公开(公告)号：US20160326887A1

公开(公告)日：2016-11-10

申请号：US14707988

申请日：2015-05-08

Applicant: United Technologies Corporation

Inventor： Ryan A. Waite ,  Benjamin F. Hagan

IPC: F01D5/18 ,  F02C7/18 ,  F01D25/12

CPC classification number: F01D5/187 ,  F01D25/12 ,  F02C7/18 ,  F05D2220/32 ,  F05D2230/50 ,  F05D2240/12 ,  F05D2260/202 ,  F05D2260/232 ,  Y02T50/673 ,  Y02T50/676

Abstract: A turbomachine component (e.g., a blade, vane, or any other suitable component) is defined at least partially in a radial direction and an axial direction orthogonal to the radial direction and includes a body defining an outer surface configured to be in thermal communication with a gas path flow in the axial direction. The component includes a thermal regulation channel system defined within the body which includes at least one radial channel configured to allow thermal regulation flow in the radial direction, and at least one axial channel configured to allow thermal regulation flow in the axial direction.

Abstract translation: 涡轮机组件（例如，叶片，叶片或任何其它合适的部件）至少部分地在与径向方向正交的径向方向和轴向方向上限定，并且包括限定外表面的主体，该外表面被配置为与 气路在轴向上流动。 该部件包括限定在主体内的热调节通道系统，该热调节通道系统包括至少一个径向通道，该径向通道构造成允许沿径向进行热调节流动，以及至少一个轴向通道，其构造成允许在轴向上的热调节流动。

公开(公告)号：US10240470B2

公开(公告)日：2019-03-26

申请号：US14911148

申请日：2014-06-30

Applicant: United Technologies Corporation

Inventor： Benjamin F. Hagan ,  Ryan A. Waite ,  Brandon W. Spangler ,  Steven B. Gautschi

IPC: F01D9/06 ,  F01D5/18

Abstract: A vane structure includes an airfoil section with a first inner airfoil wall surface and a second inner airfoil wall surface. A baffle is mounted within the airfoil section between the first inner airfoil wall surface and the second inner airfoil wall surface.

公开(公告)号：US09988912B2

公开(公告)日：2018-06-05

申请号：US14707988

申请日：2015-05-08

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Ryan A. Waite ,  Benjamin F. Hagan

IPC: F01D5/18 ,  F01D25/12 ,  F02C7/18

CPC classification number: F01D5/187 ,  F01D25/12 ,  F02C7/18 ,  F05D2220/32 ,  F05D2230/50 ,  F05D2240/12 ,  F05D2260/202 ,  F05D2260/232 ,  Y02T50/673 ,  Y02T50/676

Abstract: A turbomachine component (e.g., a blade, vane, or any other suitable component) is defined at least partially in a radial direction and an axial direction orthogonal to the radial direction and includes a body defining an outer surface configured to be in thermal communication with a gas path flow in the axial direction. The component includes a thermal regulation channel system defined within the body which includes at least one radial channel configured to allow thermal regulation flow in the radial direction, and at least one axial channel configured to allow thermal regulation flow in the axial direction.

公开(公告)号：US20160186587A1

公开(公告)日：2016-06-30

申请号：US14911148

申请日：2014-06-30

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Benjamin F. Hagan ,  Ryan A. Waite ,  Brandon W. Spangler ,  Steven B. Gautschi

IPC: F01D9/06 ,  F01D5/18

CPC classification number: F01D9/065 ,  F01D5/189 ,  F05D2220/32 ,  F05D2240/126 ,  F05D2250/182 ,  F05D2250/183 ,  F05D2250/184 ,  F05D2260/204 ,  Y02T50/673 ,  Y02T50/676

Abstract: A vane structure includes an airfoil section with a first inner airfoil wall surface and a second inner airfoil wall surface. A baffle is mounted within the airfoil section between the first inner airfoil wall surface and the second inner airfoil wall surface.

Abstract translation: 叶片结构包括具有第一内翼面壁表面和第二内翼面壁表面的翼型段。 挡板安装在第一内翼面壁表面和第二内翼面壁表面之间的翼型部分内。