TURBINE ENGINE VANE ARRANGEMENT HAVING A PLURALITY OF INTERCONNECTED VANE ARRANGEMENT SEGMENTS
摘要
A turbine engine vane arrangement and a method for manufacturing a turbine engine vane arrangement are provided. The vane arrangement includes a plurality of vane arrangement segments arranged circumferentially around an axial centerline. Each of the vane arrangement segments includes an airfoil that extends radially between a first platform segment and a second platform segment. The first platform segment extends circumferentially between a first mate face and a second mate face. The first mate face of a first of the vane arrangement segments is bonded to the second mate face of a second of the vane arrangement segments.
申请公布号
EP2901022(A4)
申请公布日期
2016.05.04
申请号
EP20130841332
申请日期
2013.01.09
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
FARAH, JORGE, I.;BURT, JONATHAN, P.;STEWART, DANA, P.