Aerodynamic seal assemblies for turbo-machinery
The present application provides an aerodynamic seal assembly for use with a turbo-machine. The aerodynamic seal assembly may include a number of springs, a shoe connected to the springs, and a secondary seal positioned about the springs and the shoe.
1. An aerodynamic seal assembly positioned between a stationary component and a rotating component of a turbo-machine, comprising:
a plurality of springs coupled to a top piece;
a shoe connected to the plurality of springs; and
a secondary seal coupled to the top piece and positioned about the plurality of springs and the shoe, wherein the secondary seal acts as a spring and as a seal that blocks a fluid flowing between the top piece and the shoe,
wherein a curvature around the rotating component has a mismatch with a curvature of the shoe such that a convergent-divergent or a convergent squeeze fluid film forms between the shoe and the rotating component during rotation of the rotating component to prevent contact of the shoe and the rotating component.
2. The aerodynamic seal assembly of claim 1 , wherein the plurality of springs comprises a plurality of bellows.
3. The aerodynamic seal assembly of claim 1 , wherein the plurality of springs comprises a plurality of folds.
4. The aerodynamic seal assembly of claim 1 , wherein the top piece is attached to the stationary component.
5. The aerodynamic seal assembly of claim 1 , wherein the plurality of springs comprises a first width and the shoe comprises a second width and wherein the first width is less than the second width.
6. The aerodynamic seal assembly of claim 1 , wherein the plurality of springs and the secondary seal comprise a nickel based or a nickel-chrome based alloy.
7. The aerodynamic seal assembly of claim 1 , wherein the secondary seal comprises a plate.
8. The aerodynamic seal assembly of claim 1 , wherein the secondary seal is configured to resist pressure load across said seal assembly.