A gas turbine engine assembly (50) adapted to separate a high pressure zone (HP) from a low pressure zone (LP) includes a seal assembly (10) configured to block gasses from passing through the interface of two adjacent components (20, 30). The seal assembly includes a rod (12).
申请公布号
EP3106622(A1)
申请公布日期
2016.12.21
申请号
EP20160168849
申请日期
2016.05.10
申请人
Rolls-Royce Corporation;Rolls-Royce North American Technologies, Inc.;Rolls-Royce High Temperature Composites Inc
发明人
SIPPEL, Aaron;FREEMAN, Ted;THOMAS, David;LAMUSGA, Joseph;SHOEMAKER, Brian
