초록 ▼

Arcuate seal layers conforming with one another are disposed between inner retainer segments and inner rails of nozzle segments of a gas turbine. The layers are secured to the aft axial face of the segments and project radially outwardly to seal against the forward axial faces of the rails. The rear

Arcuate seal layers conforming with one another are disposed between inner retainer segments and inner rails of nozzle segments of a gas turbine. The layers are secured to the aft axial face of the segments and project radially outwardly to seal against the forward axial faces of the rails. The rear axial faces of the rails have chordal seals for sealing against the forward axial faces of the support rings. The seal layers have radial cuts misaligned with one another in an axial direction to preclude leakage flows through gaps formed by the cuts. Arcuate spacers are staggered circumferentially with the arcuate retainer segments whereby an intermediate pressure plenum is formed between the finger seals and chordal seals.

대표청구항 ▼

What is claimed is: 1. A turbine comprising: a turbine nozzle segment having at least one stator vane and including an inner platform rail; a turbine nozzle inner support ring in part in axial registration with said rail on one side thereof; an inner retainer segment secured to said inner support r

What is claimed is: 1. A turbine comprising: a turbine nozzle segment having at least one stator vane and including an inner platform rail; a turbine nozzle inner support ring in part in axial registration with said rail on one side thereof; an inner retainer segment secured to said inner support ring and in part in axially spaced registration relative to said rail on an axial side of said rail opposite from said support ring; and a seal assembly extending between said inner retainer segment and said rail, said seal assembly including a plurality of seal fingers secured to said inner retainer segment and in engagement with said rail, said seal assembly including first and second sets of circumferentially adjacent seal fingers overlying one another, said first set of seal fingers having at least one gap between circumferentially adjacent fingers thereof and said second set of seal fingers having at least one gap between circumferentially adjacent fingers thereof, said first and second sets of seal fingers being staggered in a circumferential direction relative to one another with a finger of said first set of fingers overlying the one gap between the circumferentially adjacent fingers of said second set thereof. 2. A turbine according to claim 1 wherein said seal fingers are biased into engagement with said rail. 3. A turbine according to claim 1 wherein said seal fingers have a common base secured to said inner retainer segment. 4. A turbine according to claim 1 wherein said first and second sets of fingers each have a common base secured to said inner retainer segment with the fingers thereof projecting from said bases generally radially outwardly and with one set of fingers engaging said rail. 5. A turbine according to claim 4 wherein said rail and said inner support ring include a chordal seal therebetween, an inner retainer spacer between said ring and said inner retainer segment, said seal fingers between said inner retainer segment and said rail, said chordal seal and said spacer defining an intermediate pressure plenum therebetween. 6. A turbine comprising: a plurality of nozzle segments arranged about a turbine axis with each segment having at least one stator vane and an inner platform carrying an inner platform rail; inner nozzle support rings in part in spaced axial registration with said rails and on one axial side of said rails; a plurality of inner retainer segments secured to said inner supporting rings and in part in axial spaced registration relative to said rails on an axial side of said rails from said support rings; and a seal assembly between said inner retainer segments and said rails, said seal assembly including a plurality of circumferentially spaced inner retainer seals each including a plurality of circumferentially spaced seal fingers for sealing engagement with said rails, each said retainer seal including first and second sets of circumferentially adjacent seal fingers overlying one another and secured to each of said inner retainer segments, said first and second sets of fingers of each inner retainer seal having at least one gap between circumferentially adjacent fingers and said second set of seal fingers having at least one gap between circumferentially adjacent fingers thereof, said first and second sets of seal fingers being staggered in a circumferential direction relative to one another with a finger of said first set of fingers overlying the one gap between the circumferentially adjacent fingers of said second set thereof. 7. A turbine according to claim 6 wherein said first and second sets of fingers each have a common base secured to said inner retainer segment with the fingers thereof projecting from said bases generally radially outwardly and with one set thereof engaging said rails. 8. A turbine according to claim 7 including a plurality of inner retainer spacers between said rings and said inner retainer segments, said spacers being equal in number to the number of said inner retainer segments with end gaps between circumferentially adjacent end faces of the inner retainer spacers being misaligned with end gaps between said inner retainer segments. 9. A turbine according to claim 8 including a seal between the end faces of circumferentially adjacent inner retainer spacers. 10. A turbine according to claim 8 including chordal seals between said rails and said support rings, said seal assembly, said chordal seals, said spacers, said inner retainer ring segments and said rails defining an intermediate pressure plenum between said chordal seals and said seal assembly. 11. A method of installing a seal assembly in a turbine having a plurality of nozzle segments arranged about a turbine axis with each segment having at least one stator vane and an inner platform carrying an inner platform rail and inner nozzle support rings in part in spaced axial registration with said rails and on one axial side of said rails for sealing between high and low pressure regions on opposite sides of said rails, comprising the steps of: providing a plurality of inner retainer segments secured to said inner supporting rings and in part in axial spaced registration relative to said rails on an axial side of said rails opposite from said support rings; securing a plurality of circumferentially spaced inner retainer seals each including a plurality of circumferentially spaced seal fingers to said inner retainer segments; securing said inner retainer segments with said seals secured thereto to said support rings with said seals extending from said segments into sealing engagement with said rails on said axially opposite sides thereof from said support rings; providing first and second overlapping sets of said inner retainer seals with each set of seals having at least one gap between circumferentially adjacent fingers thereof, and staggering said first; and second sets of seals in a circumferential direction relative to one another enabling a finger of said first set of seals to overlie a gap between adjacent fingers of said second set of seals. 12. A method according to claim 11 wherein said first and second sets of seals each have a common base, and including securing said common bases to said inner retainer segments with said seal fingers thereof projecting into biased engagement with said rails. 13. A method according to claim 11 wherein at least a pair of said first sets of seals have seal fingers extending beyond end faces of a corresponding pair of inner retainer segments and securing said pair of said segments to said support rings and subsequently securing remaining segments to said support rings with portions thereof overlapping said extending seal fingers of said first set of seals.