Radial bearing device
10400817 ยท 2019-09-03
Assignee
Inventors
- Arthur Pintauro (Fort Collins, CO, US)
- John Karspeck (Loveland, CO, US)
- Charles Brennecke (Fort Collins, CO, US)
- Taylor Ritchie (Fort Collins, CO, US)
Cpc classification
F16C23/088
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/586
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K5/0605
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2361/91
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2240/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/585
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K5/0694
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C23/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C43/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K1/224
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16K43/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K1/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C23/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/58
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A bearing device for supporting a shaft to rotate relative to an outer hub includes: an annular outer race mountable within an interior bore of the hub, the outer race including an inwardly facing radial groove sized to receive a rounded bearing element; and an annular inner race mountable to an outwardly curved exterior surface of the shaft. The inner race includes an outwardly facing radial groove sized to receive the bearing element, the respective radial grooves of the inner and outer races together forming an annular raceway to retain the bearing element when the bearing device is assembled. The inner race further includes an axially convex surface along an innermost diameter of the inner race, the convex surface shaped to directly engage the exterior surface of the shaft when mounted thereto, such that the inner race remains in contact with the shaft while accommodating radial deflection of the shaft.
Claims
1. A bearing device for supporting a shaft to rotate relative to an outer hub, the bearing device comprising: an annular outer race mountable within an interior bore of the hub, the outer race comprising an inwardly facing radial groove sized to receive a rounded bearing element; and an annular inner race mountable to an outwardly curved exterior surface of the shaft, the inner race comprising: an outwardly facing radial groove sized to receive the bearing element, the respective radial grooves of the inner and outer races together forming an annular raceway to retain the bearing element when the bearing device is assembled; and an axially convex surface along an innermost diameter of the inner race, the convex surface comprising a continuous surface having two peripheral surface portions on either side of a crowned surface portion, the convex surface shaped to directly engage the crowned surface portion of the inner race with the exterior surface of the shaft when mounted thereto, such that the inner race remains in contact with the shaft while simultaneously accommodating radial deflection of the shaft caused by external forces, wherein each of the outer race and the inner race comprises a raised radial shoulder adjacent the respective radial grooves, the height of the shoulder of the inner race in a radial direction being greater than the height of the shoulder of the outer race in the radial direction, and wherein a ratio of the inner race shoulder height relative to the outer race shoulder height is between 1 and 1.5.
2. The bearing device of claim 1, wherein the convex surface is symmetrically curved about an axial midpoint of the inner race.
3. The bearing device of claim 1, wherein the convex surface defines a degree of curvature between 0.5? and 5?.
4. The bearing device of claim 1, wherein the raised radial shoulder of the inner race comprises a filleted lip along an edge of the outwardly facing radial groove of the inner race.
5. The bearing device of claim 4, wherein the filleted lip defines a degree of curvature of at least 70?.
6. A fluid valve, comprising: a valve body housing a valve element in an interior chamber between an inlet port and an outlet port, the valve element configured to regulate a flow of fluid through the valve body; a shaft operatively coupled to the valve element at one end, the shaft residing in an interior bore of a hub portion of the valve body; and a bearing device mounted radially between the shaft and the interior bore of the hub and configured to support the shaft to rotate relative to the valve body, the bearing device comprising an annular outer race, an annular inner race, and the bearing element retained in a raceway formed by opposing radial grooves of the races, the inner race comprising: an axially convex surface along an innermost diameter of the inner race, the convex surface comprising a continuous surface having two peripheral surface portions on either side of a crowned surface portion, the crowned surface portion of the convex surface directly engaging an outwardly curved exterior surface of the shaft, such that the inner race remains in contact with the shaft while simultaneously accommodating radial deflection of the shaft caused by fluid pressure forces, wherein each of the outer race and the inner race comprises a raised radial shoulder bracketing the respective radial grooves, the height of the shoulder of the inner race in a radial direction being greater than the height of the shoulder of the outer race in the radial direction, and wherein a ratio of the inner race shoulder height relative to the outer race shoulder height is between 1.0and 1.5.
