Bellows secondary seal for cantilevered hydrostatic advanced low leakage seal

1. A hydrostatic seal configured to be disposed between relatively rotatable components, the hydrostatic seal providing a primary seal between the relatively rotatable components, the hydrostatic seal comprising:

a seal carrier;

a beam extending axially from a forward end to an aft end, the beam connected to the seal carrier at the aft end, the beam having a free end at the forward end such that the beam is cantilevered with respect to the seal carrier, the beam having a sealing surface and a radially outward surface;

one or more teeth included on the sealing surface; and

a bellows seal operatively coupled to the seal carrier and in contact with the beam, the bellows seal extending between the seal carrier and the beam being closer to the free end than to the aft end such that the bellows seal provides a seal between a high pressure region and a lower pressure region, the high pressure region being forward of the free end, the bellows seal being closer to the free end than to the aft end and extending from the radially outward surface of the beam to the seal carrier in order to provide a secondary seal of the hydrostatic seal.

2. The hydrostatic seal of claim 1 , wherein the bellows seal is disposed between a radially inward surface of the seal carrier and the radially outward surface of the beam.

3. The hydrostatic seal of claim 1 , wherein the bellows seal extends longitudinally in a direction perpendicular to the radially outward surface of the beam.

4. The hydrostatic seal of claim 1 , wherein the beam includes a flange closer to the free end than to the aft end, the flange extending radially outwardly into a region at least partially defined by the seal carrier and the beam, the flange oriented at an angle between parallel and perpendicular to the beam, the bellows seal in contact with the flange.

5. The hydrostatic seal of claim 4 , wherein a first end of the bellows seal is operatively coupled to the seal carrier and a second end of the bellows seal is in contact with a forward face of the flange.

6. The hydrostatic seal of claim 1 , wherein the bellows seal allows for deflection of the beam.

7. A seal assembly disposed in a gas turbine engine, the seal assembly comprising:

a stator;

a rotor; and

a hydrostatic seal disposed between the stator and the rotor, the hydrostatic seal providing a primary seal between the stator and the rotor, the hydrostatic seal comprising:

a seal carrier;

a beam extending axially from a forward end to an aft end, the beam connected to the seal carrier at the aft end, the beam having a free end at the forward end such that the beam is cantilevered with respect to the seal carrier, the beam having a sealing surface and a radially outward surface;

one or more teeth included on the sealing surface; and

a bellows seal extending longitudinally from a first end to a second end, the bellows seal operatively coupled to the seal carrier at the first end, the bellows seal extending between the seal carrier and the beam being closer to the free end than to the aft end such that the bellows seal provides a seal between a high pressure region and a lower pressure region, the high pressure region being forward of the free end, the bellows seal being closer to the free end than to the aft end and extending from the radially outward surface of the beam to the seal carrier in order to provide a secondary seal of the hydrostatic seal.

8. The seal assembly of claim 7 , wherein the bellows seal is disposed between a radially inward surface of the seal carrier and the radially outward surface of the beam.

9. The seal assembly of claim 7 , wherein the bellows seal extends longitudinally in a direction perpendicular to the radially outward surface of the beam.

10. The seal assembly of claim 7 , wherein the second end of the bellows seal is in contact with the radially outward surface of the beam.

11. The seal assembly of claim 7 , wherein the beam includes a flange closer to the free end than to the aft end, the flange extending radially outwardly into a region at least partially defined by the seal carrier and the beam, the flange oriented at an angle between parallel and perpendicular to the beam, the bellows seal in contact with the flange.

12. A gas turbine engine comprising:

a compressor section;

a combustor section;

a turbine section; and

a seal assembly disposed in the gas turbine engine, the seal assembly comprising a stator, a rotor, and a hydrostatic seal disposed between the stator and the rotor, the hydrostatic seal providing a primary seal between the stator and the rotor, the hydrostatic seal comprising:

a seal carrier;

a beam extending axially from a forward end to an aft end, the beam connected to the seal carrier at the aft end, the beam having a free end at the forward end such that the beam is cantilevered with respect to the seal carrier, the beam having a sealing surface and a radially outward surface;

one or more teeth included on the sealing surface; and

a bellows seal in contact with the seal carrier and in contact with the beam, the bellows seal extending between the seal carrier and the beam being closer to the free end than to the aft end such that the bellows seal provides a seal between a high pressure region and a lower pressure region, the high pressure region being forward of the free end, the bellows seal being closer to the free end than to the aft end and extending from the radially outward surface of the beam to the seal carrier in order to provide a secondary seal of the hydrostatic seal.

13. The gas turbine engine of claim 12 , wherein the bellows seal allows for deflection of the beam.