This application claims the benefit of U.S. provisional application No. 60/876,954, filed Dec. 21, 2006, the contents of which are incorporated herein by reference in their entirety.
Rolling element bearings (“rolling bearings”) are well-known to comprise a plurality of rolling elements (balls, rollers, or the like) situated between two rings or races that are annular in configuration. For purposes of strength, economy and durability, bearings are often made from metal, e.g., steel.
Airborne systems commonly make use of large azimuth rolling bearings, e.g., bearings having an inner diameter of about 15.25 centimeters (cm) (6 inches (in.)) or more. The bearings are installed in rotating mechanisms (each of which comprises a rotating structure that rotates relative to a support structure) that have to be made from light aluminum alloys in order to control weight. Such bearings and rotating mechanisms can be found in airborne applications including electro-optical targeting system gimbals for camera mounts, search light gimbals, and elsewhere. Conventional bearings are installed and fitted in such mechanisms for optimum stiffness and rotational torque at ambient temperature, but the bearings exhibit significant variations in performance at extremes of temperature in actual use. At one temperature extreme, the bearing will be internally over-loaded to much higher stiffness and rolling friction torque than is optimal; yet at another extreme, the bearing internal preload may be compromised, resulting in loss of stiffness or excessive deflection. Such temperature-related variations in bearing performance are caused by differences in coefficient of thermal expansion (CTE) between the bearing materials (e.g., hardened steels) and the materials used for the rotating mechanism (e.g., aluminum alloys). These variations in bearing performance have to be carefully analyzed, and their consequences mitigated, often necessitating utilization of larger drive motors and/or using more expensive support structure alloys with CTE properties as close to bearing steel as possible.
A rolling bearing comprises a first ring, a second ring concentric with the first ring, and a plurality of rolling elements disposed between the first and second rings. The first ring is generally annular and has a first gap therein and the second ring is generally annular and has a second gap therein.
A rotating mechanism comprises a support structure, a rotating structure, and a rolling bearing as described herein mounted on the support structure and engaging the rotating structure.
A method is provided for improving a rotating mechanism having a CTE and a non-split ring bearing therein. The non-split ring bearing has a bearing CTE that is significantly less than the mechanism CTE, and the method comprises replacing the non-split ring bearing with a bearing having a CTE equivalent to that of the non-split ring bearing and a gap in the inner ring and in the outer ring.
The rolling bearings described herein facilitate rotation in rotating mechanisms that are subject to wide working temperature variations, e.g., from 60° C. to −40° C., and wherein the CTE of the bearing is materially different from (e.g., smaller than) the CTE of the rotating mechanism in which it is used, and for large azimuth bearings. The difference in CTE between the bearing and the rotating mechanism may be, e.g., about 50% to about 100% of the bearing CTE. For example, the CTE of the support structure may be equal to or greater than about 150% of the CTE of the bearing rings, optionally up to about 200% of the CTE of the bearing rings. The bearings have a double split ring design in which both rings (the inner ring and the outer ring) are split, i.e., they each have a gap disposed radially across them. The gaps allow the rings to contract and flex as their temperature is lowered and in response to the physical force imposed by the rotating mechanism that may be contracting or expanding at a different rate from that of the bearing. The bearings exhibit reduced temperature-induced variations in bearing performance relative to non-split ring bearings.
In bearings having a double-split ring design, both rings of the bearing have gaps in them. Once properly installed in bearing support structure at room temperature, the bearings will maintain steady and predictable stiffness and torque characteristics throughout a wide temperature range, despite differences in CTE between the bearing and the support structure material. As a result, temperature-related variations in performance are greatly reduced, even if there is a significant difference between the CTE of the bearing material (e.g., steel) and the support structure material (e.g., aluminum). Thus, use of the bearings described herein results in improved rotating mechanism that comprise a support structure of a material having a different CTE from the bearing ring material, and in large azimuth bearings.
With knowledge of the CTE of the ring material, the width of the gap is chosen to approach zero at the lowest anticipated temperature and, if possible, to not exceed 50% of the ball diameter at the highest anticipated temperature. A gap having a width of about 0.76 millimeters (mm)(about 0.03 in.) to about 1.78 mm (about 0.07 in.) at room temperature will be suitable for many large azimuth bearings for airborne application.
One illustrative embodiment of a double split-ring rolling bearing is shown in
A variety of rolling bearings can have split rings as described herein: ball bearings, roller bearings, needle bearings, thrust bearings, etc.
In
Rotating mechanisms that comprise conventional, non-split ring roller bearings and in which there is a significant difference between the rotating mechanism CTE and the bearing ring CTE can be improved by replacing the non-split bearing with a bearing comprising gaps in the rings as described herein, even if the split ring bearing CTE is equivalent to that of the non-split ring bearing. A result will be a reduction in temperature-induced stress over the working temperature range of the mechanism even though the difference in CTE between the mechanism and the bearing therein is substantially unchanged.
Unless otherwise specified, all ranges disclosed herein are inclusive and combinable at the end points and all intermediate points therein. The terms “first,” “second,” and the like, herein do not denote any order, quantity, or importance, but rather are used to distinguish one element from another. Likewise, the terms “a” and “an” herein do not denote a limitation of quantity, but rather denote the presence of at least one of the referenced item. Characterizations of any feature in geometric terms (e.g., annular, circular, etc.) does not require precise adherence to geometric forms, but rather allows minor variations to accommodate reasonable manufacturing tolerances.
Although the invention has been described with reference to particular embodiments thereof, upon a reading and understanding of the foregoing disclosure, it will be understood by one of ordinary skill in the art that numerous variations and alterations to the disclosed embodiments will fall within the spirit and scope of this invention and of the appended claims.
Number | Date | Country | |
---|---|---|---|
60876954 | Dec 2006 | US |