Hydrostatic seal pinned cartridge

1. A seal assembly comprising:

a side ring, wherein the side ring comprises an annular piece of solid material;

a plurality of cartridges affixed to the side ring, wherein each cartridge of the plurality of cartridges includes a discrete module that is disconnected from an adjacent cartridge, wherein each cartridge of the plurality of cartridges comprises:

a shoulder;

a beam connected to and extending from the shoulder;

a shoe attached to an end of the beam; and

a rotary seal disposed on a bottom portion of the shoe; and

a removable pin, wherein the removable pin extends into a portion of one of the plurality of cartridges and into a portion of the side ring such that the cartridge is fastened to the side ring, wherein the side ring has a first hole, wherein the shoulder has a second hole, wherein the second hole is a circular hole disposed in and circumferentially surrounded by physical material of the cartridge, and wherein the removable pin extends into the second hole of the shoulder and into the first hole of the side ring.

2. The seal assembly of claim 1 , wherein each cartridge of the plurality of cartridges comprises an independent unit of 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 secondary seal in contact with a portion of the side ring and the shoe;

a seal cover in contact with a portion of the side ring such that the seal cover retains the secondary seal against the side ring;

a carrier disposed radially outward from all of the plurality of cartridges; and

a seal plate disposed on an axial end of the seal assembly, wherein the seal plate is in contact with the carrier.

5. The seal assembly of claim 1 , wherein each cartridge of the plurality of cartridges is affixed to the side ring via mechanical attachment.

6. The seal assembly of claim 1 , wherein the plurality of cartridges form an annular rotary seal configured to engage with a rotating structure in a seal.

7. 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 side ring with a first axial end-face and a second axial end-face;

a spring affixed to the second end-face of the side ring via a pin;

a shoe disposed radially inward of and connected to the spring;

a plurality of cartridges that form an annular rotary seal configured to sealing engage with the rotating structure, wherein each cartridge of the plurality of cartridges includes a discrete module that is disconnected from an adjacent cartridge;

a seal element extending radially inward from the shoe; and

the pin extending into a portion of the spring and into a portion of the side ring such that the cartridge is fastened to the side ring, wherein the side ring has a first hole, wherein a shoulder of one of the plurality of cartridges has a second hole, wherein the second hole is a circular hole disposed in and circumferentially surrounded by physical material of the one of the plurality of cartridges, wherein the pin affixes the spring to the side ring; and

a carrier disposed radially between and in contact with the static structure and the side ring.

8. The seal assembly of claim 7 , wherein the seal assembly is disposed in a turbine section of the gas turbine engine.

9. The seal assembly of claim 7 , wherein the floating non-contact seal comprises a portion of a hydrostatic seal.

10. The seal assembly of claim 7 , wherein the spring comprises a shoulder and a plurality of beams connected to and extending from the shoulder.

11. The seal assembly of claim 10 , wherein the side ring has a hole, and wherein the pin extends into the shoulder and into the hole of the side ring.

12. A method comprising:

rotating a rotating structure relative to a static structure while providing a seal assembly between the rotating structure and the static structure, the seal assembly comprising:

a side ring with a first axial end-face and a second axial end-face; and

a plurality of floating non-contact seal cartridges disposed radially between the rotating structure and the static structure, wherein each cartridge of the plurality of non-contact seal cartridges includes a discrete module that is disconnected from an adjacent cartridge, wherein each floating non-contact seal cartridge is affixed to the second end-face of the side ring via a pin inserted into portions of the side ring and the floating non-contact seal cartridge, wherein each floating non-contact seal cartridge comprises:

a shoulder, wherein a first portion of the pin is inserted into a first hole in the shoulder, wherein a second portion of the pin is inserted into a second hole in the side ring, wherein the second hole is a circular hole disposed in and circumferentially surrounded by physical material of the cartridge;

a beam extending from the shoulder;

a shoe disposed radially inward of and connected to the beam; and

a seal element extending radially inward from the shoe;

flowing air from an upstream side of the seal assembly, across the plurality of floating non-contact seal cartridges, and to a downstream side of the seal assembly;

actuating the shoe at least one of radially outward and radially inward; and

supporting each floating non-contact seal with a pin.

13. The method of claim 12 , further comprising preventing relative motion between the shoulder of one of the floating non-contact seal cartridges and the side ring with the pin by way of the pin affixing the floating non-contact seal cartridge to the side ring.

14. The method of claim 12 , further comprising holding a radially outward surface of the shoulder against a carrier disposed radially between each of the floating non-contact seal cartridges and the static element.

15. The method of claim 12 , further comprising using the seal assembly within a turbine section of a gas turbine engine.