A turbine shroud for a gas turbine engine includes an annular metallic carrier and a ceramic-containing blade track. A connection is formed between the annular metallic carrier and the ceramic-containing blade track by insert pins extending through metallic carrier into the ceramic-containing blade track.
申请公布号
EP3037628(A1)
申请公布日期
2016.06.29
申请号
EP20150200301
申请日期
2015.12.16
申请人
ROLLS-ROYCE CORPORATION;ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.
发明人
SIPPEL, AARON D.;VARNEY, BRUCE E.;FREEMAN, TED J.;WALSTON, JEFFREY A.;SHI, JUN
