Low friction carbon—carbon seal assembly
A seal assembly for a gas turbine engine, having a seal formed of a carbon material; and a seal seat positioned for rotation relative to the seal, wherein the seal and the seal seat each have a sealing surface which together define a sliding seal, and wherein at least the sealing surface of the seal seat is made of the same carbon material as the sealing surface of the seal.
1. A seal assembly for a gas turbine engine, comprising:
a seal comprising a carbon material; and
a seal seat positioned for rotation relative to the seal, wherein the seal and the seal seat are mounted between a rotational shaft and stationary structure of the gas turbine engine, and each of the seal and the seal seat have a sealing surface which together define a sliding seal, and wherein at least the sealing surface of the seal seat is made of the same carbon material as the sealing surface of the seal, wherein the seal seat has a recessed area, and a carbon-based block mounted in the recess, the carbon-based block defining the sealing surface of the seal seat, and wherein the sealing surfaces of the seal and the seal seat are the same material selected from the group consisting of electrographitic grade carbon, carbon-graphite grade carbon, and combinations thereof.
2. The seal assembly of claim 1 , wherein the seal seat comprises carbon-based material matching the seal.
3. The seal assembly of claim 1 , wherein the sealing surfaces of the seal and the seal seat define a coefficient of friction of less than 0.1.
4. The seal assembly of claim 1 , wherein the sealing surfaces of the seal and the seal seat are the same electrographitic grade carbon.
5. The seal assembly of claim 1 , wherein the sealing surfaces define an oil seal between the rotational shaft and the stationary structure of the gas turbine engine.
6. The seal assembly of claim 1 , further comprising film controllers in the seal to control formation of transfer film on the seal seat.
7. The seal assembly of claim 1 , wherein the seal and the seal seat can be moved relative to each other with no break-in phase.
8. The seal assembly of claim 1 , wherein the sealing surface of the seal and the sealing surface of the seal seat are flat radial surfaces with respect to an axis of rotation of the gas turbine engine.
9. The seal assembly of claim 8 , wherein the sliding seal is defined along a single contact plane of the sealing surface of the seal seat and the sealing surface of the seal.