The present disclosure relates to bushing bearings, and more specifically self-adjusting bushing bearings with magnetic levitation.
The following U.S. patents are hereby incorporated herein by reference, in entirety.
U.S. Pat. No. 8,870,459 discloses a self-adjusting bushing bearing for engagement with a shaft. A bearing housing is provided. A bearing sub-assembly is received inside of the bearing housing and the bearing sub-assembly is adapted to receive the shaft. The bearing sub-assembly has at least two bearing segments and at least one springy element engaged with the bearing housing which compresses the bearing segments toward one another.
U.S. Pat. No. 9,790,988 discloses a self-adjusting bushing bearings having a springy element. The self-adjusting bushing bearing has a bearing subassembly that is configured to be received in a housing and also has a plurality of bearing segments that together are configured to receive a shaft therein. A springy element biases the plurality of bearing segments radially inwardly towards the shaft. The springy element is mated with at least one bearing segment in the plurality of bearing segments.
U.S. Pat. No. 9,995,342 discloses a self-adjusting bushing bearing with a shaft seal for engaging a shaft. The self-adjusting bushing bearing has a plurality of bearing segments configured to receive a shaft therein. A springy element engages an outer surface of the plurality of bearing segments and biases the plurality of bearing segments towards the shaft. A shaft seal coupled to the springy element is configured to contact the shaft when the shaft is received in the plurality of bearing segments so as to create an operable seal between the shaft and the housing.
This Summary is provided herein to introduce a selection of concepts that are further described herein below in the Detailed Description. This Summary is not intended to identify key or essential features from the claimed subject matter, nor is it intended to be used as an aid in limiting the scope of the claimed subject matter.
The present disclosure generally relates to a self-adjusting bushing bearing that is receivable within a housing and configured to control movement of a shaft therein. Shaft magnet segments are configured to receive the shaft therein, where each of the shaft magnet segments has an inner portion having an inner polarity and an outer portion of the shaft magnet segments has an outer polarity that is opposite the inner polarity. Bearing magnet segments are configured to receive the shaft magnet segments therein, where each of the bearing magnet segments has an inner portion having an inner polarity and an outer portion of the bearing magnet segments has an outer polarity that is opposite the inner polarity. A springy element is disposed between the housing and the bearing magnet segments to bias the bearing magnet segments radially inwardly relative to the shaft magnet segments. The outer polarity of the shaft magnet segments is the same as the inner polarity of the bearing magnet segments so as to repel each other.
Another embodiment of the present disclosure generally relates to a self-adjusting bushing bearing that is receivable within a housing and configured to control movement of a shaft therein. Shaft magnet segments are configured to receive the shaft therein, where each of the shaft magnet segments has an inner portion having an inner polarity and an outer portion of the shaft magnet segments has an outer polarity that is opposite the inner polarity. Bearing magnet segments are configured to receive the shaft magnet segments therein, where each of the bearing magnet segments has an inner portion having an inner polarity and an outer portion of the bearing magnet segments has an outer polarity that is opposite the inner polarity. A springy element is disposed between the housing and the shaft to bias the shaft radially inwardly relative to the housing. The outer polarity of the shaft magnet segments is the same as the inner polarity of the bearing magnet segments so as to repel each other.
Another embodiment of the present disclosure generally relates to a self-adjusting bushing bearing that is receivable within a housing and configured to control movement of a shaft therein. Shaft magnet segments are configured to receive the shaft therein, where each of the shaft magnet segments has an inner portion having an inner polarity and an outer portion of the shaft magnet segments has an outer polarity that is opposite the inner polarity. Bearing magnet segments are configured to receive the shaft magnet segments therein, where each of the bearing magnet segments has an inner portion having an inner polarity and an outer portion of the shaft magnet segments has an outer polarity that is opposite the inner polarity, where the outer polarity of the shaft magnet segments is the same as the inner polarity of the bearing magnet segments so as to repel each other. A springy element is disposed between the shaft and the shaft magnet segments to bias the shaft magnet segments radially outwardly away from the shaft. A magnetic thrust washer receives the shaft therein and is axially displaced from the bearing magnet segments, where the magnetic thrust washer has an inner portion having an inner polarity and an outer portion of the shaft magnet segments has an outer polarity that is opposite the inner polarity, and where the magnetic thrust washer is positioned such that the inner portion of the magnetic thrust washer repels both the inner portions of the bearing magnet segments and the outer portions of the shaft magnet segments. The bearing magnet segments are rotationally fixed relative to the housing.
