MAXMET COMPOSITES FOR TURBINE ENGINE COMPONENT TIPS
摘要
A turbine engine system includes a turbine engine component having an airfoil portion and a tip, which turbine engine component having a MAXMET composite bonded to the tip. The MAXMET composite has MAX phases in a metal matrix.
申请公布号
WO2014149097(A2)
申请公布日期
2014.09.25
申请号
WO2013US75292
申请日期
2013.12.16
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
AMINI, SHAHRAM;STROCK, CHRISTOPHER W.;BURLATSKY, SERGEI F;NOVIKOV, DMITRI;FURRER, DAVID ULRICH
