A gas turbine engine assembly adapted to separate a high pressure zone from a low pressure zone includes a seal assembly configured to block gasses from passing through the interface of two adjacent components. The seal assembly includes a rod.
申请公布号
CA2929244(A1)
申请公布日期
2016.11.28
申请号
CA20162929244
申请日期
2016.05.06
申请人
ROLLS-ROYCE CORPORATION;ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.;ROLLS-ROYCE HIGH TEMPERATURE COMPOSITES, INC.
发明人
SIPPEL, AARON D.;FREEMAN, TED J.;THOMAS, DAVID J.;LAMUSGA, JOSEPH P.;SHOEMAKER, BRIAN J.
