Carbon seal spring assembly
A carbon seal assembly for a gas turbine engine is disclosed. The carbon seal assembly includes a first carbon seal. The carbon seal assembly also includes a first carbon seal spring configured to provide force against the first carbon seal in a first axial direction, the first carbon seal spring having an annular shape and circumferentially disposed around a first shaft of the gas turbine engine.
1. A gas turbine engine comprising:
a first carbon seal configured to form a seal against a first rotating shaft of the gas turbine engine, wherein the first rotating shaft has a first diameter;
a second carbon seal configured to form a seal against a second rotating shaft of the gas turbine engine, wherein the second rotating shaft has a second diameter that is different than the first diameter;
a mating hardware disposed between the first carbon seal and the second carbon seal;
a first carbon seal spring configured to provide force against the first carbon seal in a first axial direction and provide force against the mating hardware in a second axial direction opposite the first axial direction, the first carbon seal spring having an annular shape and circumferentially disposed around the first rotating shaft of the gas turbine engine; and
a second carbon seal spring having the annular shape, circumferentially disposed around the second rotating shaft of the gas turbine engine, and configured to provide force against the second carbon seal in the second axial direction and configured to provide force against the mating hardware in the first axial direction.
2. The gas turbine engine of claim 1 , wherein the first carbon seal spring is a wave spring, a bellows spring, a large diameter coil spring, a large diameter tapered coil spring, or a diaphragm spring.
3. The gas turbine engine of claim 1 , wherein the second carbon seal spring is a wave spring, a bellows spring, a large diameter coil spring, a large diameter tapered coil spring, or a diaphragm spring.
4. The gas turbine engine of claim 1 , wherein the first carbon seal spring and the second carbon seal spring are a same type of spring.
5. The gas turbine engine of claim 1 , wherein the first carbon seal spring and the second carbon seal spring are a different type of spring.
6. The gas turbine engine of claim 1 , wherein the mating hardware comprises:
a first retention surface disposed radially between the first carbon seal spring and the first rotating shaft; and
a second retention surface disposed radially between the second carbon seal spring and the second shaft.
7. The gas turbine engine of claim 6 , wherein the first retention surface is disposed radially outward of the second retention surface.
8. The gas turbine engine of claim 1 , wherein the mating hardware is disposed radially outward of and extends axially across a transition from the first diameter to the second diameter.