Mast bearing race

1. A mast bearing race, comprising:

a rotor aircraft mast having a central axis with a raised portion, the raised portion comprising an outer surface generally parallel to the central axis and a first side and a second side on opposite sides of the raised portion;

an outer race comprising a bearing surface on an inner face of the outer race;

an inner race comprising a bearing surface on an outer face of the inner race and a first angled face on an inner face of the inner race, the inner race positioned on the raised portion with the first angled face abutting the first side;

a nut having a second angled face abutting the second side and an outer threaded portion threadedly connected to the inner face of the of the inner race; and

a plurality of rollers disposed between the inner and outer races, each roller of the plurality of rollers being in contact with the bearing surfaces of the outer and inner races.

2. The mast bearing race of claim 1 , wherein the first angled face of the inner race and the second angled face of the nut are angled between 40°-50° relative to the central axis.

3. The mast bearing race of claim 1 , wherein the inner race comprises a plurality of castellations on an axial face of the inner race.

4. The mast bearing race of claim 1 , wherein the nut comprises a plurality of castellations on an axial face of the nut.

5. The mast bearing race of claim 1 , wherein the outer race includes side walls configured to retain the plurality of rollers between the inner and outer races.

6. A bearing system comprising:

a shaft comprising a raised portion extending radially outward, the raised portion comprising a first angled face on a first side of the raised portion and a second angled face on a second side of the raised portion;

a bearing comprising:

an outer race comprising a bearing surface on an inner face of the outer race;

an inner race comprising a bearing surface on an outer face of the inner race and a third angled face on an inner face of the inner race that is configured to mate with the first angled face; and

a plurality of rollers disposed between the inner and outer races, each roller of the plurality of rollers being in contact with the bearing surfaces of the outer and inner races.

7. The bearing system of claim 6 , wherein a diameter of the inner race is smaller than an outer diameter of the raised portion.

8. The bearing system of claim 6 , comprising:

a nut comprising a fourth angled face on an inner surface of the nut and a threaded portion on an outer surface of the nut;

wherein the inner face of the inner race comprises a threaded portion; and

wherein the threaded portion of the nut is configured to engage the threaded portion of the inner race.

9. The bearing system of claim 8 , wherein the third angled face and the fourth angled face are angled between 40°-50° relative to a central axis passing through the shaft.

10. The bearing system of claim 8 , wherein the nut comprises a plurality of castellations on an axial face of the nut.

11. The bearing system of claim 6 , wherein the inner race comprises a plurality of castellations on an axial face of the inner race.

12. The bearing system of claim 6 , wherein the outer race includes side walls that retain the plurality of rollers between the inner and outer races.

13. The bearing system of claim 6 , wherein the shaft is a mast of a rotor aircraft.

14. A method of securing a bearing onto a shaft, the method comprising:

sliding the bearing onto a first end of the shaft until an inner race of the bearing meets a raised portion of the shaft;

forcing the bearing onto the raised portion to form a press fit between the bearing and the raised portion, wherein an angled face on an inner face of the inner race contacts a first angled face of the raised portion;

sliding a nut onto a second end of the shaft until the nut abuts the inner race of the bearing; and

rotating the nut to engage threads of the nut with threads of the inner race and to secure the bearing to the shaft, when the bearing is secured to the saft an angled face on an inner face of the inner race contacts a first angled face of the raised portion and an angled face on an inner face of the nut contacts a second angled face of the raised portion.

15. The method of claim 14 , wherein the rotating the nut to engage the threads of the nut with the threads of the inner race causes the angled face of the inner race and the angled face of the nut to generate a clamping force between angled faces of the inner race and the nut that locks the bearing onto the shaft.

16. The method of claim 14 , wherein the inner race comprises a plurality of castellations on an axial face of the inner race.

17. The method of claim 14 , wherein the nut comprises a plurality of castellations on an axial face of the nut.

18. The method of claim 14 , wherein the shaft is a mast of a rotor aircraft.