Shroud assembly for turbine engine

1. A shroud assembly for a turbine engine having a compressor, a combustor, and a turbine within a casing, with the turbine having a plurality of annularly-arranged fixed vanes defining nozzles therebetween and a plurality of annularly-arranged rotating blades paired with the fixed vanes to define one stage of the turbine, the shroud assembly comprising:

a shroud having a front side confronting the blades and a back side opposite the front side:

a hanger configured to couple the shroud with the casing:

a cooling conduit extending through at least a portion of the hanger to supply a cooling fluid stream to the back side of the shroud; and

at least one particle separator having a through passage forming part of the cooling conduit and a scavenge conduit branching from the through passage;

wherein the at least one particle separator separates particles from the cooling fluid stream in the form of a concentrated-particle stream containing the separated particles, which is directed along the scavenge conduit, and the remaining cooling fluid stream forms a reduced-particle stream, which is passed along the cooling conduit to the back side of the shroud;

wherein the at least one particle separator comprises at least one centrifugal separator; and

wherein the at least one centrifugal separator comprises an angular velocity decreaser located within through passage, downstream of the angular velocity increaser.

2. The shroud assembly of claim 1 wherein the scavenge conduit comprises a scavenge conduit inlet located downstream of the angular velocity increaser and upstream of the angular velocity decreaser.

3. The shroud assembly of claim 1 wherein the at least one particle separator comprises at least one inertial separator having a turn in the through passage defining an outer wall of the through passage, and the scavenge conduit has an inlet at the outer wall, with the turn being shaped to change the direction of the cooling fluid stream such that particles entrained in the cooling fluid stream are carried by their inertia against the outer wall where they enter the scavenge conduit along with a portion of the cooling fluid stream to form the concentrated-particle stream.

4. The shroud assembly of claim 3 wherein the turn changes the direction of the cooling fluid stream at least 90 degrees.

5. The shroud assembly of claim 4 wherein the turn changes the direction of the cooling fluid stream at least 180 degrees.

6. The shroud assembly of claim 3 wherein the turbine engine defines a centerline, about which the blades rotate, and the turn has an inlet and an outlet, which are radially offset from each other relative to the centerline.

7. A shroud assembly for a turbine engine having a compressor, a combustor, and a turbine within a casing, with the turbine having a plurality of annularly-arranged fixed vanes defining nozzles therebetween and a plurality of annularly-arranged rotating blades paired with the fixed vanes to define one stage of the turbine, the shroud assembly comprising:

a shroud having a front side confronting the blades and a back side opposite the front side;

a hanger configured to couple the shroud with the casing;

a cooling conduit extending through at least a portion of the hanger to supply a cooling fluid stream to the back side of the shroud; and

at least one particle serparator having through passage forming part of the cooling conduit and a scavenge conduit branching from the through passage;

wherein the at least one particle separator separates particles from the cooling fluid stream in the form of a concentrated-particle stream containing the separated particles, which is directed along the scavenge conduit, and the remaining cooling fluid stream forms a reduced-particle stream, which is passed along the cooling conduit to the back side of the shroud;

wherein the at least one particle separator comprises at least one inertial separator having a turn in the through passage defining an outer wall of the through passage, and the scavenge conduit has an inlet at the outer wall, with the turn being shaped to change the direction of the cooling fluid stream such that particles entrained in the cooling fluid stream are carried by their inertia against the outer wall where they enter the scavenge conduit along with a portion of the cooling fluid stream to form the concentrated-particle stream; and

wherein the scavenge conduit has a scavenge outlet between the hanger and the plurality of annularly-arranged fixed vanes.

8. The shroud assembly of claim 7 wherein the scavenge outlet is fluidly coupled downstream of the plurality of annularly-arranged rotating blades.

9. A shroud assembly for a turbine engine having a compressor, a combustor, and a turbine within a casing, with the turbine having a plurality of annularly-arranged fixed vanes defining nozzles therebetween and a plurality of annularly-arranged rotating blades paired with the fixed vanes to define one stage of the turbine, the shroud assembly comprising:

a shroud having a front side confronting the blades and a back side opposite the front side;

a hanger configured to couple the shroud with the casing;

a cooling conduit extending through at least a portion of the hanger to supply a cooling fluid stream to the back side of the shroud; and

at least one particle separator having a through passage forming part of the cooling conduit and a scavenge conduit branching from the through passage;

wherein the at least one particle separator separates particles from the cooling fluid stream in the form of a concentrated-particle stream containing the separated particles, which is directed along the scavenge conduit, and the remaining cooling fluid stream forms a reduced-particle stream, which is passed along the cooling conduit to the back side of the shroud; and

wherein the scavenge conduit has a scavenge outlet between the hanger and the plurality of annularly-arranged fixed vanes.

10. The shroud assembly of claim 9 wherein the scavenge outlet is fluidly coupled downstream of the plurality of annularly-arranged rotating blades.

11. A shroud assembly for a turbine engine having a compressor, a combustor, and a turbine within a casing, with the turbine having a plurality of annularly-arranged fixed vanes defining nozzles therebetween and a plurality of annularly-arranged rotating blades paired with the fixed vanes to define one stage of the turbine, the shroud assembly comprising:

a shroud having a front side confronting the blades and a back side opposite the front side;

a hanger configured to couple the shroud with the casing;

a cooling conduit extending through at least a portion of the hanger to supply a cooling fluid stream to the back side of the shroud; and

at least one particle separator having a through passage forming part of the cooling conduit and a scavenge conduit branching from the through passage;

wherein the at least one particle separator separates particles from the cooling fluid stream in the form of a concentrated-particle stream containing the separated particles, which is directed along the scavenge conduit, and the remaining cooling fluid stream forms a reduced-particle stream, which is passed along the cooling conduit to the back side of the shroud;

wherein the at least one particle separator comprises at least one inertial separator having a turn in the through passage defining an outer wall of the through passage, with the turn being shaped to change the direction of the cooling fluid stream such that particles entrained in the cooling fluid stream are carried by their inertia against the outer wall; and

wherein the turbine engine defines a centerline, about which the blades rotate, and the turn has an inlet and an outlet, which are radially offset from each other relative to the centerline;

wherein the at least one particle separator comprises at least one centrifugal separator; and

wherein the at least one centrifugal separator comprises on angular velocity decreaser located within through passage, downstream of the angular velocity increaser.

12. The shroud assembly of claim 11 wherein the scavenge conduit comprises a scavenge conduit inlet located downstream of the angular velocity increaser and upstream of the angular velocity decreaser.

13. The shroud assembly of claim 11 wherein the turn changes the direction of the cooling fluid stream at least 90 degrees.

14. The shroud assembly of claim 13 wherein the turn changes the direction of the cooling fluid stream at least 180 degrees.