Bellows preload and centering spring for a fan drive gear system
An assembly includes a first tapered roller bearing and a second tapered roller bearing and a bellows spring. The bellows spring is disposed adjacent the first tapered roller bearing and the second tapered roller bearing.
1. An assembly comprising:
a first tapered roller bearing, wherein the first tapered roller bearing has an outer race;
a second tapered roller bearing;
a bearing support disposed adjacent the second tapered roller bearing; and
a bellows spring disposed adjacent the first tapered roller bearing and the second tapered roller bearing, wherein the bellows spring is snapped into an interference fit with the outer race of the first tapered roller bearing, and wherein the bellows spring is snapped into an interference fit with the bearing support.
2. The assembly of claim 1 , further comprising a shim disposed between the bellows spring and the bearing support.
3. The assembly of claim 1 , wherein the bellows spring comprises a corrugated single piece annular ring.
4. The assembly of claim 3 , wherein the bellows spring comprises a steel.
5. The assembly of claim 3 , wherein the bellows spring has a cross-sectional thickness that is variable as the bellows spring extends axially along an engine centerline.
6. The assembly of claim 1 , further comprising a spacer that is disposed between an inner race of the first tapered roller bearing and an inner race of the second tapered roller bearing.
7. A gas turbine engine, comprising:
a bearing support mounted within the gas turbine engine;
a shaft rotatably mounted within the gas turbine engine adjacent the bearing support;
a first tapered roller bearing and a second tapered roller bearing disposed between the shaft and the bearing support, wherein the first tapered roller bearing has an outer race and the bearing support is disposed adjacent the second tapered roller bearing; and
a bellows spring positioned adjacent the first tapered roller bearing and the second tapered roller bearing within a bearing compartment, wherein the bellows spring is snapped into an interference fit with the outer race of the first tapered roller bearing, and wherein the bellows spring is snapped into an interference fit with the bearing support.
8. The gas turbine engine of claim 7 , wherein a bearing support is disposed adjacent the first tapered roller bearing and is contacted by the bellows spring.
9. The gas turbine engine of claim 7 , wherein the bellows spring comprises a corrugated single piece annular ring.
10. The gas turbine engine of claim 9 , wherein the bellows spring comprises a steel.
11. The gas turbine engine of claim 9 , wherein the bellows spring has a cross-sectional thickness that is variable as the bellows spring extends axially along an engine centerline.
12. The gas turbine engine of claim 7 , further comprising a secondary sleeve disposed between the first tapered roller bearing and the bearing support.
13. The gas turbine engine of claim 7 , further comprising a squeeze film damper positioned between the first roller bearing and the bearing support to reduce shaft vibration and instability.
14. The gas turbine engine of claim 7 , further comprising a spacer that is disposed between an inner race of the first tapered roller bearing and an inner race of the second tapered roller bearing.
15. A method of applying a preload to a first tapered roller bearing and a second tapered roller bearing, the method comprising:
disposing the first tapered roller bearing within a bearing compartment;
positioning the second tapered roller bearing adjacent the first tapered roller bearing within the bearing compartment; and
disposing a bellows spring within the bearing compartment between the first tapered roller bearing and the second tapered roller bearing to apply the preload to both the first tapered roller bearing and the second tapered roller bearing;
snapping the bellows spring into an interference fit with an outer race of the first tapered roller bearing; and
snapping the bellows spring into an interference fit with a bearing support that is disposed adjacent the second tapered roller bearing, wherein the bellows spring applies preload in an axial direction with respect to an engine centerline and is accommodating of flexing in a radial direction with respect to the engine centerline by the first tapered roller bearing and the second tapered roller bearing.
16. The method of claim 15 , further comprising a bearing support disposed adjacent the first tapered roller bearing, the bellows spring applies preload to the bearing support which transfers the preload to the second tapered roller bearing.