초록

The present invention provides a seal for a gas turbine engine, comprising an annular ring with an L-shaped cross-section having a radially extending leg and an axially extending leg. A plurality of corrugations are formed in the axial leg so as to make it compliant in the circumferential direction.

대표청구항 ▼

1. A seal for a gas turbine engine, comprising: a circumferentially extending ring, said ring having a radially extending leg and an axially extending leg, said axially extending leg comprising a plurality of corrugations. 2. The seal of claim 1, wherein said corrugations comprise an annular a

1. A seal for a gas turbine engine, comprising: a circumferentially extending ring, said ring having a radially extending leg and an axially extending leg, said axially extending leg comprising a plurality of corrugations. 2. The seal of claim 1, wherein said corrugations comprise an annular array of alternating convex and concave undulations formed in said axially extending leg. 3. The seal of claim 1, wherein said seal is formed from a metal alloy. 4. The seal of claim 1 further comprising a plurality of holes formed through said radially extending leg. 5. The seal of claim 1 further comprising a plurality of elongated slots formed through said radially extending leg. 6. The seal of claim 1 further comprising a plurality of countersunk holes formed through said radially extending leg. 7. A joint assembly for a gas turbine engine, comprising: a first generally annular member having a first radially extending joint face, a second generally annular member having a second radially extending joint face; and an annular seal disposed between said first and second annular members, said seal comprising: a radially extending leg connected to an axially extending leg, wherein said radially extending leg is disposed between said first joint face and said second joint face, wherein said axially extending leg is corrugated in a circumferential direction. 8. The joint assembly of claim 7, wherein said seal is formed from a metal alloy. 9. The joint assembly of claim 7 further comprising a plurality of holes formed through said radially extending leg. 10. The joint assembly of claim 7 further comprising a plurality of elongated slots formed through said radially extending leg. 11. The joint assembly of claim 7 further comprising a plurality of countersunk holes formed through said radially extending leg of said discourager seal. 12. A joint assembly for a gas turbine engine, comprising: a generally annular turbine frame having a first radially extending joint face; a generally annular turbine casing disposed axially rearward of said turbine frame and having a second radially extending joint face; an annular turbine nozzle disposed radially inward of said turbine frame, said turbine nozzle comprising a hollow airfoil and an arcuate band, said band having an exit hole formed therein; an annular turbine shroud having a surface defining a gas flowpath, said turbine shroud disposed radially inward of said turbine casing, such that an annular cavity is defined between said turbine casing and said turbine shroud, and such that a circumferentially extending gap is defined between said turbine shroud and said turbine nozzle, said gap being in fluid communication with said flowpath and said annular cavity; and an annular discourager seal disposed between said turbine frame and said turbine casing, said discourager seal comprising a radially extending leg connected to an axially extending leg, wherein said radially extending leg is disposed between said first joint face and said second joint face, and said axially extending leg is disposed so as to redirect a fluid flow from said exit hole, and wherein said axially extending leg comprises an annular array of corrugations. 13. The joint assembly of claim 12, wherein said discourager seal is formed from a metal alloy. 14. The joint assembly of claim 12 further comprising a plurality of holes formed through said radially extending leg of said discourager seal. 15. The joint assembly of claim 12 further comprising a plurality of elongated slots formed through said radially extending leg of said discourager seal. 16. The joint assembly of claim 12 further comprising a plurality of countersunk holes formed through said radially extending leg of said discourager seal.