Cooling circuits for a multi-wall blade

Patent metadata

Field	Value
Publication number	US-10240465-B2
Application number	US-201615334454-A
Country	US
Kind code	B2
Filing date	Oct 26, 2016
Priority date	Oct 26, 2016
Publication date	Mar 26, 2019
Grant date	Mar 26, 2019

Abstract

A trailing edge cooling system for a multi-wall blade, including: a set of outward legs extending toward a trailing edge of the multi-wall blade and fluidly coupled to a coolant feed; a set of return legs extending away from the trailing edge of the multi-wall blade and fluidly coupled to a coolant collection passage; and a connecting system for fluidly coupling the set of outward legs and the set of return legs; wherein the set of outward legs is radially offset from the set of return legs along a radial axis of the multi-wall blade.

First claim

What is claimed is:

1. A trailing edge cooling system for a multi-wall blade, comprising:
a set of outward legs extending toward a trailing edge of the multi-wall blade and fluidly coupled to a coolant feed;
a set of return legs extending away from the trailing edge of the multi-wall blade and fluidly coupled to a coolant collection passage; and
a connecting system for fluidly coupling the set of outward legs and the set of return legs;
wherein the set of outward legs is radially offset from the set of return legs along a radial axis of the multi-wall blade.

2. The trailing edge cooling system according to claim 1 , wherein the set of return legs is circumferentially offset relative to the set of outward legs.

3. The trailing edge cooling system according to claim 2 , wherein the set of outward legs extends along a suction side of the multi-wall blade and the set of return legs extends along a pressure side of the multi-wall blade, or wherein the set of outward legs extends along the pressure side of the multi-wall blade and the set of return legs extends along the suction side of the multi-wall blade.

4. The trailing edge cooling system according to claim 1 , wherein the coolant feed is fluidly coupled to a plurality of sets of outward legs, and wherein the coolant collection passage is fluidly coupled to a plurality of sets of return legs.

5. The trailing edge cooling system according to claim 4 , wherein a first outward leg in a given set of outward legs is fluidly coupled by the connecting system to a return leg in an adjacent set of return legs, and wherein a second outward leg in the given set of outward legs is fluidly coupled by the connecting system to a return leg in another adjacent set of return legs.

6. The trailing edge cooling system according to claim 5 , wherein the connecting system comprises an aft connection, the aft connection connecting the outward legs of each set of outward legs and the return legs of each set of return legs.

7. The trailing edge cooling system according to claim 6 , wherein the aft connection includes contoured portions positioned at points between the outward legs of each set of outward legs and between the return legs of each set of return legs.

8. The trailing edge cooling system according to claim 5 , wherein the connecting system comprises a plurality of turns.

9. The trailing edge cooling system according to claim 4 , wherein an outward leg in a given set of outward legs is fluidly coupled by a first turn to a return leg in an adjacent set of return legs, and wherein the outward leg in the given set of outward legs is fluidly coupled by a second turn to a return leg in another adjacent set of return legs.

10. The trailing edge cooling system according to claim 9 , wherein the given set of outward legs includes a single outward leg.

11. The trailing edge cooling system according to claim 10 , wherein the adjacent sets of return legs each include a single return leg.

12. A multi-wall turbine blade, comprising:
a trailing edge cooling system disposed within the multi-wall turbine blade, the trailing edge cooling system comprising:
a set of outward legs extending toward a trailing edge of the multi-wall blade and fluidly coupled to a coolant feed;
a set of return legs extending away from the trailing edge of the multi-wall blade and fluidly coupled to a coolant collection passage; and
a connecting system for fluidly coupling the set of outward legs and the set of return legs;
wherein the set of outward legs is radially offset from the set of return legs along a radial axis of the multi-wall blade.

13. The multi-wall turbine blade according to claim 12 , wherein the set of return legs is circumferentially offset relative to the set of outward legs.

14. The multi-wall turbine blade according to claim 12 , wherein the set of outward legs extends along a suction side of the multi-wall blade and the set of return legs extends along a pressure side of the multi-wall blade, or wherein the set of outward legs extends along the pressure side of the multi-wall blade and the set of return legs extends along the suction side of the multi-wall blade.

15. The multi-wall turbine blade according to claim 12 , wherein the coolant feed is fluidly coupled to a plurality of sets of outward legs, and wherein the coolant collection passage is fluidly coupled to a plurality of sets of return legs.

16. The multi-wall turbine blade according to claim 15 , wherein a first outward leg in a given set of outward legs is fluidly coupled by the connecting system to a return leg in an adjacent set of return legs, and wherein a second outward leg in the given set of outward legs is fluidly coupled by the connecting system to a return leg in another adjacent set of return legs.

17. The multi-wall turbine blade according to claim 16 , wherein the connecting system comprises an aft connection, the aft connection connecting the outward legs of each set of outward legs and the return legs of each set of return legs.

18. The multi-wall turbine blade according to claim 17 , wherein the aft connection includes contoured portions positioned at points between the outward legs of each set of outward legs and between the return legs of each set of return legs.

19. The multi-wall turbine blade according to claim 15 , wherein the connecting system comprises a plurality of turns, and wherein an outward leg in a given set of outward legs is fluidly coupled by a first turn to a return leg in an adjacent set of return legs, and wherein the outward leg in the given set of outward legs is fluidly coupled by a second turn to a return leg in another adjacent set of return legs.

20. A turbomachine, comprising:
a gas turbine system including a compressor component, a combustor component, and a turbine component, the turbine component including a plurality of turbine blades, at least one of the turbine blades including a multi-wall blade; and
a trailing edge cooling system disposed within the multi-wall blade, the trailing edge cooling system including:
a set of outward legs extending toward a trailing edge of the multi-wall blade and fluidly coupled to a coolant feed;
a set of return legs extending away from the trailing edge of the multi-wall blade and fluidly coupled to a coolant collection passage; and
a connecting system for fluidly coupling the set of outward legs and the set of return legs;
wherein the set of outward legs is radially and circumferentially offset from the set of return legs along a radial axis of the multi-wall blade.

Assignees

• Gen Electric

Inventors

• Weber David Wayne
• Hanet Robert Peter
• Foster Gregory Thomas
• Leary Brendon James

Classifications

• F05D2240/122

  related to the trailing edge of a stator vane · CPC title

• F02C3/04

  having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) · CPC title

• F05D2260/202

  by film cooling · CPC title

• F05D2240/304

  related to the trailing edge of a rotor blade · CPC title

• F05D2240/35

  Combustors or associated equipment · CPC title