A foil thrust bearing forms the primary rotating interface for a film riding face seal. This face seal includes a spring system that will allow the entire assembly to translate axially relative to a static attachment. The complete assembly will form a hybrid foil/film riding face seal that shows much promise at being sufficiently flexible to enable operation in a gas turbine engine. The seal includes a flexible top plate having a non-flat surface under its working conditions, and a spring support system to allow the top plate to accommodate axial excursions and out-of-flat distortions.
申请公布号
WO03004911(A2)
申请公布日期
2003.01.16
申请号
WO2002US21191
申请日期
2002.07.03
申请人
R & D DYNAMICS CORPORATION;AGRAWAL, GIRIDHARI, L.;PATEL, KIRTIKUMAR, H.;MUNSON, JOHN, H.
发明人
AGRAWAL, GIRIDHARI, L.;PATEL, KIRTIKUMAR, H.;MUNSON, JOHN, H.