To provide a sealing assembly for use in a turbomachine.
The turbomachine 100 includes a rotatable element 140. The rotatable element includes an end portion. The end portion defines an outer surface. The turbomachine also includes stationary portions 108/110/114/116 that partially extend circumferentially about the rotatable element such that the stationary portion and the rotatable element at least partially define a rotor shaft cavity therebetween. The end portion of the rotatable element extends through at least a portion of the rotor shaft cavity. The turbomachine further includes at least one sealing assembly that includes sealing elements 130/132 formed across the end portion of the rotatable element. The sealing element defines a plurality of grooves partially extending circumferentially about a portion of the outer surface of the end portion of the rotatable element.
JOHN JOSHY
JP2007303463A | 2007-11-22 | |||
JPH09287667A | 1997-11-04 |
WO1995034745A1 | 1995-12-21 | |||
WO1995034745A1 | 1995-12-21 |
Hirokazu Ogura
Toshihisa Kurokawa
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