Seal for a gas turbine engine having improved flexibility
View Patent ↗A seal extending between adjacent slots of a gas turbine engine is disclosed. The seal comprises a plurality of generally planar members fixed together along a central axis. The outer member further comprises rounded ends that encompass the second and plurality of third generally planar members. The seal disclosed herein improves sealing capability by providing a more compliant seal over the prior art while reducing the mechanical loads experienced along the seal weld joint, thereby improving seal durability.
1. A seal extending between adjacent slots of a gas turbine engine, said seal comprising:
an outer sleeve having a first generally planar member including a length, a width, and a first thickness, a first rounded end and a second rounded end, each of said rounded ends having a height, said width extending between said first and second ends;
a second generally planar member opposite said first generally planar member and extending generally between said first rounded end and said second rounded end, said second member having a second thickness and at least one step, thereby forming a raised portion of said second generally planar member;
a plurality of third generally planar members having a third thickness with at least one of said third members positioned within said raised portion of said second member;
a centerline extending along said length of said first planar member of said outer sleeve; and,
wherein at least one of said plurality of third generally planar members and said second generally planar member extend to a position within said first and second rounded ends and are fixed to said first generally planar member only along said centerline, such that said height of said rounded ends is greater than any other height along said width of said seal between said rounded ends.
2. The seal of claim 1 wherein said plurality of third members comprises three members.
3. The seal of claim 1 wherein said first, second, and plurality of third generally planar members are fixed together by a means such as welding through each of said generally planar member thicknesses.
4. The seal of claim 1 wherein said first thickness is greater than said second thickness and said third thickness.
5. The seal of claim 1 wherein said seal is fabricated from a high temperature cobalt-based alloy.
6. The seal of claim 5 wherein said outer sleeve is fabricated from a sheet having a first thickness between 0.015 inches and 0.050 inches.
7. The seal of claim 5 wherein said second and third generally planar members are fabricated from a sheet having a second and third thickness, respectively, between 0.010 inches and 0.040 inches.
8. The seal of claim 1 wherein said rounded ends of said seal are in contact with at least one wall of each of said adjacent slots.
9. A seal extending between adjacent slots of a gas turbine engine, said seal comprising:
an outer sleeve having a first generally planar member including a length, a width, and a first thickness, a substantially rounded first end, a substantially rounded second end, each of said rounded ends having a height, said width extending between said first end and said second end;
a second generally planar member opposite said first generally planar member and extending generally between said first end and said second end, said second member having a second thickness and at least one step, thereby forming a raised portion of said second generally planar member;
a plurality of third generally planar members having a third thickness with at least one of said third members positioned immediately adjacent to and within said raised portion of said second member;
a centerline extending along said length of said first planar member of said outer sleeve; and,
wherein said second generally planar member and at least one of said plurality of third generally planar members extend to a position within said first and second rounded ends, such that portions of said second planar member and at least one of said plurality of third generally planar members are enclosed by said substantially rounded first and second ends of said outer sleeve, said second generally planar member and at least one of said plurality of third generally planar members are fixed to said first generally planar member only along said centerline, and wherein said height of said rounded ends is greater than any other height along said width of said seal between said rounded ends.
10. The seal of claim 9 wherein said plurality of third members comprises three members.
11. The seal of claim 9 wherein said first, second, and plurality of third generally planar members are fixed together by a means such as welding through each of said generally planar member thicknesses.
12. The seal of claim 9 wherein said first thickness is greater than said second thickness and said third thickness.
13. The seal of claim 9 wherein said seal is fabricated from a high temperature cobalt-based alloy.
14. The seal of claim 13 wherein said outer sleeve is fabricated from a sheet having a first thickness between 0.015 inches and 0.050 inches.
15. The seal of claim 13 wherein said second and third generally planar members are fabricated from a sheet having a second and third thickness, respectively, between 0.010 inches and 0.040 inches.
16. The seal of claim 9 wherein said rounded ends of said seal are in contact with at least one wall of each of said adjacent slots.