Helicopter rotor damper

• US 5,372,478 A
• Filed: 02/04/1993
• Issued: 12/13/1994
• Est. Priority Date: 02/04/1993
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: McCafferty, Hugh A.
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): Sgantzos, Mark
• Application Number:
  US08/013,367
• Time in Patent Office: 677 Days
• Field of Search: 416/106, 416/107, 416/134 A, 416/140, 416/244 D
• US Class Current: 416/106
• CPC Class Codes: B64C 27/51 Damping of blade movements

Abstract

A hollow rotor hub is provided at the top of the rotor shaft for a multi-bladed helicopter. The blades being mounted to the rotor hub on spherical elastomeric bearings which provide for coincident rotor blade hinges for blade pitch, flap and lead-lag motions. The invention discloses a lead-lag damper contained in a housing at the center of the hollow rotor hub. The damper consists of a series of damping plates, each plate being connected to one of the rotor blades. The damping plates are separated from each other and from the damper housing by elastomeric layers bonded to the plates and to the housing. Lead-lag damping is provided by the shear in the elastomeric layers. The damper may be fastened to the air frame in a conventional manner, it may be mounted on a spindle for rotation about the rotor axis independent of rotor shaft rotation or may be free-floating and attached only to the rotor blades and not to the rotor shaft. With suitable selection of elastomeric damping material properties, it can provide blade to hub damping, blade to blade damping or combinations thereof.

Claims

1. A rotor hub for a helicopter rotor rotatable about a rotor axis,said hub comprising;

a rotor shaft having a central opening at its upper end and extending at least partially through its length along the rotor axis;

a plurality of rotor blades attached to said rotor shaft and rotatable therewith about the rotor axis;

spherical bearing means for attaching said rotor blades to said rotor shaft, said spherical bearings providing for motion of said blades in blade pitch, flap and lead-lag directions, the hinge points of said motions being coincident in the spherical bearing;

a damper assembly assembled in the central opening of said rotor shaft for providing damping in the lead-lag direction, said damper comprising;

a damper housing assembled in said rotor shaft and centered on the rotor axis said housing being a hollow structure having upper and lower walls;

a plurality of damper plates mounted in said damper housing, one plate being provided for each of said rotor blades;

elastomeric material assembled between said plates and between said plates and the damper housing;

means for attaching each of said blades to a separate one of said damper plates.

2. A rotor hub according to claim 1 wherein said damper plates are circular plates having their center coincident with said rotor axis, said damper plates being stacked one on top of the other in concentric layers, said elastomeric material between said plates being bonded to its adjacent plates and an elastomeric layer being bonded to the top surface of the top damper plate and to the inside surface of the upper wall of said housing and an elastomeric layer bonded to the bottom surface of the lowest damper plate and the inner surface of the lower wall of said housing.

3. A rotor hub according to claim 1 wherein said damper plates are approximately semi-circular plates having their circle center coincident with said rotor axis, said damper plates being stacked one on top of the other in concentric layers, each layer containing two damper plates forming a circular structure, said elastomeric material between said plates being bonded to its adjacent plates and an elastomeric layer being bonded to the top surface of the top damper plate and to the inside surface of the upper wall of said housing and an elastomeric layer bonded to the bottom surface of the lowest damper plate and the inner surface of the lower wall of said housing.

4. A rotor hub according to claim 1 wherein said damper plates are approximately quarter circle plates having their circle center coincident with said rotor axis, said damper plates being assembled in a single layer containing four damper plates forming a circular structure, said elastomeric material between said plates being bonded to its adjacent plates and an elastomeric layer being bonded to the top surface of the damper plates and to the inside surface of the upper wall of said housing and an elastomeric layer bonded to the bottom surface of the damper plates and the inner surface of the lower wall of said housing.

5. A rotor hub for a helicopter rotor according to claim and further comprising means for attaching said damper housing to said rotor shaft for rotation therewith.

