Segmented air floating seal

• US 20060249912A1
• Filed: 07/15/2005
• Published: 11/09/2006
• Est. Priority Date: 05/05/2005
• Status: Abandoned Application

• Current Assignee: Jack W. Wilson Jr
• Original Assignee: Jack W. Wilson Jr
• Inventors: Wilson, Jack W. Jr.
• Application Number:
  US11/183,275
• Publication Number:
  US 20060249912A1
• Time in Patent Office: Days
• US Class Current: 277/409
• CPC Class Codes: F16J 15/442 segmented

Abstract

A segmented floating seal assembly used in a gas turbine engine to seal a rotary shaft. The segmented seal is made from a fiber reinforced ceramic matrix composite (FRCMC) material having a polymer-derived pre-ceramic resin in its ceramic state, fibers of Nextel, and a filler material. The seal segments are secured to respective support plates, and the support plates are each biased by a spring member secured to a support ring mounted in the engine. The material in the seal segments are resistive to very high temperatures, are not brittle, allow little flow across the seal face, and durable.

Claims

1. A seal assembly to provide a seal against a rotary shaft, comprising:

a support ring;

a plurality of bias members each connected to the support ring;

a plurality of support plates, each support plates being connected to a respective bias member;

a plurality of seal segments, each seal segment being connected to a respective support plate, each seal segment having a curved seal face of substantially the same radius as the rotary shaft; and

,

the seal segments being made of a fiber reinforced ceramic matrix composite material.

2. The seal assembly of claim 1, and further comprising:

The fiber reinforced ceramic matrix composite material includes a pre-ceramic resin in its ceramic state, and fibers.

3. The seal assembly of claim 2, and further comprising:

the pre-ceramic resin is a polymer-derived pre-ceramic resin.

4. The seal assembly of claim 3, and further comprising:

the polymer-derived pre-ceramic resin is one of silicon-carboxyl resin and alumina silicate resin.

5. The seal assembly of claim 1, and further comprising:

The fibers are comprised of one or more of alumina, Nextel 312, Nextel 440, Nextel 510, Nextel 550, silicon nitride, silicon carbide, HPZ, graphite, carbon, and peat.

6. The seal assembly of claim 5, and further comprising:

The fibers being in the form of non-continuous, loose fibers having lengths of about 0.2 to 5.0 inches.

7. The seal assembly of claim 6, and further comprising:

The fibers comprise a volume percent of about 15 to 60 percent

8. The seal assembly of claim 1, and further comprising:

The seal segments also being made of a filler material, the filler material comprising one of alumina, mullite, silica, silicon carbide, titania, silicon nitride, boron nitride, carbon, magnesium oxide, and boron carbide.

9. The seal assembly of claim 8, and further comprising:

The filler material comprises a volume percent of about 0 to 50 percent.

10. The seal assembly of claim 4, and further comprising:

The fibers are comprised of one or more of alumina, Nextel 312, Nextel 440, Nextel 510, Nextel 550, silicon nitride, silicon carbide, HPZ, graphite, carbon, and peat.

11. The seal assembly of claim 10, and further comprising:

The fibers being in the form of non-continuous, loose fibers having lengths of about 0.2 to 5.0 inches.

12. The seal assembly of claim 11, and further comprising:

The fibers comprise a volume percent of about 15 to 60 percent

13. The seal assembly of claim 12, and further comprising:

The seal segments also being made of a filler material, the filler material comprising one of alumina, mullite, silica, silicon carbide, titania, silicon nitride, boron nitride, carbon, magnesium oxide, and boron carbide.

14. a process for sealing a rotary shaft in a gas turbine engine, comprising the steps of:

providing for a plurality of seal segments around the rotary shaft;

providing for a support plate to support each of the seal segments;

providing for a bias means connected to each of the support plates; and

,

providing for the seal segments to be made from a fiber reinforced ceramic matrix composite material.

15. The process for sealing a rotary shaft of claim 14, and further comprising the steps of:

Providing for the fiber reinforced ceramic matrix composite material to be a pre-ceramic resin in its ceramic state, and fibers.

16. The process for sealing a rotary shaft of claim 15, and further comprising the steps of:

Providing for the pre-ceramic resin to be a polymer-derived pre-ceramic resin.

17. The process for sealing a rotary shaft of claim 16, and further comprising the steps of:

Providing for the polymer-derived pre-ceramic resin to be one of silicon-carboxyl resin and alumina silicate resin.

18. The process for sealing a rotary shaft of claim 17, and further comprising the steps of:

Providing for the fibers to be comprised of one or more of alumina, Nextel 312, Nextel 440, Nextel 510, Nextel 550, silicon nitride, silicon carbide, HPZ, graphite, carbon, and peat.

19. The process for sealing a rotary shaft of claim 18, and further comprising the steps of:

Providing for the fibers to be in the form of non-continuous, loose fibers having lengths of about 0.2 to 5.0 inches.

20. The process for sealing a rotary shaft of claim 19, and further comprising the steps of:

Providing for the fiber reinforced ceramic matrix composite material to include a filler material, the filler material comprising one of alumina, mullite, silica, silicon carbide, titania, silicon nitride, boron nitride, carbon, magnesium oxide, and boron carbide.