Multi-directional elastomeric dampened ball joint assembly

Patent metadata

Field	Value
Publication number	US-9458877-B2
Application number	US-201313749495-A
Country	US
Kind code	B2
Filing date	Jan 24, 2013
Priority date	Jan 24, 2013
Publication date	Oct 4, 2016
Grant date	Oct 4, 2016

Abstract

A method and apparatus for reducing a force. An apparatus comprises a multi-directional joint assembly and a damper associated with the multi-directional joint assembly. The multi-directional joint assembly has a first end and a second end. The first end and the second end move relative to each other. The damper is comprised of a number of elastomeric layers and a number of rigid layers interspersed with each other reducing at least one of a force and a moment.

First claim

What is claimed is:

1. An apparatus comprising:
a beam having a first end of a multi-directional joint assembly connected thereto, wherein the first end comprises a ball distally connected to the beam by a first elongate member and a first portion of an enclosure of the multi-directional joint assembly, the enclosure comprised of the first portion and a second portion, wherein the ball is held within an interior of the enclosure;
a rotorcraft having a second end of the multi-directional joint assembly connected thereto, wherein the second end comprises a hemispherical socket distally connected to the rotorcraft by a second elongate member and extending through a hole in the second portion, wherein the ball is pivotally held within the hemispherical socket by a frusto-spherical ring directly connected to the hemispherical socket; and
a damper disposed between the hemispherical socket and the second portion, wherein the damper is comprised of a number of elastomeric layers and a number of rigid layers interspersed with each other.

2. The apparatus of claim 1 , wherein the damper is an elastomeric bearing.

3. The apparatus of claim 1 , wherein the number of rigid layers and the number of elastomeric layers are associated with each other and the multi-directional joint assembly.

4. The apparatus of claim 1 , wherein the number of elastomeric layers is comprised of a number of materials selected from the group of neoprene, a thermoplastic elastomer, synthetic polyisoprene, polybutadiene, ethylene-vinyl acetate, and chlorosulfonated polyethylene.

5. The apparatus of claim 1 , wherein the number of rigid layers is selected from the group of a metal and a plastic.

6. The apparatus of claim 1 , wherein the damper absorbs energy from a number of loads caused by at least one of a number of forces and a number of moments applied to at least one of the first portion and the second portion of the multi-directional joint assembly.

7. The apparatus of claim 6 , wherein the number of forces is selected from at least one of a normal force, a torsional force, and a bending force, and wherein the number of moments is selected from one of torsion and a bending moment.

8. The apparatus of claim 1 , wherein the damper is connected to the ball and the socket.

9. The apparatus of claim 8 , wherein the multi-directional joint assembly further comprises:
an elongate member extending from the ball, wherein the elongate member is associated with a cavity of the enclosure in which the ball and socket are located.

10. The apparatus of claim 9 , wherein the damper is directly connected to the enclosure and the socket and is indirectly connected to the ball by the enclosure and the elongate member.

11. The apparatus of claim 1 , wherein an outer surface of the socket contacts the damper.

12. The apparatus of claim 1 , wherein the first portion and the second portion of the enclosure are connected at a second midpoint of the ball, and wherein the first midpoint and the second midpoint are the same when no bending force is applied to the multi-directional joint.

13. A multi-directional elastomeric dampened ball joint assembly comprising:
a beam having a first end of a multi-directional joint assembly connected thereto;
a rotorcraft having a second end of the multi-directional joint assembly connected thereto;
an enclosure and a multi-directional joint, the enclosure comprised of a first portion and a second portion, wherein the multi-directional joint comprises a first end comprising a ball associated with the first portion and distally connected to the beam by a first elongate member;
a second end comprising a hemispherical socket associated with the second portion and distally connected to the rotorcraft by a second elongate member and extending through a hole in the second portion, wherein the ball is moveably held in a cavity in the socket;

a frusto-spherical ring directly connected to the hemispherical socket, wherein the ring pivotally holds the ball within the hemispherical socket; and
a hemispherical elastomeric bearing disposed between the hemispherical socket and the second portion and having alternating rigid layers and elastomeric layers, wherein an outer surface of the hemispherical elastomeric bearing is associated with an inner surface of the enclosure, an inner surface of the hemispherical elastomeric bearing is associated with an outer surface of the socket, and wherein the hemispherical elastomeric bearing absorbs energy and reduces at least one of a force and a moment applied to at least one of the first portion and the second portion.

14. The multi-directional elastomeric dampened ball joint assembly of claim 13 , wherein the ball, the socket, and the hemispherical elastomeric bearing are located within an interior of the enclosure.

Assignees

• Boeing Co

Inventors

• Bouwer Scott Hendrik

Classifications

• F16F1/406

  characterised by the shape of the elastic elements · CPC title

• F16C11/083

  by means of parts of rubber or like materials · CPC title

• F16C11/0695

  Mounting of ball-joints, e.g. fixing them to a connecting rod · CPC title

• B64C27/22

  Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft · CPC title

• F16C11/06 Primary

  Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints (universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts F16D3/16) · CPC title