Ring segment and turbomachine including same
A ring segment and a turbomachine including the ring segment are provided. The ring segment installed on an inner circumferential surface of a casing and disposed to face an end of a blade disposed inside the casing, the ring segment includes a segment body disposed inside the casing in a radial direction of the casing and including a plurality of cooling channels through which cooling air flows, a pair of segment protrusions protruding outward from the segment body, coupled to the inner circumferential surface of the casing, and spaced apart from each other in a flow direction of fluid flowing through the casing to form an RS cavity into which cooling air is introduced, wherein when the segment body has a cross section along an imaginary plane including a radial straight line of the casing, the cooling channel is formed such that a width in a direction perpendicular to a radial direction of the casing is greater than a width in the radial direction of the casing.
1. A ring segment installed on an inner circumferential surface of a casing and disposed to face an end of a blade disposed inside the casing, the ring segment comprising:
a segment body disposed inside the casing in a radial direction of the casing and including a plurality of cooling channels through which cooling air flows; and
a pair of segment protrusions protruding outward from the segment body, coupled to the inner circumferential surface of the casing, and spaced apart from each other in a flow direction of fluid flowing through the casing to form an RS cavity through which cooling air flows,
wherein when the segment body has a cross section along an imaginary plane including a radial straight line of the casing, the cooling channel is formed such that a width in a direction perpendicular to a radial direction of the casing is greater than a width in the radial direction of the casing.
2. The ring segment according to claim 1 , wherein the plurality of cooling channels comprise:
a plurality of first cooling channels passing through a downstream end of the segment body in the flow direction of the fluid flowing through the casing, extending upstream from the downstream end of the segment body, and extending in a reverse direction downstream from an upstream side of the segment body; and
a plurality of second cooling channels alternately disposed with the plurality of first cooling channels, passing through an upstream end of the segment body in the flow direction of the fluid flowing through the casing, extending downstream from the upstream end of the segment body, and extending in a reverse direction upstream from a downstream side of the segment body.
3. The ring segment according to claim 1 , wherein the cooling channel is formed to extend along the flow direction of the fluid flowing through the casing and includes a plurality of curved portions bent in circumferential direction of the casing.
4. The ring segment according to claim 3 , wherein the plurality of curved portions comprise a plurality of first bent portions bent in a first circumferential direction of the circumferential directions of the casing and a plurality of second bent portions alternately arranged with the plurality of first bent portions and bent in a second circumferential direction different from the first circumferential direction.
5. The ring segment according to claim 3 , wherein the cooling channel includes a U-shaped return portion in which a fluid changes a flow direction thereof so that the fluid flows to a second curved portion of the plurality of curved portions from a first curved portion of the plurality of curved portions, and
wherein the first curved portion and the second curved portion are adjacent to each other in the circumferential direction.
6. The ring segment according to claim 3 , wherein the cooling channel comprises:
an inlet connected to one of the curved portions to receive cooling air from the RS cavity and through which the received cooling air flows into the plurality of curved portions; and
an outlet connected to one of the curved portions to communicate with outside of the segment body and through which the cooling air flowing through the plurality of curved portions is discharged downstream or upstream in the flow direction of the fluid flowing through the casing.
7. The ring segment according to claim 3 , wherein in a cross-section of the segment body when viewed along the circumferential direction of the casing, the curved portion is formed such that a width W D in the flow direction of the fluid flowing through the casing is greater than a width W R in the radial direction of the casing.
8. The ring segment according to claim 3 , wherein in a cross-section of the segment body when viewed along the flow direction of the fluid flowing through the casing, the curved portion is formed such that a width W C in the circumferential direction of the casing is greater than a width W R in the radial direction of the casing.
9. The ring segment according to claim 2 , wherein each of the first cooling channel and the second cooling channel includes an inlet through which the cooling air introduced into the RS cavity is supplied, and
the inlet of the first cooling channel and the inlet of the second cooling channel are disposed adjacent to each other in the flow direction of the fluid flowing through the casing.
