Curved seal with relief cuts for adjacent gas turbine components
A flexible seal is used to seal between two adjacent gas turbine components. The flexible seal includes at least one metal ply having a forward end, an aft end axially separated from the forward end, and an intermediate portion between the forward end and the aft end. The intermediate portion defines a continuous curve in the circumferential direction, such that the aft end is circumferentially, and optionally radially, offset from the forward end. A plurality of relief cuts is defined through the at least one metal ply between the forward end and the aft end to increase flexibility and improve sealing in seal slots that are radially offset from one another.
1. A flexible seal for sealing between two adjacent components of a gas turbine, the flexible seal comprising:
at least one metal ply extending between a forward end and an aft end axially separated from the forward end, the at least one metal ply curving continuously from the forward end to the aft end in a circumferential direction of the gas turbine, such that the aft end is circumferentially offset from the forward end; and
wherein a plurality of relief cuts is defined through the at least one metal ply between the forward end and the aft end.
2. The flexible seal of claim 1 , wherein the seal has an axial length between 5 inches and 50 inches.
3. The flexible seal of claim 2 , wherein the at least one metal ply comprises a plurality of plies joined together at one or more locations along the axial length; and wherein the plurality of relief cuts includes a first set of relief cuts defined through a first ply of the plurality of plies and a second set of relief cuts defined through a second ply of the plurality of plies.
4. The flexible seal of claim 2 , wherein the plurality of relief cuts is distributed uniformly along the axial length.
5. The flexible seal of claim 1 , wherein the at least one metal ply defines one or more inflection points only in a radial direction, when the flexible seal is installed between the two adjacent components of the gas turbine; and wherein the plurality of relief cuts includes a pair of relief cuts at each of the one or more inflection points.
6. The flexible seal of claim 1 , wherein the plurality of relief cuts includes a first set of relief cuts defined from a first edge of the at least one metal ply and a second set of relief cuts defined from a second edge of the at least one metal ply; and wherein a first relief cut of the first set of relief cuts is proximate to a second relief cut of the second set of relief cuts.
7. The flexible seal of claim 1 , wherein at least one relief cut of the plurality of relief cuts extends inwardly from an edge of the at least one metal ply and includes a stress-reducing feature at a terminal end of the relief cut inboard of the edge.
8. The flexible seal of claim 1 , wherein a first relief cut of the plurality of relief cuts is disposed at a first axial location and extends inwardly from a first edge of the at least one metal ply; and wherein a second relief cut of the plurality of relief cuts is disposed at the first axial location and extends inwardly from a second edge of the at least one metal ply opposite the first relief cut.
9. A flexible seal for sealing between two adjacent gas turbine components, the flexible seal comprising:
a forward end and an aft end, wherein the aft end is axially, radially, and circumferentially offset from the forward end;
a first edge and a second edge opposite one another and extending between the forward end and the aft end;
wherein a continuous circumferential curve is defined between the forward end and the aft end;
wherein a plurality of relief cuts is defined through the flexible seal between the forward end and the aft end; and
wherein a first relief cut of the plurality of relief cuts extends from the first edge towards the second edge, and wherein a second relief cut of the plurality of relief cuts extends from the second edge towards the first edge.
10. The flexible seal of claim 9 , wherein the seal has an axial length between 5 inches and 50 inches.
11. The flexible seal of claim 10 , wherein the flexible seal comprises a plurality of plies joined together at one or more locations along the axial length; and wherein the plurality of relief cuts includes a first set of relief cuts defined through a first ply of the plurality of plies and a second set of relief cuts defined through a second ply of the plurality of plies.
12. The flexible seal of claim 10 , wherein the plurality of relief cuts is distributed uniformly along the axial length.
13. The flexible seal of claim 9 , wherein the flexible seal defines one or more inflection points only in the radial direction, when the flexible seal is installed between the two adjacent gas turbine components; and wherein the plurality of relief cuts includes a pair of relief cuts at each of the one or more inflection points.
14. The flexible seal of claim 9 , wherein the plurality of relief cuts includes a first set of relief cuts defined from the first edge of the flexible seal and a second set of relief cuts defined from the second edge of the flexible seal; and wherein the first set of relief cuts and the second set of relief cuts are in an axially alternating arrangement.
15. The flexible seal of claim 9 , wherein at least one relief cut of the plurality of relief cuts extends inwardly from the first edge of the flexible seal and includes a stress-reducing feature at a terminal end of the relief cut inboard of the first edge.
16. The flexible seal of claim 9 , wherein the first relief cut of the plurality of relief cuts is disposed at a first axial location and extends inwardly from the first edge of the flexible seal; and
wherein the second relief cut of the plurality of relief cuts is disposed at the first axial location and extends inwardly from the second edge of the flexible seal opposite the first relief cut.