FILM RIDING SEAL FOR TURBINES
An seal is described for a turbine with a first sealing surface mounted on a stationary part of a turbine and a second sealing surface mounted on a rotating part of the turbine, the surfaces being structured such that in operation the thin film of a fluid medium is generated between the two surfaces reducing contact and/or leakage with at least one of the first or second sealing surface mounted such that it is subject to a retracting force which opens the seal while stationary or at slow rotation speeds of the turbine and subject to a force counteracting the retracting force at operational rotation speeds of the turbine. The surface of the sealing face may incorporate patterns straight or helical in nature to help induce the fluid into the gap and maintain the fluid film.
1 . A turbine seal comprising a first sealing surface mounted on a stationary part of a turbine and a second sealing surface mounted on a rotating part of the turbine, the surfaces being structured such that in operation a thin film of a fluid medium is generated between the two surfaces reducing contact and/or leakage with at least one of the first or second sealing surface mounted such that at least one of the first or second sealing surface is subject to a retracting force which opens the seal while stationary or at slow rotation speeds of the turbine and subject to a force counteracting the retracting force at operational rotation speeds of the turbine.
2 . The seal of claim 1 , wherein one of the sealing surfaces is connected to a fluid feed line providing pressurized fluid into a space behind at least one of the sealing surfaces such that the pressure of the fluid contributes to the force counteracting the retracting force at operational rotation speeds of the turbine.
3 . The seal of claim 1 , wherein the sealing surfaces are essentially perpendicular to the main axis of the turbine.
4 . The seal of claim 2 , wherein the fluid feed line comprises a bore through a shroud connecting the space behind at least one of the sealing surfaces to fluid at an upstream pressure.
5 . The seal of claim 2 , wherein the fluid feed line comprises a bore through the stationary part of a turbine connecting the space behind at least one of the sealing surfaces to fluid at an upstream pressure.
6 . The seal of claim 2 , wherein the fluid feed line comprises a circumferential channel equalizing the pressure along the space behind at least one of the sealing surfaces.
7 . The seal of claim 1 , wherein at least one of the sealing surfaces is mounted onto a seal pad directly or indirectly connected to an elastic element to provide the retracting force acting to disengage the two surfaces of the seal.
8 . The seal of claim 1 , wherein the sealing surfaces are mounted at a shrouded tip of turbine blades and the adjacent static parts of the turbine.
9 . The seal of claim 8 , wherein two pairs of first and second sealing surfaces are oriented essentially perpendicular to the main axis of the turbine the shrouded tip of turbine blades running between the pair.
10 . The seal of claim 1 , wherein the first sealing surface mounted on a stationary part of a turbine is mounted on a carrier element, which in turn has sufficient clearance to allow for thermal expansion of the casing without dislocating the seal.
11 . The seal of claim 1 , further comprising seals placed at a tip of rotating turbine blades to seal the passage of fluid around the tip from an upstream side to a downstream side of the blades.
12 . The seal of claim 1 , wherein the sealing surfaces are essentially perpendicular to the radial direction.
13 . The seal of claim 12 , wherein the sealing surfaces are mounted onto a radial extension of a shroud or of a tip of rotating turbine blades.
14 . The seal of claim 1 , wherein at least one of the sealing surfaces is patterned to facilitate the generation of the fluid film between the surfaces.