10. The ring segment according to claim 2 , wherein the segment body is disposed outside the plurality of cooling channels in the radial direction and includes a cooling cavity into which the cooling air is introduced from the RS cavity and through which the cooling air is supplied to the plurality of cooling channels, and
the cooling cavity is divided into a first cooling cavity communicating with the first cooling channel and a second cooling cavity communicating with the second cooling channel by a partition wall installed therein.
11. A turbo machine comprising:
a stator comprising a casing through which fluid passes, a vane coupled to an inner circumferential surface of the casing to guide the fluid, and a ring segment installed on the inner circumferential surface of the casing and disposed between vanes adjacent to each other in a flow direction of the fluid; and
a rotor comprising a disk installed inside the stator and a blade coupled to an outer circumferential surface of the disk and rotated by the fluid,
wherein the ring segment comprises:
a segment body disposed inside the casing in a radial direction of the casing and having a plurality of channels through which cooling air flows;
a pair of segment protrusions protruding outward from the segment body, coupled to the inner circumferential surface of the casing, and spaced from each other in a flow direction of the fluid flowing through the casing to form an RS cavity into which the cooling air is introduced, and
wherein when the segment body has a cross section along an imaginary plane including a radial straight line of the casing, the cooling channel is formed such that a width in a direction perpendicular to a radial direction of the casing is greater than a width in the radial direction of the casing.
12. The turbo machine according to claim 11 , wherein the plurality of cooling channels comprise:
a plurality of first cooling channels passing through a downstream end of the segment body in the flow direction of the fluid flowing through the casing, extending upstream from the downstream end of the segment body, and extending in a reverse direction downstream from an upstream side of the segment body; and
a plurality of second cooling channels alternately disposed with the plurality of first cooling channels, passing through an upstream end of the segment body in the flow direction of the fluid flowing through the casing, extending downstream from the upstream end of the segment body, and extending in a reverse direction upstream from a downstream side of the segment body.
13. The turbo machine according to claim 11 , wherein the cooling channel is formed to extend along the flow direction of the fluid flowing through the casing and includes a plurality of curved portions bent in circumferential direction of the casing.
14. The turbo machine according to claim 13 , wherein the plurality of cooling channels comprise a plurality of first bent portions bent in a first circumferential direction of the casing and a plurality of second bent portions arranged alternately with the plurality of first bent portions and bent in a second circumferential direction different from the first circumferential direction.
15. The turbo machine according to claim 13 , wherein the cooling channel includes a U-shaped return portion in which a fluid changes a flow direction thereof so that the fluid flows to a second curved portion of the plurality of curved portions from a first curved portion of the plurality of curved portions, and
wherein the first curved portion and the second curved portion are adjacent to each other in the circumferential direction.
16. The turbo machine according to claim 13 , wherein the cooling channels comprise:
an inlet connected to one of the curved portions to receive cooling air from the RS cavity and through which the received cooling air flows into the plurality of curved portions; and
an outlet connected to one of the curved portions to communicate with outside of the segment body and through which the cooling air flowing through the plurality of curved portions is discharged downstream or upstream in the flow direction of the fluid flowing through the casing.
17. The turbo machine according to claim 13 , wherein in a cross-section of the segment body when viewed along the circumferential direction of the casing, the curved portion is formed such that a width W D in the flow direction of the fluid flowing through the casing is greater than a width W R in the radial direction of the casing.
18. The turbo machine according to claim 13 , wherein in a cross-section of the segment body when viewed along the flow direction of the fluid flowing through the casing, the curved portion is formed such that a width W C in the circumferential direction of the casing is greater than a width W R in the radial direction of the casing.
19. The turbo machine according to claim 12 , wherein each of the first cooling channel and the second cooling channel includes an inlet through which the cooling air introduced into the RS cavity is supplied, and
the inlet of the first cooling channel and the inlet of the second cooling channel are disposed adjacent to each other in the flow direction of the fluid flowing through the casing.
20. The turbo machine according to claim 12 , wherein the segment body is disposed outside the plurality of cooling channels in the radial direction and includes a cooling cavity into which the cooling air is introduced from the RS cavity and through which the cooling air is supplied to the plurality of cooling channels, and
the cooling cavity is divided into a first cooling cavity communicating with the first cooling channel and a second cooling cavity communicating with the second cooling channel by a partition wall installed therein.