6. A rotor hub according to claim 5 wherein said damper plates are circular plates having their center coincident with said rotor axis, said damper plates being stacked one on top of the other in concentric layers, said elastomeric material between said plates being bonded to its adjacent plates and an elastomeric layer being bonded to the top surface of the top damper plate and to the inside surface of the upper wall of said housing and an elastomeric layer bonded to the bottom surface of the lowest damper plate and the inner surface of the lower wall of said housing.

7. A rotor hub according to claim 5 wherein said damper plates are approximately semi-circular plates having their circle center coincident with said rotor axis, said damper plates being stacked one on top of the other in concentric layers, each layer containing two damper plates forming a circular structure, said elastomeric material between said plates being bonded to its adjacent plates and an elastomeric layer being bonded to the top surface of the top damper plate and to the inside surface of the upper wall of said housing and an elastomeric layer bonded to the bottom surface of the lowest damper plate and the inner surface of the lower wall of said housing.

8. A rotor hub according to claim 5 wherein said damper plates are approximately quarter circle plates having their circle center coincident with said rotor axis, said damper plates being assembled in a single layer containing four damper plates forming a circular structure, said elastomeric material between said plates being bonded to its adjacent plates and an elastomeric layer being bonded to the top surface of the damper plates and to the inside surface of the upper wall of said housing and an elastomeric layer bonded to the bottom surface of the damper plates and the inner surface of the lower wall of said housing.

9. A rotor hub for a helicopter rotor rotatable about a rotor axis, said hub comprising;

a rotor shaft having a central opening at its upper end and extending at least partially through its length along the rotor axis;

a plurality of rotor blades attached to said rotor shaft and rotatable therewith about the rotor axis;

spherical bearing means for attaching said rotor blades to said rotor shaft, said spherical bearings providing for motion of said blades in blade pitch, flap and lead-lag directions, the hinge points of said motions being coincident in the spherical bearing;

a damper assembly assembled in the central opening of said rotor shaft for providing damping in the lead-lag direction, said damper comprising;

a damper housing assembled in said rotor shaft and centered on the rotor axis said housing being a hollow structure having upper and lower walls;

a plurality of damper plates mounted in said damper housing, one plate being provided for each of said rotor blades;

elastomeric material assembled between said plates and between said plates and the damper housing;

means for attaching each of said blades to one of said damper plates;

a spindle attached to said rotor shaft for rotation therewith; and

means for mounting said damper housing on said spindle for rotation on said spindle about the rotor axis independent of the rotation of said rotor shaft.

10. A rotor hub according to claim 9 wherein said damper plates are circular plates having their center coincident with said rotor axis, said damper plates being stacked one on top of the other in concentric layers, said elastomeric material between said plates being bonded to its adjacent plates and an elastomeric layer being bonded to the top surface of the top damper plate and to the inside surface of the upper wall of said housing and an elastomeric layer bonded to the bottom surface of the lowest damper plate and the inner surface of the lower wall of said housing.

11. A rotor hub according to claim 9 wherein said damper plates are approximately semi-circular plates having their circle center coincident with said rotor axis, said damper plates being stacked one on top of the other in concentric layers, each layer containing two damper plates forming a circular structure, said elastomeric material between said plates being bonded to its adjacent plates and an elastomeric layer being bonded to the top surface of the top damper plate and to the inside surface of the upper wall of said housing and an elastomeric layer bonded to the bottom surface of the lowest damper plate and the inner surface of the lower wall of said housing.

12. A rotor hub according to claim 9 wherein said damper plates are approximately quarter circle plates having their circle center coincident with said rotor axis, said damper plates being assembled in a single layer containing four damper plates forming a circular structure, said elastomeric material between said plates being bonded to its adjacent plates and an elastomeric layer being bonded to the top surface of the damper plates and to the inside surface of the upper wall of said housing and an elastomeric layer bonded to the bottom surface of the damper plates and the inner surface of the lower wall of said housing.