发明名称 Machine cavity seal
摘要 There is disclosed a seal assembly (32) for a machine such as a gas turbine engine. The seal assembly has a support structure (38) to which a resiliently deformable seal member (34) is mounted. A seal land (40) is opposingly spaced from the support structure (38) to define a gap therebetween, wherein the height of the seal member (34) in an undeformed condition is greater than the height (36) of the gap such that the seal member is deformingly pressed against the seal land (40) by the support structure to seal the gap therebetween in use. The support structure (38) and/or seal land (40) comprise an actuable member (40; 44; 46), said member being actuable in a direction towards the other of the support structure and seal land to improve the resistance of the seal assembly (32) to an adverse condition in use, such as a fire.
申请公布号 US9382808(B2) 申请公布日期 2016.07.05
申请号 US201514604220 申请日期 2015.01.23
申请人 ROLLS-ROYCE plc 发明人 Hodgkinson Carl
分类号 F16J15/16;F01D11/00;F16J15/08 主分类号 F16J15/16
代理机构 Oliff PLC 代理人 Oliff PLC
主权项 1. A seal assembly comprising: a support structure to which a resiliently deformable seal member is mounted; and a seal land opposingly spaced from the support structure to define a gap therebetween, the height of the seal member in an undeformed condition being greater than the height of the gap such that the seal member is deformingly pressed against the seal land by the support structure to seal the gap therebetween, wherein the support structure and/or seal land comprise an actuable member that comprises a shape memory material, said actuable member being actuable in response to an adverse condition so as to move in a direction towards the other of the support structure and seal land to improve the resistance of the seal assembly to the adverse condition.
地址 London GB