FLOW DISCOURAGER FOR VANE SEALING AREA OF A GAS TURBINE ENGINE
摘要
An interface within a gas turbine engine includes a sealing surface defined by a portion of a vane platform. A seal is in contact with said sealing surface. A barrier is transverse to the sealing surface.
申请公布号
WO2014210496(A1)
申请公布日期
2014.12.31
申请号
WO2014US44631
申请日期
2014.06.27
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
OLS, JOHN T.;ALLEN, RICHARD N.;SANCHEZ, PAUL K.;PORTER, STEVEN D.;LEMOINE, JONATHAN
