Bearing-raceway systems and methods
A bearing raceway for a shaft includes a tubular sleeve comprising a raceway section and a clamp section, the raceway section having a hardened outer surface and a first, axially linear, inner surface, and the clamp section having first threads and a second, axially non-linear, inner surface, where the first threads are configured to mate with second threads on a nut to clamp the tubular sleeve to the shaft.
1. A bearing raceway for a shaft, the bearing raceway comprising:
a tubular sleeve comprising a raceway section and a clamp section;
the raceway section having a hardened outer surface and a first, axially linear, inner surface, wherein the first, axially linear, inner surface runs an entire length of the raceway section; and
the clamp section having first threads and a second, axially non-linear, inner surface, wherein the second inner surface comprises a first engagement profile, wherein the first engagement profile comprises at least one of a semi-circular groove, a recess and a dimple and is configured to mate with a second engagement profile on the shaft to resist axial movement of the bearing raceway;
wherein the first threads are internal threads and are configured to mate with second threads on a nut to clamp the tubular sleeve to the shaft.
2. The bearing raceway of claim 1 , wherein the clamp section comprises a detent on the second inner surface.
3. The bearing raceway of claim 1 , wherein the clamp section comprises tabs separated by slots.
4. The bearing raceway of claim 3 , wherein the tabs comprise detents on the second inner surface.
5. The bearing raceway of claim 1 , wherein the first engagement profile is positioned between the raceway section and the first threads.
6. The bearing raceway of claim 5 , wherein the first engagement profile comprises a face oriented away from the raceway section toward the first threads.
7. The bearing raceway of claim 5 , wherein a diameter of the clamp section is greater than a diameter of the raceway section.
8. A rotor aircraft mast bearing assembly, comprising:
a bearing raceway secured to a mast of a rotor aircraft, the mast comprising a central axis and a raised portion having a first mast surface that is parallel to the central axis, the bearing raceway comprising a tubular sleeve having a raceway section and a clamp section;
the raceway section having a hardened outer surface and a first, axially linear, inner surface positioned on the first mast surface, wherein the first, axially linear, inner surface runs an entire length of the raceway section;
the clamp section having first threads and a second, axially non-linear, inner surface, wherein the second inner surface comprises a first engagement profile, wherein the first engagement profile comprises at least one of a semi-circular groove, a recess and a dimple and is configured to mate with the raised portion to resist axial movement of the shaft bearing raceway; and
a nut having second threads threaded with the first threads imparting a clamping force to the mast;
wherein the first threads are internal threads.
9. The rotor aircraft mast bearing assembly of claim 8 , wherein the clamp
section comprises a first detent mated with a second detent on the mast.
10. The rotor aircraft mast bearing assembly of claim 8 , wherein the clamp section comprises tabs separated by slots; and
the first thread are on the tabs.
11. The rotor aircraft mast bearing assembly of claim 10 , wherein the tabs comprise first detents mated with a second detent on the mast.
12. The rotor aircraft mast bearing assembly of claim 8 , wherein the first engagement profile is a face oriented away from the raceway section and toward the first threads.