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On example of a rotorcraft bearing system includes a bearing housing attached to an elastomeric bearing on a longitudinal axis, an end surface of the elastomeric bearing attached to an end surface of the bearing housing. The rotorcraft bearing system also includes a sliding contact bearing having an

On example of a rotorcraft bearing system includes a bearing housing attached to an elastomeric bearing on a longitudinal axis, an end surface of the elastomeric bearing attached to an end surface of the bearing housing. The rotorcraft bearing system also includes a sliding contact bearing having an end surface. The rotorcraft bearing system also includes an intermediate sliding contact bearing material layer. Under load on the longitudinal axis, the end surface of the sliding contact bearing is configured to contact an opposing end surface of the bearing housing through the intermediate sliding contact bearing material layer to form a rotational slip joint.

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1. A rotorcraft bearing system comprising: a bearing housing attached to an elastomeric bearing on a longitudinal axis, an end surface of the elastomeric bearing attached to an end surface of the bearing housing;a sliding contact bearing having an end surface; andan intermediate sliding contact bear

1. A rotorcraft bearing system comprising: a bearing housing attached to an elastomeric bearing on a longitudinal axis, an end surface of the elastomeric bearing attached to an end surface of the bearing housing;a sliding contact bearing having an end surface; andan intermediate sliding contact bearing material on the end surface of the sliding contact bearing, wherein, under no load on the longitudinal axis, the intermediate sliding contact bearing material is untouched by the bearing housing, and wherein, under load on the longitudinal axis, the intermediate sliding contact bearing material is configured to touch an opposing end surface of the bearing housing to form a rotational slip joint. 2. The rotorcraft bearing system of claim 1, wherein the opposing end surface of the bearing housing includes a polished surface. 3. The rotorcraft bearing system of claim 2, wherein the intermediate sliding contact bearing material is attached to the end surface of the sliding contact bearing. 4. The rotorcraft bearing system of claim 1, wherein the end surface of the sliding contact bearing includes a polished surface. 5. The rotorcraft bearing system of claim 4, wherein the intermediate sliding contact bearing material is attached to the opposing end surface of the bearing housing. 6. The rotorcraft bearing system of claim 1, wherein the sliding contact bearing material includes a frictional material. 7. The rotorcraft bearing system of claim 6, wherein the sliding contact bearing material includes at least one of tetrafluoroethylene (TFE), PEEK, or brass. 8. The rotorcraft bearing system of claim 1, further comprising an intermediate polymer layer between the intermediate sliding contact bearing material layer and the elastomeric bearing. 9. The rotorcraft bearing system of claim 8, wherein the intermediate polymer layer includes rubber. 10. The rotorcraft bearing system of claim 8, wherein the intermediate polymer layer is attached to and touches the end surface of the bearing housing. 11. The rotorcraft bearing system of claim 1, further comprising a retaining member attached to the bearing housing and configured to couple with the sliding contact bearing to prevent the bearing housing and the sliding contact bearing from separating when the load on the longitudinal axis is removed. 12. The rotorcraft bearing system of claim 11, wherein the retaining member comprises: a retaining ring; anda hook member attached to the retaining ring, the hook member configured to be received by a recess in the bearing housing. 13. The rotorcraft bearing system of claim 12, wherein the retaining ring is attached to the bearing housing. 14. The rotorcraft bearing system of claim 1, wherein the bearing housing and the sliding contact bearing surround and define a spindle hole configured to receive a spindle. 15. A rotorcraft bearing system comprising: a bearing housing attached to an elastomeric bearing on a longitudinal axis, an end surface of the elastomeric bearing attached to an end surface of the bearing housing; anda sliding contact bearing having an end surface attached to and touching a sliding contact bearing material, wherein, under no load on the longitudinal axis, the end surface of the sliding contact bearing is configured to define a gap between the sliding contact bearing and the bearing housing, and the bearing housing is configured to be untouched by the sliding contact bearing material, and wherein, under load on the longitudinal axis, the end surface of the sliding contact bearing is configured to contact an opposing end surface of the bearing housing through the sliding contact bearing material layer to form a rotational slip joint. 16. The rotorcraft bearing system of claim 15, wherein the opposing end surface of the bearing housing includes a polished surface. 17. The rotorcraft bearing system of claim 15, wherein the sliding contact bearing material includes at least one of tetrafluoroethylene (TFE), PEEK, or brass. 18. The rotorcraft bearing system of claim 15, wherein the opposing end surface of the bearing housing and the end surface of the sliding contact bearing are the same material. 19. The rotorcraft bearing system of claim 15, further comprising a retaining member attached to the bearing housing and configured to couple with the sliding contact bearing to prevent the bearing housing and the sliding contact bearing from separating when the load on the longitudinal axis is removed wherein the retaining member comprises: a retaining ring; anda hook member attached to the retaining ring, the hook member configured to be received by a recess in the bearing housing. 20. A rotorcraft bearing system comprising: a sliding contact bearing, wherein a first end surface of the sliding contact bearing touches a sliding contact material; anda bearing housing attached to an elastomeric bearing on a longitudinal axis, a first end surface of the elastomeric bearing attached to a first end surface of the bearing housing, wherein, under no load on the longitudinal axis, the sliding contact material is spaced apart from the second end surface of the sliding contact bearing housing to define a gap between the bearing housing and the material, and under load on the longitudinal axis, the sliding contact material is configured to touch the second end surface of the bearing housing to form a rotational slip joint.