Elastomeric bearing system motion limiter

Patent metadata

Field	Value
Publication number	US-9884680-B2
Application number	US-200813139015-A
Country	US
Kind code	B2
Filing date	Dec 11, 2008
Priority date	Dec 11, 2008
Publication date	Feb 6, 2018
Grant date	Feb 6, 2018

Abstract

The invention relates to a backing plate used for an elastomeric bearing system, the backing plate comprising a plate which defines an at least partial annulus about an axis, a motion limiter and a redundant pivot which extend from the plate so as to respond to a retainer plate disbond.

First claim

What is claimed is:

1. A tail rotor blade assembly comprising:
a flexbeam;
a torque tube defined at least partially around said flexbeam;
a retainer mounted to said flexbeam;
an elastomeric bearing having an inner race and an outer race defined along an axis, said inner race mounted to said retainer, wherein said elastomeric bearing includes an outer damper portion adjacent said outer race, an inner snubber portion adjacent said inner race, and a rigid transition layer between said outer damper portion and said inner snubber portion;
a backing plate mountable to said outer race, said torque tube between said backing plate and said outer race;
wherein said backing plate includes a redundant pivot generally opposite a motion limiter;
wherein said motion limiter is outboard of said redundant pivot; and
wherein a surface of said rigid transition layer contacts a wall of said motion limiter in a retainer disbond condition.

2. The assembly as recited in claim 1 , wherein the inner race is spherical in shape and the outer race is a planar plate shape.

3. The assembly as recited in claim 2 , wherein the inner snubber portion includes concentric semi-spherical laminates to accommodate blade pitch and flap change.

4. The assembly as recited in claim 2 , wherein the outer damper portion includes generally flat laminates to accommodate in-plane, lead-lag motions.

5. The assembly as recited in claim 1 , wherein said plate defines an annulus radial opening located generally at zero degrees, said motion limiter located generally at 90 degrees and said redundant pivot located generally at 270 degrees.

6. The assembly as recited in claim 1 , wherein said redundant pivot includes a cylinder with a semi-spherical end section.

7. A tail rotor blade assembly comprising:
a backing plate comprising:
a plate which defines an at least partial annulus about an axis;
a motion limiter which extends from said plate generally parallel to said axis;
a redundant pivot which extends from said plate generally parallel to said axis;
wherein said plate defines an annulus radial opening located generally at zero degrees, said motion limiter located generally at 90 degrees, and said redundant pivot located generally at 270 degrees; and

an elastomeric bearing comprising:
an inner race and an outer race defined along an axis, wherein the inner race is spherical in shape and the outer race is a planar plate shape, and wherein said plate is attached to said outer race;
an outer damper portion adjacent said outer race, wherein the outer damper portion includes generally flat laminates;
an inner snubber portion adjacent said inner race, wherein the inner snubber portion includes semi-spherical laminates; and
a rigid transition layer between said outer damper portion and said inner snubber portion, wherein a surface of said rigid transition layer contacts a wall of said motion limiter in a retainer disbond condition.

8. The backing plate as recited in claim 7 , wherein said plate is semi-annular.

9. The backing plate as recited in claim 8 , wherein said plate defines a “C” shape.

10. The backing plate as recited in claim 7 , wherein said redundant pivot includes a cylinder with a semi-spherical end section.

11. The backing plate as recited in claim 7 , wherein said plate defines a plurality of apertures about said axis.

12. The backing plate as recited in claim 11 , further comprising a nut cage adjacent each of said multiple of apertures.

Assignees

• Meyer Leon M
• Lay Richard C
• Schmaling David N
• Sikorsky Aircraft Corp

Inventors

• Meyer Leon M
• Lay Richard C
• Schmaling David N

Classifications

• B64C27/35

  having elastomeric joints · CPC title

• B64C27/33 Primary

  having flexing arms · CPC title