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The present disclosure relates to a turbomachine that includes a first component and a second component coupled to another and a seal assembly between the two components. The seal assembly may include an upstream corner shim and a downstream corner shim, where one of the upstream corner shim or the

The present disclosure relates to a turbomachine that includes a first component and a second component coupled to another and a seal assembly between the two components. The seal assembly may include an upstream corner shim and a downstream corner shim, where one of the upstream corner shim or the downstream corner shim includes a pressure actuation feature configured to block a flow of gas between the two components.

대표청구항 ▼

1. A turbomachine comprising: a first component comprising a first seal slot with a first corner;a second component coupled to the first component, wherein the second component comprises a second seal slot with a second corner;a gap between the first component and the second component; anda seal ass

1. A turbomachine comprising: a first component comprising a first seal slot with a first corner;a second component coupled to the first component, wherein the second component comprises a second seal slot with a second corner;a gap between the first component and the second component; anda seal assembly disposed in the first component, the second component, and a portion of the gap, wherein the seal assembly comprises a first corner shim and a second corner shim, and wherein each of the first corner shim and the second corner shim include two or more members connected by one or more corners and the first corner shim comprises a pressure actuation feature configured to cover end gaps in the first seal slot, the second seal slot, or both when a pressure in the gap exceeds a threshold biasing force of the pressure actuation feature. 2. The turbomachine of claim 1, wherein the first corner shim comprises a first portion and a second portion. 3. The turbomachine of claim 2, wherein the pressure actuation feature comprises a first deformable feature of the first portion and a second deformable feature of the second portion. 4. The turbomachine of claim 3, wherein the first deformable feature is between 3% and 50% of the first portion and the second deformable feature is between 3% and 50% of the second portion. 5. The turbomachine of claim 1, wherein the pressure actuation feature comprises a first corrugated portion of the first corner shim and a single-corrugated portion of the first corner shim. 6. The turbomachine of claim 5, wherein the single-corrugated portion comprises a first curved portion and a second curved portion separated by a single kink. 7. The turbomachine of claim 1, wherein the pressure actuation feature comprises a first corrugated portion of the first corner shim and a dual-corrugated portion of the first corner shim. 8. The turbomachine of claim 7, wherein the dual-corrugated portion of the first corner shim comprises a first kink and a second kink. 9. The turbomachine of claim 8, wherein the dual-corrugated portion comprises a first curved portion, a second curved portion, and a deformable feature, the first curved portion and the second curved portion are separated by the first kink, and the second curved portion and the deformable feature are separated by the second kink. 10. The turbomachine of claim 1, wherein the threshold biasing force is configured to be substantially equal to a pressure force corresponding to the fluid flowing through the end gaps. 11. A power generation system, comprising: a turbomachine;a first component of the turbomachine comprising a first seal slot, wherein the first seal slot comprises a first segment and a second segment coupled to one another by a first corner;a second component of the turbomachine coupled to the first component, wherein the second component comprises a second seal slot, and the second seal slot comprises a third segment and a fourth segment coupled to one another by a second corner;a gap between the first component and the second component; anda seal assembly positioned in the first seal slot, the second seal slot, and a portion of the gap, wherein the seal assembly comprises: a first corner shim positioned in the first segment, the second segment, the third segment, and the fourth segment; anda second corner shim positioned in the first segment, the second segment, the third segment, and the fourth segment, wherein each of the first corner shim and the second corner shim include two or more members connected by one or more corners and the second corner shim comprises a pressure actuation feature configured to cover end gaps in the first seal slot, the second seal slot, or both when a pressure in the gap exceeds a threshold biasing force of the pressure actuation feature. 12. The turbomachine of claim 11, wherein the first corner shim comprises a first portion and a second portion. 13. The turbomachine of claim 12, wherein the pressure actuation feature comprises a first deformable feature of the first portion and a second deformable feature of the second portion. 14. The turbomachine of claim 11, wherein the pressure actuation feature comprises a first corrugated portion of the first corner shim and a single-corrugated portion of the first corner shim. 15. The turbomachine of claim 11, wherein the pressure actuation feature comprises a first corrugated portion of the first corner shim and a dual-corrugated portion of the first corner shim. 16. The power generation system of claim 11, wherein the threshold biasing force is configured to be substantially equal to a pressure force corresponding to the fluid flowing through the end gaps. 17. A method, comprising: disposing a first portion of a seal assembly in a first seal slot of a first component of a turbomachine, wherein the seal assembly comprises a first corner shim and a second corner shim, and wherein each of the first corner shim and the second corner shim include two or more members connected by one or more corners and the first corner shim comprises a pressure actuation feature;disposing a second portion of the seal assembly in a second seal slot of a second component of the turbomachine; andcoupling the first component to the second component to form a gap between the first component and the second component, wherein the pressure actuation feature is configured to cover end gaps in the first seal slot, the second seal slot, or both when a pressure in the gap exceeds a threshold biasing force of the pressure actuation feature. 18. The method of claim 17, comprising forming the pressure actuation feature by bending a first portion of the first corner shim to form a first deformable feature of the first portion and bending a second portion of the first corner shim to form a second deformable feature of the second portion. 19. The method of claim 17, wherein the pressure actuation feature comprises a first corrugated portion of the first corner shim and a single-corrugated portion of the first corner shim. 20. The method of claim 17, wherein the pressure actuation feature comprises a first corrugated portion of the first corner shim and a dual-corrugated portion of the first corner shim.