Dual hydorstatic seal assembly
A seal assembly includes first and second rings. The first ring includes a first outer ring, a first beam connected to the first outer ring, and a first shoe. The first shoe includes free and fixed ends and is configured to move radially. The second seal ring is disposed axially adjacent and is attached to the first seal ring. The second seal ring includes a second outer ring, a second beam connected to the second outer ring, and a second shoe. The second shoe includes free and fixed ends and is configured to move in a generally radial direction. The free end of the second shoe is disposed axially adjacent to the fixed end of the first shoe. The fixed end of the second shoe is disposed axially adjacent to the free end of the first shoe.
1. A seal assembly comprising:
a first seal ring comprising:
a first outer ring;
a first beam connected to the first outer ring;
a first shoe connected to and extending from the first beam, the first shoe with a first free end and a first fixed end, wherein the first shoe is configured to move in a generally radial direction relative to the first outer ring;
a second seal ring disposed axially adjacent and attached to the first seal ring, wherein the first seal ring is attached to the second seal ring via mechanical attachment, wherein the second seal ring comprises:
a second outer ring;
a second beam connected to the second outer ring; and
a second shoe connected to and extending from the second beam, the second shoe with a second free end and a second fixed end, wherein the second shoe is configured to move in a generally radial direction relative to the second outer ring, wherein the second free end of the second shoe is disposed axially adjacent to the first fixed end of the first shoe, and wherein the second fixed end of the second shoe is disposed axially adjacent to the first free end of the first shoe, and
at least one pin that is engaged with the first seal ring and the second seal ring such that the first and second seal rings are attached to each other via the at least one pin.
2. The seal assembly of claim 1 , further comprising a hydrostatic seal.
3. The seal assembly of claim 1 , wherein the seal assembly is configured to be disposed in a turbine section of a gas turbine engine.
4. The seal assembly of claim 1 and further comprising:
a spacer disposed axially adjacent and in contact with one of the first seal ring or the second seal ring;
a secondary seal in contact with the spacer and against one of the first seal ring or the second seal ring;
a seal cover in contact with a portion of the spacer such that the seal cover retains the secondary seal against the spacer and one of the first seal ring or the second seal ring;
a carrier disposed radially outward from the first seal ring and the second seal ring; and
a seal plate disposed on an axial end of the seal assembly opposite from the seal cover, wherein the seal plate is radially inward from and in contact with the carrier.
5. The seal assembly of claim 1 , wherein the at least one pin comprises a plurality of pins, wherein a first pin of the plurality of pins attaches the first outer ring of the first seal ring to the second outer ring of the second seal ring, wherein a second pin of the plurality of pins attaches the first free end of the first shoe to the second fixed end of the second shoe, and wherein a third pin of the plurality of pins attaches the first fixed end of the first shoe to the second free end of the second shoe.
6. The seal assembly of claim 1 , wherein the first seal ring is attached to the second seal ring via chemical attachment.
7. The seal assembly of claim 6 , wherein the first seal ring is attached to the second seal ring by welding or brazing.
8. The seal assembly of claim 1 , wherein the first shoe of the first seal ring is circumferentially aligned with the second shoe of the second seal ring.
9. The seal assembly of claim 1 and further comprising a seal element connected to and extending radially inward from at least one of the first shoe and the second shoe.
10. A seal assembly for use in a gas turbine engine, the seal assembly comprising:
a rotating structure;
a static structure aligned with the rotating structure along a radial direction;
a floating non-contact seal disposed between the rotating structure and the static structure, the floating non-contact seal comprising:
a first seal ring comprising:
a first outer ring;
a first beam connected to the first outer ring; and
a first shoe connected to and extending from the first beam, the first shoe with a first free end and a first fixed end;
a second seal ring disposed axially adjacent and attached to the first seal ring, wherein the first seal ring is attached to the second seal ring via mechanical attachment, wherein the second seal ring comprises:
a second outer ring;
a second beam connected to the second outer ring; and
a second shoe connected to and extending from the second beam, the second shoe with a second free end and a second fixed end, wherein the second free end of the second shoe is disposed axially adjacent to the first fixed end of the first shoe, and wherein the second fixed end of the second shoe is disposed axially adjacent to the first free end of the first shoe;
at least one pin that is engaged with the first seal ring and the second seal ring such that the first and second seal rings are attached to each other via the pin; and
a seal element connected to and extending radially inward from at least one of the first shoe and the second shoe.
11. The seal assembly of claim 10 , wherein the seal assembly is disposed in a turbine section of the gas turbine engine.
12. The seal assembly of claim 10 , wherein the floating non-contact seal comprises a hydrostatic seal.
13. The seal assembly of claim 10 , wherein the floating non-contact seal is configured to sealingly engage with the rotating element.