Spherical mounted cylindrical roller bearing system
A planetary gear system is provided in one example embodiment and may include a planet gear further comprising a bearing system, the bearing system further comprising an inner bearing assembly comprising a spherical bearing and an outer race; an outer bearing assembly comprising a plurality of cylindrical roller bearings, an inner race, and an outer race; and a race element comprising an inner surface and an outer surface, wherein the outer surface of the race element is the inner race for the outer bearing assembly and the inner surface of the race element is associated with the outer race for the inner bearing assembly.
1. A planetary gear system, comprising:
a planet gear further comprising a bearing system, the bearing system further comprising:
an inner bearing assembly comprising a spherical bearing and an outer race;
an outer bearing assembly comprising a plurality of cylindrical roller bearings, an inner race, and an outer race; and
a race element comprising an inner surface and an outer surface, wherein the outer surface of the race element is the inner race for the outer bearing assembly and the inner surface of the race element is associated with the outer race for the inner bearing assembly.
2. The planetary gear system of claim 1 , wherein the inner bearing assembly allows tilting movements of the planet gear.
3. The planetary gear system of claim 1 , wherein the outer bearing assembly allows rotational movements for the planet gear and supports, at least in part, radial loads for the planet gear.
4. The planetary gear system of claim 1 , wherein the outer race of the inner bearing assembly is integral with the race element.
5. The planetary gear system of claim 1 , wherein the outer race for the outer bearing assembly is backup material of the planet gear.
6. The planetary gear system of claim 1 , wherein the race element further comprises:
an outer shoulder associated with the outer surface of the race element that maintains alignment of the plurality of cylindrical roller bearings with the inner race of the outer bearing assembly; and
an outer structural element associated with the outer surface of the race element that is to receive a retaining device.
7. The planetary gear system of claim 6 , wherein the retaining device secures the plurality of cylindrical roller bearings to the inner race of the outer bearing assembly and wherein the inner race of the outer bearing assembly provides a clearance distance that allows axial movements of the plurality of cylindrical roller bearings along the inner race.
8. The planetary gear system of claim 1 , wherein the spherical bearing comprises an inner diameter to facilitate mounting the bearing system on a post.
9. The planetary gear system of claim 1 , further comprising a carrier that comprises a plurality of carrier posts.
10. The planetary gear system of claim 9 , further comprising:
a sun gear;
a ring gear, wherein the planet gear is one of a plurality planet gears of the planetary gear system, wherein each planet gear is mounted to each carrier post of the plurality of carrier posts.
11. An aircraft, comprising:
a fuselage; and
at least one propulsion system, the at least one propulsion system comprising at least one planetary gear system, the at least one planetary gear system further comprising a plurality of planet gears, wherein each planet gear further comprises a bearing system, the bearing system of each planet gear further comprising:
an inner bearing assembly comprising a spherical bearing and an outer race;
an outer bearing assembly comprising a plurality of cylindrical roller bearings, an inner race, and an outer race; and
a race element comprising an inner surface and an outer surface, wherein the outer surface of the race element is the inner race for the outer bearing assembly and the inner surface of the race element is associated with the outer race for the inner bearing assembly.
12. The aircraft of claim 11 , wherein the inner bearing assembly of each bearing system allows tilting movements for each planet gear.
13. The aircraft of claim 11 , wherein the outer bearing assembly of each bearing system allows rotational movements for each planet gear and supports, at least in part, radial loads for each planet gear.
14. The aircraft of claim 11 , wherein the aircraft is a tiltrotor aircraft comprising at least two propulsion systems having proprotors that are moveable between a helicopter mode and an airplane mode.
15. The aircraft of claim 11 , wherein the aircraft is a rotorcraft.
16. The aircraft of claim 11 , wherein the outer race of the inner bearing assembly is integral with the race element.
17. The aircraft of claim 11 , wherein the outer race for the outer bearing assembly is backup material of the planet gear.
18. The aircraft of claim 11 , wherein the race element further comprises:
an outer shoulder associated with the outer surface of the race element that maintains alignment of the plurality of cylindrical roller bearings with the inner race of the outer bearing assembly; and
an outer structural element associated with the outer surface of the race element that is to receive a retaining device.
19. The aircraft of claim 18 , wherein the retaining device secures the plurality of cylindrical roller bearings to the inner race of the outer bearing assembly and wherein the inner race of the outer bearing assembly provides a clearance distance that allows axial movements of the plurality of cylindrical roller bearings along the inner race.
20. The aircraft of claim 11 , wherein the spherical bearing comprises an inner diameter to facilitate mounting the bearing system on a post.