초록 ▼

Nozzle segments mounting vanes are received in circumferentially extending, generally dovetail-shaped grooves in an outer casing of a steam turbine, the nozzle segments forming part of a stage with rotating buckets of the steam turbine. The inclined slashfaces of the adjoining bases of the nozzle se

Nozzle segments mounting vanes are received in circumferentially extending, generally dovetail-shaped grooves in an outer casing of a steam turbine, the nozzle segments forming part of a stage with rotating buckets of the steam turbine. The inclined slashfaces of the adjoining bases of the nozzle segments are provided with circumferentially opening slots to receive spline seals. The spline seals preclude or minimize steam leakage flow past the gap between the adjoining nozzle segments thereby enhancing the steam flow through the partitions of the nozzles.

대표청구항 ▼

1. In a steam turbine having a rotor, a stationary casing surrounding the rotor and a plurality of circumferentially extending nozzle segments in circumferentially extending grooves about said casing, a method of retrofitting the nozzle segments to provide seals between the opposed endfaces of adjac

1. In a steam turbine having a rotor, a stationary casing surrounding the rotor and a plurality of circumferentially extending nozzle segments in circumferentially extending grooves about said casing, a method of retrofitting the nozzle segments to provide seals between the opposed endfaces of adjacent nozzle segments comprising the steps of:removing the nozzle segments from the steam turbine; forming at least one slot in each endface of the removed nozzle segments; disposing a spline seal in slots of opposed endfaces of the nozzle segments; and inserting the nozzle segments into the grooves of the casing whereby the spline seals extend between adjacent segments for minimizing or precluding steam leakage flows between said adjacent segments. 2. A method according to claim 1 including forming two slots in each end face of the removed nozzle segments, and disposing a spline seal in each slot of the opposite endfaces whereby the two spline seals extend between the adjacent nozzle segments in assembly of the segments in the turbine.3. A method according to claim 2 including forming one of said two slots in the endfaces in a generally axial direction, forming another of said two slots in the endfaces in a generally inclined radial outward downstream direction, and disposing spline seals in said respective slots to minimize or preclude leakage flows in generally radial and axial directions, respectively.