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US 10,308,356 B2Granted
Axial springs for rotor hub assembly
AssigneeBell Helicopter Textron Inc.
InventorsDalton T Hampton, Thomas Clement Parham, Jr.
Life of this patent
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Abstract
A rotor hub assembly for a rotorcraft includes a yoke forming a bearing bore. The yoke has a teetering axis extending through the bearing bore. The rotor hub assembly includes a flapping bearing disposed in the bearing bore. The flapping bearing is operable to regulate teetering of the yoke about the teetering axis. The rotor hub assembly includes an axial spring abutting the flapping, thereby reducing movement of the flapping bearing along the teetering axis.
Claims15
A rotor hub assembly for a rotorcraft comprising:
- a yoke forming a bearing bore, the yoke having a teetering axis extending through the bearing bore;
- a flapping bearing disposed in the bearing bore, the flapping bearing operable to regulate teetering of the yoke about the teetering axis;
- an axial spring abutting the flapping bearing, thereby reducing movement of the flapping bearing along the teetering axis;
- and
- a retention bracket adapted to secure the axial spring against the flapping bearing, the retention bracket including at least one receiving hole;
- wherein the axial spring further comprises a distal end having an end cap adapted to abut the retention bracket, the end cap structurally separable from the retention bracket and the end cap including at least one boss insertable into the at least one receiving hole of the retention bracket.
3 more elements
A rotor hub assembly for a rotorcraft comprising:
- a yoke forming a bearing bore, the yoke having a plane of rotation and a teetering axis disposed substantially along the plane of rotation and extending through the bearing bore;
- a plurality of rotor blade assemblies coupled to and rotatable with the yoke;
- a flapping bearing assembly disposed in the bearing bore, the flapping bearing assembly including a trunnion having a central mast bore, first and second trunnion arms extending outwardly therefrom substantially along the teetering axis and first and second flapping bearings disposed respectively about the first and second trunnion arms, the flapping bearings operable to regulate teetering of the yoke about the teetering axis;
- first and second axial springs respectively abutting the first and second flapping bearings operable to reduce movement of the yoke along the teetering axis, thereby reducing movement of the flapping bearings along the teetering axis;
- and
- first and second retention brackets coupled to the yoke and respectively securing the first and second axial springs against the first and second flapping bearings, each retention bracket including a pair of receiving holes;
- wherein the first and second axial springs each further comprise a distal end having an end cap adapted to abut a respective one of the retention brackets, each end cap structurally separable from the respective retention bracket and each end cap including a pair of bosses that are insertable into the pair of receiving holes of the respective retention bracket.
4 more elements
A rotorcraft comprising:
- a fuselage;
- a tailboom extending from the fuselage, the tailboom having an aft portion;
- and
- a rotor hub assembly rotatably coupled to the aft portion of the tailboom, the rotor hub assembly comprising:
- a yoke forming a bearing bore, the yoke having a plane of rotation and a teetering axis disposed substantially along the plane of rotation and extending through the bearing bore;
- a plurality of rotor blade assemblies coupled to and rotatable with the yoke;
- a flapping bearing assembly disposed in the bearing bore, the flapping bearing assembly including a trunnion having a central mast bore, first and second trunnion arms extending outwardly therefrom substantially along the teetering axis and first and second flapping bearings disposed respectively about the first and second trunnion arms, the flapping bearings operable to regulate teetering of the yoke about the teetering axis;
- first and second axial springs respectively abutting the first and second flapping bearings operable to reduce movement of the yoke along the teetering axis, thereby reducing movement of the flapping bearings along the teetering axis;
- and
- first and second retention brackets coupled to the yoke and respectively securing the first and second axial springs against the first and second flapping bearings, each retention bracket including a pair of receiving holes;
- wherein the first and second axial springs each further comprise a distal end having an end cap adapted to abut a respective one of the retention brackets, each end cap structurally separable from the respective retention bracket and each end cap including a pair of bosses that are insertable into the pair of receiving holes of the respective retention bracket.
8 more elements
Dependencies are inferred from the claim text.