发明名称 |
Turbine shroud segment with inter-segment overlap |
摘要 |
A turbine shroud has a plurality of shroud segments disposed circumferentially one adjacent to another. Each segment has a flow restrictor projecting integrally from one end face thereof and overlapping a corresponding end face of a circumferentially adjacent segment. The overlap between the circumferentially adjacent segments restricts gas leakage through the inter-segment gap between adjacent shroud segments. |
申请公布号 |
US9079245(B2) |
申请公布日期 |
2015.07.14 |
申请号 |
US201113222028 |
申请日期 |
2011.08.31 |
申请人 |
Pratt & Whitney Canada Corp. |
发明人 |
Durocher Eric;Lefebvre Guy |
分类号 |
B22F5/00;F01D11/00;F01D9/02;F01D11/08;C22C19/03;C22C19/07;B22F7/06;B22F3/22 |
主分类号 |
B22F5/00 |
代理机构 |
Norton Rose Fulbright Canada LLP |
代理人 |
Norton Rose Fulbright Canada LLP |
主权项 |
1. A turbine shroud assembly of a gas turbine engine, comprising a plurality of shroud segments disposed circumferentially one adjacent to another, wherein circumferentially adjacent shroud segments have confronting sides defining an inter-segment gap therebetween, and wherein a flow restrictor integrally projects from a first one of said confronting sides of a first shroud segment through the inter-segment gap and into overlapping relationship with a cooperating joint surface provided at a second one of said confronting sides of an adjacent second shroud segment, said flow restrictor and said joint surface defining a clearance therebetween configured to accommodate thermal expansion during hot operating conditions, said clearance and said inter-segment gap being configured to cooperatively define a tortuous leakage path in a generally radial direction between said first and second shroud segments at said hot operating conditions, wherein each of the shroud segments has a shroud body including forward and aft hooks extending from a radially outer surface of a platform having an opposite radially inner hot gas path side surface, and wherein the flow restrictor has a generally axially extending portion integrally projecting from the platform and a generally radially extending portion integrally projecting from at least one of the forward and aft hooks, wherein each of the shroud segments has a metal injection molded (MIM) shroud body, and wherein said flow restrictor forms part of said MIM shroud body. |
地址 |
Longueil, Quebec CA |