Turbine bucket having outlet path in shroud

Patent metadata

Field	Value
Publication number	US-9885243-B2
Application number	US-201514923685-A
Country	US
Kind code	B2
Filing date	Oct 27, 2015
Priority date	Oct 27, 2015
Publication date	Feb 6, 2018
Grant date	Feb 6, 2018

Abstract

A turbine bucket according to embodiments includes: a base; a blade coupled to the base, extending radially outward from the base, and including: a body having: a pressure side; a suction side opposing the pressure side; a leading edge between the pressure side and the suction side; and a trailing edge between the pressure side and the suction side on a side opposing the leading edge; and a plurality of radially extending cooling passageways within the body; and a shroud coupled to the blade radially outboard of the blade, including: a plurality of radially extending outlet passageways fluidly connected with a first set of the plurality of radially extending cooling passageways within the body; and an outlet path extending at least partially circumferentially through the shroud and fluidly connected with all of a second, distinct set of the plurality of radially extending cooling passageways within the body.

First claim

What is claimed is:

1. A turbine bucket comprising:
a base;
a blade coupled to the base and extending radially outward from the base, the blade including:
a body having:
a pressure side; a suction side opposing the pressure side; a leading edge between the pressure side and the suction side; and a trailing edge between the pressure side and the suction side on a side opposing the leading edge; and

a plurality of radially extending cooling passageways within the body; and

a shroud coupled to the blade radially outboard of the blade, the shroud including:
a plurality of radially extending outlet passageways fluidly connected with a first set of the plurality of radially extending cooling passageways within the body;
an outlet path extending at least partially circumferentially through the shroud and fluidly connected with all of a second, distinct set of the plurality of radially extending cooling passageways within the body; and
a rail delineating an approximate mid-point between a leading half of the shroud and a trailing half of the shroud, wherein the outlet path extends within the shroud through the leading half and the rail.

2. The turbine bucket of claim 1 , further comprising:
at least one bleed aperture fluidly coupled with at least one of the first set of the plurality of radially extending cooling passageways, the at least one bleed aperture extending through the body at the trailing edge.

3. The turbine bucket of claim 2 , further comprising a plenum within the body, the plenum fluidly connected with first set of the plurality of radially extending cooling passageways and the at least one bleed aperture.

4. The turbine bucket of claim 3 , wherein the plenum fluidly isolates the first set of the plurality of radially extending cooling passageways from the outlet path.

5. The turbine bucket of claim 4 , wherein the plenum has a trapezoidal cross-sectional shape within the body, as seen in a cross-sectional plane intersecting the leading edge and the trailing edge.

6. The turbine bucket of claim 1 , wherein the plurality of radially extending outlet passageways extend from the body to a radially outer region.

7. The turbine bucket of claim 6 , wherein the plurality of radially extending outlet passageways are fluidly isolated from the outlet path in the shroud.

8. The turbine bucket of claim 7 , wherein the plurality of radially extending outlet passageways are located proximate the trailing edge of the body.

9. The turbine bucket of claim 1 , wherein an entirety of a cooling fluid passing through the second, distinct set of the plurality of radially extending cooling passageways within the body exits the body through the outlet path.

10. The turbine bucket of claim 9 , wherein the plurality of radially extending outlet passageways fluidly outlet to a location radially outboard of the shroud, and wherein the outlet path outlets to the location radially outboard of the shroud.

11. A turbine bucket comprising:
a base;
a blade coupled to the base and extending radially outward from the base, the blade including:
a body having:
a pressure side; a suction side opposing the pressure side; a leading edge between the pressure side and the suction side; and a trailing edge between the pressure side and the suction side on a side opposing the leading edge;

a plurality of radially extending cooling passageways within the body; and
at least one bleed aperture fluidly coupled with a first set of the plurality of radially extending cooling passageways, the at least one bleed aperture extending through the body at the trailing edge; and

a shroud coupled to the blade radially outboard of the blade, the shroud including:
an outlet path extending at least partially circumferentially through the shroud and fluidly connected with all of a second, distinct set of the plurality of radially extending cooling passageways within the body; and
a rail delineating an approximate mid-point between a leading half of the shroud and a trailing half of the shroud, wherein the outlet path extends within the shroud through the leading half and the rail.

12. The turbine bucket of claim 11 , further comprising a plenum within the body, the plenum fluidly connected with first set of the plurality of radially extending cooling passageways and the at least one bleed aperture.

13. The turbine bucket of claim 12 , wherein the plenum fluidly isolates the first set of the plurality of radially extending cooling passageways from the outlet path.

14. The turbine bucket of claim 13 , wherein the plenum has a trapezoidal cross-sectional shape within the body, as seen in a cross-sectional plane intersecting the leading edge and the trailing edge.

15. The turbine bucket of claim 11 , wherein an entirety of a cooling fluid passing through the second, distinct set of the plurality of radially extending cooling passageways within the body exits the body through the outlet path.

16. The turbine bucket of claim 11 , wherein the outlet path outlets to a location radially outboard of the shroud, wherein the at least one bleed aperture outlets to a location radially inboard of the shroud at the trailing edge.

17. A turbine comprising:
a stator; and
a rotor contained within the stator, the rotor having:
a spindle; and
a plurality of buckets extending radially from the spindle, at least one of the plurality of buckets including:
a base;
a blade coupled to the base and extending radially outward from the base, the blade including:
a body having:
 a pressure side; a suction side opposing the pressure side; a leading edge between the pressure side and the suction side; and a trailing edge between the pressure side and the suction side on a side opposing the leading edge; and
a plurality of radially extending cooling passageways within the body; and

a shroud coupled to the blade radially outboard of the blade, the shroud including:
a plurality of radially extending outlet passageways fluidly connected with a first set of the plurality of radially extending cooling passageways within the body;
an outlet path extending at least partially circumferentially through the shroud and fluidly connected with all of a second, distinct set of the plurality of radially extending cooling passageways within the body; and
a rail delineating an approximate mid-point between a leading half of the shroud and a trailing half of the shroud, wherein the outlet path extends within the shroud through the leading half and the rail.

18. The turbine of claim 17 , further comprising:
at least one bleed aperture fluidly coupled with at least one of the first set of the plurality of radially extending cooling passageways, the at least one bleed aperture extending through the body at the trailing edge; and
a plenum within the body, the plenum fluidly connected with first set of the plurality of radially extending cooling passageways and the at least one bleed aperture.

Assignees

• Gen Electric

Inventors

• Chouhan Rohit
• Jaiswal Shashwat Swami
• Taylor Zachary James

Classifications

• F01D17/105

  by passing part of the fluid · CPC title

• F01D5/02

  Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title

• F01D9/02

  Nozzles; Nozzle boxes; Stator blades; Guide conduits {, e.g. individual nozzles (nozzle boxes F01D9/047)} · CPC title

• F05D2260/20

  Heat transfer, e.g. cooling · CPC title

• F01D11/08

  for sealing space between rotor blade tips and stator (specially-shaped blade tips therefor F01D5/20) · CPC title