Curved seal for adjacent gas turbine components
A flexible seal for sealing between two adjacent gas turbine components includes 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 offset from the forward end. In other cases, the forward and aft ends are axially, radially, and circumferentially offset from one another. A method of sealing using the flexible seal includes inserting, in an axial direction, the aft end of the flexible seal into a recess defined by respective seal slots of two adjacent gas turbine components; and pushing the flexible seal in an axial direction through the recess until the forward end is disposed within the recess.
1. A flexible seal for sealing between two adjacent gas turbine components, the flexible seal comprising:
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 defining a continuous curve in the circumferential direction, such that the aft end is circumferentially offset from the forward end; and
a first set of plies and a second set of plies joined at one or more axial locations over the forward end and the intermediate portion to the second set of plies, an aft end of the first set of plies being separated from an aft end of the second set of plies to form a bi-furcated aft end of the seal; and
wherein the seal has an axial length of between 2 inches and 50 inches.
2. The flexible seal of claim 1 , wherein the intermediate portion defines one or more inflection points only in the radial direction, when the seal is installed between the two adjacent gas turbine components.
3. The flexible seal of claim 1 , further comprising an anchor disposed at the forward end of the seal, wherein the anchor defines a through-hole or an indentation configured to facilitate removal of the seal.
4. A flexible seal for sealing between two adjacent gas turbine components, the seal comprising:
a forward end, an aft end, and a plurality of plies joined together at one or more locations along an axial length of the seal, the axial length being between 2 inches and 50 inches;
wherein the aft end is axially, radially, and circumferentially offset from the forward end;
wherein a continuous circumferential curve is defined between the forward end and the aft end; and
wherein the plurality of plies includes a first set of plies and a second set of plies; and wherein an aft end of the first set of plies is separated from an aft end of the second set of plies to form a bi-furcated aft end of the seal.
5. The flexible seal of claim 4 , wherein the intermediate portion is between the forward end and the aft end, and wherein the intermediate portion of the seal defines the continuous circumferential curve.
6. The flexible seal of claim 5 , wherein the intermediate portion of the seal defines one or more inflection points only in the radial direction, when the seal is installed between the two adjacent gas turbine components.
7. The flexible seal of claim 4 , further comprising an anchor disposed at the forward end of the seal, wherein the anchor defines a through-hole or an indentation configured to facilitate removal of the seal.
8. The flexible seal of claim 4 , wherein the seal has a width, the width varying along the axial length of the seal.
9. A flexible seal for sealing between two adjacent gas turbine components, the seal comprising:
a forward end and an aft end axially separated from the forward end;
an intermediate portion between the forward end and the aft end, the intermediate portion defining a continuous curve in the circumferential direction, such that the aft end is axially, radially, and circumferentially offset from the forward end,
wherein the flexible seal has an axial length,
wherein the flexible seal comprises a plurality of plies joined together at one or more locations along the axial length, wherein the plurality of plies includes a first set of plies and a second set of plies, the first set of plies being joined over the forward end and the intermediate portion to the second set of plies; and wherein an aft end of the first set of plies is separated from an aft end of the second set of plies to form a bi-furcated aft end of the flexible seal.
10. The flexible seal of claim 9 , wherein the intermediate portion defines one or more inflection points only in the radial direction, when the seal is installed between the two adjacent gas turbine components.
11. The flexible seal of claim 9 , wherein the axial length of the flexible seal is between 2 inches and 50 inches.
12. The flexible seal of claim 9 , further comprising an anchor disposed at the forward end of the seal, wherein the anchor defines a through-hole or an indentation configured to facilitate removal of the seal.
13. The flexible seal of claim 9 , wherein the flexible seal has a width, the width varying along the axial length of the seal.