公开(公告)号：US10316974B2

公开(公告)日：2019-06-11

申请号：US15681829

申请日：2017-08-21

Applicant: ROLLS-ROYCE plc

Inventor： Helen Webster ,  Luke Hamilton ,  Murad Khader ,  Robert Grasse

IPC: F16J15/40 ,  F01D11/04 ,  F16J15/16 ,  F01D25/22

Abstract: Air-riding seal arrangement between two components are rotatable relative to each other about a rotation axis. The seal arrangement includes an axially slidable carrier module mounted to one component and runner provided by other components. The carrier module and runner have respective and opposing annular sealing faces in a seal arrangement normal operation are axially spaced to form an air-seal therebetween separating a high-pressure region at one side of the air-seal from low-pressure region at the other side. The carrier module has a front and rear portions, and carrier module sealing face is provided by the front portion. The front portion has first and second rotation positions relative to the rear portion, the first rotation position being in normal operation, and second rotation position being in event of high speed touchdown of the annular sealing faces when contact between sealing faces rotates the front portion to the second rotation position.