Another embodiment of the present disclosure generally relates to a self-adjusting bushing bearing that is receivable within a housing and configured to control movement of a shaft therein. Shaft magnet segments are configured to receive the shaft therein, where each of the shaft magnet segments has an inner portion having an inner polarity and an outer portion of the shaft magnet segments has an outer polarity that is opposite the inner polarity. Bearing magnet segments are configured to receive the shaft magnet segments therein, where each of the bearing magnet segments has an inner portion having an inner polarity and an outer portion of the shaft magnet segments has an outer polarity that is opposite the inner polarity, where the outer polarity of the shaft magnet segments is the same as the inner polarity of the bearing magnet segments so as to repel each other. A first springy element is disposed between the housing and the bearing magnet segments to bias the bearing segments inwardly towards the shaft. A second springy element is disposed between the shaft and the shaft magnet segments to bias the shaft magnet segments radially outwardly away from the shaft. The outer polarity of the shaft magnet segments is the same as the inner polarity of the bearing magnet segments so as to repel each other.
Various other features, objects and advantages of the disclosure will be made apparent from the following description taken together with the drawings.
The present disclosure is described with reference to the following figures.
Self-Adjusting Bushing Bearings (SABBs) are generally known in the art, exemplified by the devices disclosed in U.S. Pat. No. 8,870,459. SABBs are generally known to comprise at least two bearing segments configured to receive a shaft, also having at least one springy element that engages the outside surfaces of the bearing segments to compress the bearing segments toward one another in an inward direction. This springy element also contacts the inside surface of a housing when the SABB is received within the housing. In this regard, the springy elements bias the bearing segments into contact with the shaft when a shaft is received inside the SABB, maintaining this contact despite wear of the elements. This use of springy elements generally allows the machining tolerances of the shaft and housing containing the SABB to not be near as tight as required for standard bushing, ball, and roller bearings. Furthermore, the springy elements allow the same SABB to accommodate both conical and cylindrical shafts.
Through research and experimentation, the present inventor has identified further opportunities for improving upon SABBs known in the art, specifically through the use of magnetic levitation. The use of magnetic force in bearings to keep the rotating parts from contacting each other has many advantages, including having: 1) essentially no friction; 2) no wear of mating parts; 3) no “stiction” as an increased friction (and wear) at start-up until the contact surfaces are fully lubricated; 4) no failures due to loss of lubricant; 5) no failures due to degradation of the lubricant over time; 5) no failures due to contamination of the lubricant, and 6) essentially no change in friction due to changes in temperature, to name a few.
However, magnetic bearing systems known in the art are very expensive because in addition to the use of permanent magnets to provide a separating force between the shaft and housing, additional electromagnets and associated control circuits are needed to maintain the stability of the assembly due to the Earnshaw Theorem. Earnshaw's Theorem states that a collection of point charges cannot be maintained in a stable stationary equilibrium configuration solely by the electrostatic interaction of the charges. This was first mathematically demonstrated by British mathematician Samuel Earnshaw in 1842. It is usually referenced to magnetic fields, but was first applied to electrostatic fields.
The instability is because the strength of a magnetic field falls off as the inverse-square of the distance. For example, the force of the same magnet with a given gap g is ¼th as strong when the gap is doubled to 2 g. Earnshaw showed that this non-linear force vs. distance characteristic is unstable if, for example, you try to use a bushing bearing made out of a permanent magnet material in which the inside surface of the bushing bearing has the same magnetic polarity as the outside surface of the shaft.
The Earnshaw Theorem is based solely upon electrostatic/magnetic forces. However, the Self-Adjusting Bushing Bearing (SABB) described in U.S. Pat. Nos. 8,870,459, 9,790,988, and 9,995,342 are based on the addition of a resilient or a “springy element” that can be designed to complement the magnetic force such that the combined spring force and magnetic repulsion force vs. radial displacement provides dynamic stability. In other words, the inventor has recognized that the “springy element” feature U.S. Pat. Nos. 8,870,459, 9,790,988, and 9,995,342 can be used to provide the resilience necessary to stabilize an SABB with magnetic levitation using repelling permanent magnet bearing surfaces.
The result of this configuration is that the bearing magnet segments 4 are magnetically repelled away from the shaft magnet segments 3 by virtue of the same magnetic polarities facing one another. This in turn causes magnetic levitation of the bearing magnet segments 4 relative to the shaft magnet segments 3, and likewise relative to the shaft 1 contained within the housing 2.
Additionally, the present inventor has recognized that if the springy element 5 is an O-ring or X-ring, by itself or in combination with a leaf spring, it will also provide vibration damping (D), as depicted in
The slope (SMagnet) of the magnetic forces Fm within the linear approximation region of the Magnet Force Fm versus gap G from G/G0=1 to G/G0=1.66 is approximated as follows:
The Slope (SSpring) of the Spring Force Fm versus gap G is the mirror image of the slope of the Magnet Force Fm vs gap G:
SSpring=0.97 Eqn. 2)
SSpring=Δ(FSpring/F0)/Δ(G/G0)=0.97 Eqn. 3)
Solving Eqn. 3) for ΔFSpring/ΔG:
ΔFSpring/ΔG=0.97(F0/G0)=KSpring Eqn. 4)
KSpring=0.97(F0/G0) Eqn. 5)
By way of example:
The result demonstrated above shows that dynamic stability for a permanent magnet repulsion force of 10 lbs at a gap of 0.010″ can be achieved with a springy element having a spring rate (K) of 970 Lbs/in and an installed opposing force of 10 lbs. The above KSpring and loads are for illustrative purpose and do not mean that other KSpring and loads would not also result in dynamic stability. A major function of the disclosed device is that the decrease in the magnetic repulsion force as the gap G increases will be compensated by the increase in springy element 5 force such that the combined force will oppose any radial motion of the shaft 1, thereby creating a dynamic and stable response to a perturbation.
