Patent ID: 9057279
Filing Date: 2015-06-16
Classification: F01D,F16J

Abstract:
1. A labyrinth seal arranged to impede leakage flow though a gap between confronting surfaces of static and moving parts in an axial fluid flow turbomachine, the labyrinth seal comprising: a plurality of axially spaced and circumferentially extending sealing fins arranged in leakage flow series, the fins projecting across the gap from at least one of the confronting parts towards an opposing confronting part such that distal ends of the fins are in sealing proximity to the opposing confronting part; a plurality of chambers defined by successive fins in leakage flow series; each fin having an upstream-facing surface of which at least a distal portion thereof is inclined towards the upstream direction of the leakage flow to form a vortex-producing flow recirculation surface operative to deflect the leakage flow in the upstream direction and create recirculating vortices in the leakage flow within the chambers defined by successive fins, wherein one of the confronting surfaces of the static and moving parts is castellated and comprises at least one land and at least one relatively recessed portion, each land and each recessed portion being in sealing proximity to the distal end of a sealing fin and wherein successive sealing fins alternately comprise at least one first fin having a straight upstream-facing surface inclined towards the upstream direction and at least one second fin having an upstream-facing surface of which at least the distal portion is inclined towards the upstream direction, the distal end of each first fin being in sealing proximity to a land and the distal end of each second fin being in sealing proximity to a recessed portion, wherein the upstream-facing surface of the at least one second fin is variably curved concavely over its whole length, a maximum concavity being at its distal end.