Axial springs for rotor hub assembly

Patent metadata

Field	Value
Publication number	US-10308356-B2
Application number	US-201615359594-A
Country	US
Kind code	B2
Filing date	Nov 22, 2016
Priority date	Nov 22, 2016
Publication date	Jun 4, 2019
Grant date	Jun 4, 2019

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.

First claim

What is claimed is:

1. 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.

2. The rotor hub assembly as recited in claim 1 wherein the axial spring further comprises a plurality of alternating metallic and elastomeric layers.

3. The rotor hub assembly as recited in claim 1 wherein the axial spring further comprises a plurality of substantially circular metallic and elastomeric bodies arranged in alternating layers.

4. The rotor hub assembly as recited in claim 1 further comprising:
a mast;
wherein, the yoke forms a mast bore adapted to receive the mast therethrough; and
wherein, the mast is substantially perpendicular to the teetering axis.

5. The rotor hub assembly as recited in claim 1 wherein the retention bracket is adapted to be coupled to the yoke.

6. The rotor hub assembly as recited in claim 1 wherein the retention bracket further comprises a raised central portion.

7. The rotor hub assembly as recited in claim 1 wherein the at least one boss further comprises a safety hole adapted to receive a safety wire to prevent the at least one boss from disengaging with the at least one receiving hole.

8. The rotor hub assembly as recited in claim 1 wherein the yoke is rotatable in a plane of rotation; and
wherein the teetering axis is disposed substantially along the plane of rotation.

9. The rotor hub assembly as recited in claim 1 further comprising:
a flapping bearing assembly disposed in the bearing bore comprising:
a trunnion having a central mast bore and first and second trunnion arms extending outwardly therefrom substantially along the teetering axis;
the flapping bearing disposed about the first trunnion arm; and
a second flapping bearing disposed about the second trunnion arm.

10. The rotor hub assembly as recited in claim 1 further comprising:
a plurality of rotor blade assemblies coupled to the yoke.

11. The rotor hub assembly as recited in claim 10 wherein the yoke further comprises a central portion and a pair of oppositely disposed end portions, the pair of oppositely disposed end portions each coupled to one of the plurality of rotor blade assemblies.

12. 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.

13. The rotor hub assembly as recited in claim 12 wherein each of the axial springs further comprises a plurality of alternating metallic and elastomeric layers.

14. The rotor hub assembly as recited in claim 12 wherein each of the axial springs further comprises a plurality of substantially circular metallic and elastomeric bodies arranged in alternating layers.

15. 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.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Hampton Dalton T
• Parham Jr Thomas Clement

Classifications

• B64C27/82

  characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft · CPC title

• B64C27/35

  having elastomeric joints · CPC title

• B64C27/43 Primary

  see-saw type, i.e. two-bladed rotor · CPC title

• B64C27/32 Primary

  Rotors · CPC title

• B64C27/78

  in association with pitch adjustment of blades of anti-torque rotor · CPC title