Ball joints are used in fluid lines to impart limited flexibility for the purpose of accommodating tolerances, thermal expansion and vehicular motion. They can be used in almost any type of fluid line. However, the particular joint under consideration is adapted for use in jet aircraft pneumatic environmental control systems, and in engine bleed air ducting. Reference is made to U.S. Pat. No. 6,860,519 for an understanding of the basic operation of such joints, the contents of which are fully incorporated herein by reference.
Under high dynamic contact loads, the bearings in such joints can gall when two surfaces of similar materials slide against one another, thereby increasing the friction that can lead to increased bending moments and possibly component failure. Bearings in the prior art are also susceptible to temperature failure and deformation under high loads, leading to the loss of the pre-load and weaknesses in the joint. The present invention is designed to overcome these drawbacks and others of the prior art.
The present invention is a flexible ball joint for high pressure lines such as those found in aircraft applications. The ball joint includes a housing enclosing a bellows that couples a first tube or conduit to a second tube or conduit. The joint includes a toroidal bearing between mating flaps of the ball component that is made of a high strength material such as steel or nickel alloys as suitable for the application. The toroidal bearing is structurally stable under nominal loads due to its strength properties, resisting deformation as is found in other ball joints. The toroidal bearing includes a spacer that prevents friction and high compressive contact loads from generating between adjacent like surfaces. The spacer minimizes friction through the use of dissimilar materials, improving the bending moment characteristics of the flexure joint. The bearing may further include a thin, graphite mesh between the outer surface of the toroidal bearing and the spacer. The spacer may be titanium, and may be perforated to allow the particulate graphite to extrude into the dynamic surface so as to further reduce the friction through “dry” lubrication. This further reduces the wear on the joint and preserves the integrity of the joint over the lifetime of the mechanism.
These and other features of the invention will best be understood as described below in the detailed description of the invention in conjunction with the associated drawings.
In
Mounted on the annulus 15 is a toroidal bearing 17 that extends around the annulus and bears directly against the shoulder 37, where radially inward pressure is applied by the constraining cover 20 and cap 21. The cover 20 has two portions, a cylindrical portion terminating at a distal edge 47, where the distal edge 47 engages the distal lip 43 of the outer annulus 12 to close the ball joint, and a frusto-conical proximal portion that extends over the toroidal bearing 17. The end cap 21 bears against the cover 20 and provides closure to the joint at a proximal end, where rim 49 encloses the inner annulus 15 to seal the joint. The cap 21 may also be integral to cover 20 as opposed to a separate component.
The toroidal bearing 17 is structurally stable under the normal compressive loads and therefore holds its preload under more severe conditions than prior art joints. Also, for components under dynamic high compressive contact loads, it is advantageous to separate similar materials from sliding contact that can cause galling and an increased bending moment. The titanium insert 19 significantly minimizes the occurrence of galling and reduces the friction which has direct impact to bending moment characteristics of the flex joint. Low bending moment is a key design feature of flex joints of this kind.
The foregoing descriptions and illustrations are not intended to be limited, and various modifications and alterations are available without departing from the present invention. Accordingly, all such modifications and alterations are intended to be considered part of the present invention. The scope of the invention is properly limited to the words of the appended claims, using their plain and ordinary meanings, in view of (but not constrained by) the foregoing descriptions and drawings.
This application claims priority from U.S. Application No. 62/100,396, filed Jan. 6, 2015, the content of which is incorporated herein by reference in its entirety.
Number | Date | Country | |
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62100396 | Jan 2015 | US |