<p>A turbine shroud for a gas turbine engine includes an annular metallic carrier, a blade track, and a cross-key connection formed between the annular metallic carrier and the ceramic blade track. The cross-key connection is formed between the annular metallic carrier and inserts included in the blade track. The inserts are bonded to an annular runner also included in the blade track by a braze layer.</p>
申请公布号
WO2014143230(A1)
申请公布日期
2014.09.18
申请号
WO2013US72767
申请日期
2013.12.03
申请人
LANDWEHR, SEAN E.;WESTPHAL, WILLIAM;FREEMAN, TED J.;CHAMBERLAIN, ADAM L.
发明人
LANDWEHR, SEAN E.;WESTPHAL, WILLIAM;FREEMAN, TED J.;CHAMBERLAIN, ADAM L.