壁之间并且具有从平台朝向端部延伸的第一通道和流体连接到第一通道并从端部朝向平台延伸到端部的第二通道。 平台冷却通道流体地连接到端部并横向延伸到平台中。 冷却孔将平台冷却通道流畅地连接到外表面。

公开(公告)号：US11047241B2

公开(公告)日：2021-06-29

申请号：US15022622

申请日：2014-09-12

Applicant: United Technologies Corporation

Inventor： Scott W. Gayman ,  Brandon W. Spangler

IPC: F01D5/18

Abstract: A gas turbine engine airfoil includes a platform, and spaced apart walls that provide an exterior airfoil surface that extends radially from the platform to an end opposite the platform. A serpentine cooling passage is arranged between the walls and has a first passageway that extends from the platform toward the end and a second passageway fluidly connecting to the first passageway and extending from the end toward the platform to an end. A platform cooling passageway is fluidly connected to the end and extends transversely into the platform. A cooling hole fluidly connects the platform cooling passageway to an exterior surface.