GAS TURBINE ENGINE INNER CASE WITH NON-INTEGRAL VANES
摘要
A gas turbine engine includes a circumferential array of vanes slidably supported in an inner case shroud segment. Multiple segments are secured to one another to provide an annular engine static structure section. The inner case shroud segment and the vanes have different material properties than one another.
申请公布号
EP3097270(A2)
申请公布日期
2016.11.30
申请号
EP20140879918
申请日期
2014.12.26
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
HAYFORD, RICHARD K.;ROGERS, MARK J.;CARMAN, KENNETH E.;RICHARDSON, CARL S.;EARL, JONATHAN J.
