发明名称 Composite retention feature
摘要 A retention feature for use in a gas turbine engine is disclosed herein. The retention feature includes a ceramic post, an insert, and a braze layer coupling the insert to the ceramic post. The ceramic post includes a body adapted to be coupled to a turbine engine component and a head coupled to the body. The insert is arranged in a space formed in the head and the braze layer extends from the ceramic post to the insert to bond the insert to the ceramic post.
申请公布号 US9506356(B2) 申请公布日期 2016.11.29
申请号 US201314094304 申请日期 2013.12.02
申请人 Rolls-Royce North American Technologies, Inc.;Rolls-Royce Corporation 发明人 Loftus Peter;Chamberlain Adam L.;Freeman Ted J.
分类号 F01D5/30;F01D5/04;F01D9/04;G01P15/18;E21B45/00;E21B44/00 主分类号 F01D5/30
代理机构 Barnes & Thornburg LLP 代理人 Barnes & Thornburg LLP
主权项 1. A retention feature for use in a gas turbine engine comprising a ceramic post including a body adapted to be coupled to a turbine engine component and a head coupled to the body, the head formed to include a space that forms a channel opening away from the body and extending through the head of the ceramic post, a first insert arranged in the space, a first braze layer extending from the ceramic post to the first insert to bond the first insert to the ceramic post, a second insert arranged in the space, and a second braze layer extending from the ceramic post to the second insert to bond the second insert to the ceramic post, wherein the second insert is spaced apart from the first insert, wherein the first insert is sized to fill a portion of the channel along an axis of the channel, the second insert is sized to fill another portion of the channel along the axis of the channel, and the second insert is spaced apart from the first portion of the channel along the axis.
地址 Indianapolis IN US