As discussed above, the embodiment of
The figures further show an embodiment in which two shaft magnet segments 3 are wrapped around the shaft 1; however, other numbers of shaft magnet segments 3 are also anticipated by the present disclosure. The shaft magnet segments 3 are radially magnetized such that an inner portion 23A having a first polarization (e.g., South) next to the shaft 1, and an opposing outer portion 23B having a second polarization that is opposite the first polarization (North in this example). Three bearing magnet segments 4 that are concentric with the two shaft magnet segments 3. The bearing magnet segments 4 are radially magnetized so as to define an inner portion 24A having a first polarity (in this example, North) at its inner diameter, in other words, facing radially inwardly towards the shaft magnet segments 3 and shaft 1. Likewise, an outer portion 24B of the bearing magnet segments 4 has an opposite second polarity, which in this example would necessarily be South. In this manner, the outer portions 23B of the shaft magnet segments 3 are adjacent to the inner portion 24A of the bearing magnet segments 4, which has the same polarity and thus oppose each other.
A springy element 5 is disposed between the bearing magnet segments 4 to the inside diameter of the housing 2, which in certain examples prevents rotational movement therebetween. As best shown in
The magnetic thrust washers 6 are resiliently loaded against the bearing magnet segment 4, for example by a thrust springy element 11, such as an X-ring, for example. Both the magnetic thrust washer 6 and thrust springy element 11 are supported by a thrust retainer 12 that is axially located on the shaft 1 by snap ring 13. It will be recognized that the relative positions of these elements may also be modified, including relative to the housing 2, for example. It will also be recognized that
Yet another exemplary embodiment is provided in
Both the second springy element 18 and the first springy element 16 provide resiliency for angular and radial misalignment, shock, and any differences due to differences in coefficients of thermal expansion. In this embodiment, the second springy element 18 provides the necessary preload to stabilize the permanent magnet repulsion forces while the first springy element 16 dampens vibrations.
The second springy elements 18 (or leaf springs used as any of the springy elements 5) can be fabricated to produce any desired force vs. deflection characteristics by changing the thickness, width, length, and/or material. The leaf springs can also be stacked on top of one another. Furthermore, if the leaves are triangular shaped they will deflect semi-circularly and will be uniformly stressed.
While the embodiments shown generally relate to that of a rotational bearing, the invention can also be used as a linear bearing. For example, the bearing magnet segments 4 could be made with an axial dimension equal to the desired linear travel and secured by the snap rings and thrust washer assemblies that act as a cushion at the end of the travel each way. The shaft magnet segments 3, springy elements 5, and shaft 1 would then be able to translate relative to the bearing segment magnets 4 and vice versa.
A distinction between the SABB 30 presently disclosed and those known in the art is the magnetic levitation provided by the incorporation of permanent magnets. As shown in
In certain embodiments, magnetic thrust washers 6 are positioned at each end of the SABB 30 and are positioned along the axis of the housing 2 by means of snap rings 13 that engage to retain the retainer 12 in position relative to the shaft 1. As shown in
The figures show various embodiments for the discussion below. Various other configurations can be assembled based on the same principle but utilizing different components. For example, the figures show the use of an O-rings or leaf springs, but other components individually or in combination can be used such as X-rings and coil springs. Furthermore, since the embodiment is based on the SABB patents incorporated by reference herein, all the features described in the patents can be added such as shaft seals and lubricants. Additionally, because of the magnetism of the permanent magnets, a lubricant could be used that contains stable suspensions of magnetic material to help ensure that the lubricant remains in contact with the magnet surfaces and does not leak out without seals or with seals that fail. Finally, since magnetic strength of a permanent magnet or paramagnetic material can be increased by bringing other magnets in series with it, the magnetic SABB load carrying capacity can be enhanced by the addition of other permanent magnets or electromagnets without the necessary electronic control systems used in conventional electromagnetic bearings.
This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to make and use the invention. Certain terms have been used for brevity, clarity, and understanding. No unnecessary limitations are to be inferred therefrom beyond the requirement of the prior art because such terms are used for descriptive purposes only and are intended to be broadly construed. The patentable scope of the invention is defined by the claims and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have features or structural elements that do not differ from the literal language of the claims, or if they include equivalent features or structural elements with insubstantial differences from the literal languages of the claims.
This application claims the benefit of and priority to U.S. Provisional Patent Application No. 62/966,844, filed Jan. 28, 2020, which is hereby incorporated by reference in entirety.
Number | Date | Country | |
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62966844 | Jan 2020 | US |