公开(公告)号：US20170145860A1

公开(公告)日：2017-05-25

申请号：US14945789

申请日：2015-11-19

Applicant: General Electric Company

Inventor： Jason David Shapiro

IPC: F01D25/28 ,  F01D25/00 ,  F04D29/053 ,  F04D29/52 ,  B29C70/54 ,  F04D29/02 ,  B29C70/34 ,  B29C70/12 ,  B29C53/02 ,  F01D11/08 ,  F04D29/64

CPC classification number: F01D25/28 ,  B29C53/02 ,  B29C53/04 ,  B29C70/12 ,  B29C70/342 ,  B29C70/545 ,  B29K2105/12 ,  B29L2031/7504 ,  F01D11/08 ,  F01D25/005 ,  F01D25/246 ,  F04D29/023 ,  F04D29/545 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2240/11 ,  F05D2260/30 ,  F05D2300/603 ,  F05D2300/6033 ,  Y02T50/672

Abstract: The present disclosure is directed to a component for a gas turbine. The component includes a component wall having a radially inner surface, a radially outer surface, a first circumferential surface, and a second circumferential surface. A first boss extends radially outwardly from the radially outer surface, includes a first circumferentially outer surface, and defines a first aperture extending axially therethrough. A second boss extends radially outwardly from the radially outer surface and is circumferentially spaced apart from the first boss. The second boss includes a second circumferentially outer surface and defines a second aperture extending axially therethrough. The first circumferentially outer surface of the first boss and the second circumferentially outer surface of the second boss form a pair of angles with respect to the radially inner surface.