Method and system for providing cooling for turbine components

Patent metadata

Field	Value
Publication number	US-9416662-B2
Application number	US-201314016769-A
Country	US
Kind code	B2
Filing date	Sep 3, 2013
Priority date	Sep 3, 2013
Publication date	Aug 16, 2016
Grant date	Aug 16, 2016

Abstract

A system for providing cooling for a turbine component that includes an outer surface exposed to combustion gases is provided. A component base includes at least one fluid supply passage coupleable to a source of cooling fluid. At least one feed passage communicates with the at least one fluid supply passage. At least one delivery channel communicates with the at least one feed passage. At least one cover layer covers the at least one feed passage and the at least one delivery channel, defining at least in part the component outer surface. At least one discharge passage extends to the outer surface. A diffuser section is defined in at least one of the at least one delivery channel and the at least one discharge passage, such that a fluid channeled through the system is diffused prior to discharge adjacent the outer surface.

First claim

What is claimed is:

1. A method for providing a cooling system for a turbine component that includes an outer surface that is exposed to combustion gases during turbine operation, said method comprising:
defining a component base with at least one fluid supply passage coupleable to a source of cooling fluid;
defining at least one feed passage in the component base, wherein the at least one feed passage is coupled in flow communication with the at least one fluid supply passage;
defining a plurality of delivery channels in the component base, wherein the plurality of delivery channels are coupled in flow communication with the at least one feed passage;
defining at least one cover layer on the base to cover the at least one feed passage and the plurality of delivery channels, wherein the at least one cover layer defines a boundary of the plurality of delivery channels, and at least in part defines the component outer surface;
defining discharge passage through the at least one cover layer and extending at least partially within the component base, wherein the discharge passage is fluidly coupled at one end to the plurality of delivery channels and extends from within the component base through the at least one cover layer to the outer surface; and
defining a diffuser section in the plurality of delivery channels such that a fluid channeled through the plurality of delivery channels is diffused prior to discharge adjacent the outer surface.

2. A method in accordance with claim 1 , wherein defining a diffuser section in the plurality of delivery channels comprises:
defining a first delivery channel section with a length, wherein the first delivery channel section includes a substantially constant cross-sectional area along the length; and
defining a second delivery channel section, wherein the second delivery channel section includes a discharge cross-sectional area greater than the cross-sectional area of the first delivery channel section.

3. A method in accordance with claim 1 , further comprising defining the discharge passage with an inlet cross-sectional area and a discharge cross-sectional area, such that the discharge cross-sectional area is greater than the inlet cross-sectional area.

4. A method in accordance with claim 1 , wherein said method comprises:
defining a plurality of feed passages in the component base, wherein each of the plurality of feed passages is coupled in flow communication with the at least one fluid supply passage; and
defining the plurality of delivery channels in the component base, wherein each of the plurality of delivery channels is coupled in flow communication with a corresponding feed passage.

5. A method in accordance with claim 4 , wherein said method comprises defining a distribution passage coupled in flow communication with the at least one fluid supply passage, the distribution passage further coupled in flow communication with each of the feed passages.

6. A method in accordance with claim 4 , wherein defining the discharge passage through the at least one cover layer comprises defining an elongated trench in the at least one cover layer, wherein the elongated trench is coupled in flow communication with each of the plurality of delivery channels, such that cooling fluid channeled from the plurality of delivery channels into the elongated trench is subsequently discharged from the elongated trench to define a cooling fluid film adjacent the component outer surface.

7. A method in accordance with claim 6 , wherein defining an elongated trench in the at least one cover layer comprises defining the elongated trench with an inlet end wall and an outlet end wall, wherein the inlet end wall and the outlet end wall diverge, such that cooling fluid channeled into the elongated trench is diffused prior to discharge from the elongated trench.

8. A system for providing cooling for a turbine component that includes an outer surface that is exposed to combustion gases during turbine operation, said system comprising:
a component base that includes at least one fluid supply passage coupleable to a source of cooling fluid;
at least one feed passage defined in the component base, wherein the at least one feed passage is coupled in flow communication with the at least one fluid supply passage;
a plurality of delivery channels defined in the component base, wherein the plurality of delivery channels are coupled in flow communication with the at least one feed passage;
at least one cover layer defined on the base to cover the at least one feed passage and the plurality of delivery channels, wherein the at least one cover layer defines a boundary of the plurality of delivery channels and the at least one cover layer defines at least in part the component outer surface;
a discharge passage defined through the at least one cover layer and extending at least partially within the component base, wherein the discharge passage is fluidly coupled at one end to the plurality of delivery channels and extends from within the component base through the at least one cover layer to the outer surface; and
a diffuser section defined in the plurality of delivery channels, such that a fluid channeled through the plurality of delivery channels is diffused prior to discharge adjacent the outer surface.

9. A system in accordance with claim 8 , wherein said diffuser section comprises:
a first delivery channel section defined in the base, wherein the first delivery channel section includes a length and a substantially constant cross-sectional area along the length; and
a second delivery channel section defined in the base and coupled in flow communication with the first delivery channel section, wherein the second delivery channel section includes a discharge cross-sectional area greater than the cross-sectional area of the first delivery channel section.

10. A system in accordance with claim 8 , wherein the diffuser section includes an inlet cross-sectional area and a discharge cross-sectional area, such that the discharge cross-sectional area is greater than the inlet cross-sectional area.

11. A system in accordance with claim 8 , said system comprising:
a plurality of feed passages defined in the component base, wherein each of the plurality of feed passages is coupled in flow communication with the at least one fluid supply passage, the plurality of delivery channels is defined in the component base, and each of the plurality of delivery channels is coupled in flow communication with a corresponding feed passage.

12. A system in accordance with claim 11 , wherein said system comprises comprising a distribution passage defined in the base and coupled in flow communication with the at least one fluid supply passage, and wherein said distribution passage is coupled in flow communication with each of the feed passages.

13. A system in accordance with claim 11 , wherein said system comprises an elongated trench defined in the at least one cover layer, and wherein the elongated trench is coupled in flow communication with each of the plurality of delivery channels, such that cooling fluid channeled from the plurality of delivery channels into the elongated trench is subsequently discharged from the elongated trench to define a cooling fluid film adjacent the component outer surface.

14. A system in accordance with claim 13 , wherein the elongated trench comprises an inlet end wall and an outlet end wall, and wherein the inlet end wall and the outlet end wall diverge, such that cooling fluid channeled into the elongated trench is diffused prior to discharge from the elongated trench.

15. A gas turbine syste

Assignees

• Gen Electric

Inventors

• Morgan Victor John
• Lacy Benjamin Paul

Classifications

• F02C7/12

  Cooling of plants (of component parts, see the relevant subclasses, e.g. F01D; cooling of engines in general F01P) · CPC title

• Y10T29/4932

  Turbomachine making · CPC title

• F05D2260/204

  by the use of microcircuits · CPC title

• F01D25/12

  Cooling · CPC title

• F05D2220/32

  in gas turbines · CPC title