发明名称 RADIAL SEAL WITH OFFSET RELIEF CUT
摘要 A seal assembly for a turbine engine is disclosed and includes a fixed housing including an axial surface defining an inner diameter and an annular seal that is disposed within the housing and seal against a radial surface of the fixed housing. The annular seal includes a first surface transverse to an axis of rotation and a second surface parallel to the axis of rotation defining an inner periphery. The first surface includes a first notch spaced apart from the inner periphery and overlapping the inner diameter of the fixed housing.
申请公布号 EP3063379(A1) 申请公布日期 2016.09.07
申请号 EP20140858952 申请日期 2014.10.17
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MILLER, JONATHAN LOGAN
分类号 F01D11/00;F16J15/16 主分类号 F01D11/00
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