Steam cooling turbine stator vane array

Patent metadata

Field	Value
Publication number	US-12392287-B2
Application number	US-202318121377-A
Country	US
Kind code	B2
Filing date	Mar 14, 2023
Priority date	Mar 14, 2023
Publication date	Aug 19, 2025
Grant date	Aug 19, 2025

Abstract

An assembly is provided for a turbine engine. This assembly includes a turbine vane array and a cooling system. The turbine vane array includes an inner platform, an outer platform and a plurality of turbine vanes extending between and connected to the inner platform and the outer platform. The turbine vanes include a first turbine vane, and the first turbine vane includes a first passage and a second passage. The cooling system is configured to direct a first fluid into the first passage and a second fluid into the second passage. The first fluid includes air and steam during a first mode. The second fluid includes the air without the steam during the first mode.

First claim

What is claimed is:

1. An assembly for a turbine engine, comprising:
an air source;
a steam source;
a turbine vane array including an inner platform, an outer platform and a plurality of turbine vanes extending between and connected to the inner platform and the outer platform, the plurality of turbine vanes comprising a first turbine vane, and the first turbine vane including a first passage and a second passage;
an air plenum disposed radially outboard of and formed by the outer platform;
a cooling system configured to direct a first flow into an interior of the first passage and a second flow into the second passage, the cooling system including a steam injector projecting into the first passage, the steam injector spaced from a sidewall of the first passage and forming an annulus circumscribing the steam injector, the annulus fluidly coupling the air plenum with the first passage, the cooling system configured to direct the steam from the steam source into the first passage through the steam injector, the cooling system configured to direct the air into the first passage through the air plenum, and wherein, during a first mode, the first flow comprises a mixture of air from the air source and steam from the steam source, and the second flow comprises the air from the air source without the steam from the steam source;
wherein during operation of the assembly in the first mode, the cooling system directs the first flow into the interior of the first passage.

2. The assembly of claim 1 , wherein during a second mode, the first flow comprises the air from the air source without the steam from the steam source; and the second flow comprises the air from the air source without the steam from the steam source.

3. The assembly of claim 1 , wherein
the steam injector is configured as a steam rail extending within the first passage; and
the cooling system is configured to direct the steam from the steam source into the first passage through the steam rail.

4. The assembly of claim 1 , wherein
the cooling system includes a plurality of steam injectors; and
the cooling system is configured to direct the steam from the steam source into the first passage through the plurality of steam injectors.

5. The assembly of claim 1 , wherein the cooling system is configured to direct the air from the air source into the second passage through the air plenum.

6. The assembly of claim 1 , wherein
the first turbine vane extends longitudinally between a leading edge and a trailing edge; and
the first passage is arranged at the leading edge.

7. The assembly of claim 1 , wherein
the first turbine vane extends longitudinally between a leading edge and a trailing edge; and
the second passage is arranged at the trailing edge.

8. The assembly of claim 1 , wherein
the first turbine vane extends longitudinally between a leading edge and a trailing edge; and
the first passage is disposed longitudinally between the leading edge and the second passage.

9. The assembly of claim 1 , wherein the first passage is fluidly discrete from the second passage within the first turbine vane.

10. The assembly of claim 1 , wherein the first passage is fluidly coupled with a plurality of cooling apertures through a sidewall of the first turbine vane.

11. The assembly of claim 1 , further comprising:
a combustor comprising a combustion chamber;
the turbine vane array arranged at an outlet from the combustion chamber; and
the air source comprising a diffuser plenum next to the combustor.

12. The assembly of claim 1 , wherein
the inner platform forms an inner peripheral boundary of a flowpath through the turbine vane array;
the outer platform forms an outer peripheral boundary of the flowpath through the turbine vane array; and
each of the plurality of turbine vanes extends across the flowpath between the inner platform and the outer platform.

13. An assembly for a turbine engine, comprising:
a turbine vane array including an inner platform, an outer platform and a plurality of turbine vanes extending between and connected to the inner platform and the outer platform, the plurality of turbine vanes comprising a first turbine vane, the first turbine vane including a sidewall, a passage and a plurality of cooling apertures, the passage extending within the first turbine vane along the sidewall, and the plurality of cooling apertures extending through the sidewall and fluidly coupled with the passage;
a structure forming an air plenum with the outer platform, the air plenum radially outboard of the outer platform and fluidly coupled with the passage through an inlet to the passage in the outer platform; and
a steam injector configured to direct steam into the passage, a tip of the steam injector disposed at the inlet to the passage such that the tip of the steam injector is disposed a first radial distance from the outer platform and a second radial distance from the inner platform that is greater than the first radial distance, and the tip disposed at the inlet axially offset from the sidewall forming a gap, the gap fluidly coupling the air plenum with the passage.

14. The assembly of claim 13 , wherein
the passage is a first passage, and the first turbine vane further includes a second passage discrete from the first passage; and
the air plenum is fluidly coupled with the second passage through an inlet to the second passage in the outer platform.

15. The assembly of claim 13 , further comprising:
a turbine section;
the turbine vane array arranged at an inlet to the turbine section.

16. An assembly for a turbine engine, comprising:
a steam source;
a diffuser plenum;
a combustor comprising a combustion chamber, the combustor disposed in the diffuser plenum;
a vane array arranged at an outlet from the combustion chamber, the vane array including an inner platform, an outer platform and a plurality of vanes, the inner platform forming an inner peripheral boundary of a flowpath through the vane array, the outer platform forming an outer peripheral boundary of the flowpath through the vane array, each of the plurality of vanes extending across the flowpath from the inner platform to the outer platform, and the plurality of vanes comprising a first vane with an internal passage;
an air plenum radially outboard of the outer platform and fluidly coupled with an interior of the internal passage; and
a cooling system configured to direct a fluid into the interior of the internal passage, the cooling system including a steam injector configured to direct steam into the interior of the internal passage, the steam injector disposed at an inlet to the interior of the internal passage and forming an annulus circumscribing the steam injector, and the annulus fluidly coupling the air plenum with the interior of the internal passage;
wherein during a first mode of operation, the cooling system directs the fluid into the interior of the internal passage, the fluid comprising both air from the diffuser plenum and steam from the steam source.

17. The assembly of claim 16 , wherein during a second mode of operation, the cooling system directs a second fluid into the internal passage, the second fluid comprising the air from the diffuser plenum.

Assignees

• Raytheon Tech Corp
• Rtx Corp

Inventors

• Kramer Stephen K
• Smith Lance L
• Boardman Gregory
• Dai Zhongtao

Classifications

• F05D2270/16

  to control water or steam injection · CPC title

• F05D2260/2322

  steam · CPC title

• F05D2260/212

  by water injection · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title

• F02C7/16

  characterised by cooling medium · CPC title