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公开(公告)号:US20150345331A1
公开(公告)日:2015-12-03
申请号:US14715700
申请日:2015-05-19
Applicant: General Electric Company
Inventor: Robert Carl Murray , Gregory Michael Rowley , Corey Bourassa , Byron Andrew Pritchard , Curtis Walton Stover
CPC classification number: F01D25/24 , F01D25/14 , F02C7/18 , F05D2240/11 , F05D2260/607 , Y02T50/675
Abstract: A shroud assembly for a turbine engine includes a shroud having a front side confronting the blades of a turbine and a back side opposite the front side, a hanger configured to couple the shroud to with casing of the turbine, a cooling conduit extending through the hanger to supply a cooling fluid stream to the back side of the shroud, and a particle separator having a through passage forming part of the cooling conduit and a scavenge conduit branching from the through passage.
Abstract translation: 一种用于涡轮发动机的护罩组件,包括一个护罩,其具有面向涡轮叶片的前侧和与前侧相对的后侧的护罩,构造成将护罩连接到涡轮机外壳的悬挂器,延伸穿过吊架的冷却管道 以将冷却流体流供应到护罩的后侧,以及颗粒分离器,其具有形成冷却管道的一部分的通路和从通道分支的扫气管。