Hydrostatic seal
A hydrostatic seal assembly includes a primary seal configured to maintain a selected gap between the primary seal and a rotating component. The primary seal includes a seal support, a seal shoe, and one or more seal beams operably connecting the seal support to the seal shoe. The one or more seal beams are configured as spring elements integral with the seal shoe to allow radial movement of the seal shoe relative to the seal support. A seal carrier including a radial outer wall is configured to radially position the primary seal. The seal carrier is configured for a non-contact relationship with the seal shoe during operation of the hydrostatic seal assembly.
1. A hydrostatic seal assembly, comprising:
a primary seal configured to maintain a selected gap between the primary seal and a rotating component, the primary seal including:
a seal support;
a seal shoe; and
one or more seal beams operably connecting the seal support to the seal shoe, the one or more seal beams configured as spring elements integral with the seal shoe to allow radial movement of the seal shoe relative to the seal support; and
a seal carrier including:
a radial outer wall configured to radially position the primary seal, the seal carrier configured for a non-contact relationship with the seal shoe during operation of the hydrostatic seal assembly; and
an aft wall extending radially inwardly from the radial outer wall;
wherein the aft wall does not radially overlap the one or more seal beams.
2. The hydrostatic seal of claim 1 , wherein the aft wall does not extend radially inwardly to a seal shoe radial position.
3. The hydrostatic seal of claim 1 , wherein the radial outer wall and the aft wall are formed as a single unitary component.
4. The hydrostatic seal of claim 1 , wherein the aft wall is disposed at a first axial end of the seal support and a secondary seal is disposed at a second end of the seal support opposite the first axial end.
5. The hydrostatic seal of claim 1 , wherein the seal carrier is configured for a non-contact relationship with one or more seal beams during operation of the hydrostatic seal assembly.
6. The hydrostatic seal of claim 1 , including one or more stops formed in the seal shoe configured to limit radial travel of the seal shoe.
7. A turbine section of a gas turbine engine, comprising:
a turbine stator;
a turbine rotor configured to rotate about an engine central longitudinal axis relative to the turbine stator; and
a hydrostatic seal assembly fixed to the turbine stator comprising:
a primary seal configured to maintain a selected gap between the primary seal and the turbine rotor, the primary seal including:
a seal support;
a seal shoe; and
one or more seal beams operably connecting the seal support to the seal shoe, the one or more seal beams configured as spring elements integral with the seal shoe to allow radial movement of the seal shoe relative to the seal support; and
a seal carrier including:
a radial outer wall configured to radially position the primary seal, the seal carrier configured for a non-contact relationship with the seal shoe during operation of the hydrostatic seal assembly; and
an aft wall extending radially inwardly from the radial outer wall;
wherein the aft wall does not radially overlap the one or more seal beams.
8. The turbine section of claim 7 , wherein the aft wall does not extend radially inwardly to a seal shoe radial position.
9. The turbine section of claim 7 , wherein the radial outer wall and the aft wall are formed as a single unitary component.
10. The turbine section of claim 7 , wherein the aft wall is disposed at a first axial end of the seal support and a secondary seal is disposed at a second end of the seal support opposite the first axial end.
11. The turbine section of claim 7 , wherein the seal carrier is configured for a non-contact relationship with one or more seal beams during operation of the hydrostatic seal assembly.
12. The turbine section of claim 7 , including one or more stops formed in the seal shoe configured to limit radial travel of the seal shoe.
13. A gas turbine engine, comprising:
a combustor;
a turbine section in fluid communication with the combustor, the turbine section comprising:
a turbine stator;
a turbine rotor configured to rotate about an engine central longitudinal axis relative to the turbine stator; and
a primary seal configured to maintain a selected gap between the primary seal and the turbine rotor, the primary seal including:
a seal support;
a seal shoe; and
one or more seal beams operably connecting the seal support to the seal shoe, the one or more seal beams configured as spring elements integral with the seal shoe to allow radial movement of the seal shoe relative to the seal support; and
a seal carrier including:
a radial outer wall configured to radially position the primary seal, the seal carrier configured for a non-contact relationship with the seal shoe during operation of the hydrostatic seal assembly; and
an aft wall extending radially inwardly from the radial outer wall;
wherein the aft wall does not radially overlap the one or more seal beams.
14. The gas turbine engine of claim 13 , wherein the aft wall does not extend radially inwardly to a seal shoe radial position.
15. The gas turbine engine of claim 13 , wherein the radial outer wall and the aft wall are formed as a single unitary component.
16. The gas turbine engine of claim 13 , wherein the aft wall is disposed at a first axial end of the seal support and a secondary seal is disposed at a second end of the seal support opposite the first axial end.
17. The gas turbine engine of claim 13 , wherein the seal carrier is configured for a non-contact relationship with one or more seal beams during operation of the hydrostatic seal assembly.