7. The fluid valve of claim 6, wherein the bearing device is mounted with a clearance relative to the shaft and the outer race, enabling the inner race to tilt relative to the outer race in response to radial deflection of the shaft.
8. The fluid valve of claim 7, wherein the degree of relative tilt between the inner and outer races is between 0.5? and 2.0?.
9. The fluid valve of claim 6, wherein the convex surface is symmetrically curved an axial midpoint of the inner race.
10. The fluid valve of claim 6, wherein the convex surface defines a degree of curvature of between 0.5? and 5.0?.
11. The fluid valve of claim 6, wherein the radial shoulder of the inner race comprises a filleted lip along an edge of the groove, and wherein the filleted lip defines a degree of curvature of at least 70?.
12. A bearing device for supporting a shaft to rotate relative to an outer hub, the bearing device comprising: an annular outer race mountable within an interior bore of the hub, the outer race comprising an inwardly facing radial groove sized to receive a rounded bearing element; and an annular inner race mountable to an outwardly curved exterior surface of the shaft, the inner race comprising: an outwardly facing radial groove sized to receive the bearing element, the respective radial grooves of the inner and outer races together forming an annular raceway to retain the bearing element when the bearing device is assembled, the radial grooves of the inner and outer races bordered by respective raised radial shoulders, the height of the shoulder of the inner race in a radial direction being greater than the height of the shoulder of the outer race in the radial direction, and the radial shoulder of the inner race comprising a filleted along an edge of the radial groove; and an axially convex surface along an innermost diameter of the inner race, the convex surface comprising a continuous surface having two peripheral surface portions on either side of a crowned surface portion, the convex surface symmetrically curved about an axial midpoint of the inner race and shaped to directly engage the crowned surface portion of the inner race with the exterior surface of the shaft when mounted thereto, such that the inner race remains in contact with the shaft while simultaneously accommodating radial deflection of the shaft caused by external forces, wherein a ratio of the inner race shoulder height relative to the outer race shoulder height is between 1.0 and 1.5.
13. The bearing device of claim 12, wherein the convex surface of the inner race defines a degree of curvature of between 0.5? and 5.0?.
14. The bearing device of claim 12, wherein the filleted defines a degree of curvature of at least 70?.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
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(4)
(5) Many of the features are exaggerated to better show the features, process steps, and results. Like reference numbers and designations in the various drawings indicate like elements.
DETAILED DESCRIPTION
(6) The present disclosure is directed to bearing devices including structural features for withstanding and accommodating high radial and torsional loads caused by angular shaft deflection. In particular, one or more embodiments of the present disclosure are derived from a realization that prior difficulties in producing such bearing devices can be overcome by the combined effect of certain interrelated design elements. In some examples, such elements include: (1) a crowned inner race featuring an axially convex surface engaging the curved exterior surface of the elongated rotating shaft; (2) an enlarged shoulder height along a radial raceway groove of the inner race; and (3) an enlarged radius along a filleted lip extending along the groove. As discussed in detail below, these features in combination represent a distinct paradigm shift in the technical field that enables the use of ball bearings in applications that were previously considered impracticable. Indeed, conventional deep-groove ball bearings experiencing misalignment from shaft deflection demonstrate a tendency for the balls to rotate over the race shoulder, which causes the balls and/or the races to crack from high contact stress and shear. Embodiments of the present disclosure, however, provide features that urge the contact ellipse between the balls and the races to remain contained within the raceway, and reduce contact stress between them in the event that the balls do ride up near the shoulder of the inner race.
(7) Referring first to the exemplary embodiment shown in
(8) Valve element 14 is movable relative to valve body 12, and specifically designed to regulate the flow of fluid traversing interior chamber 20 by altering the size of a flow path through the valvei.e., the valve area. Altering the valve area involves rotating valve element 14 in place about a vertical axis V. For example, rotating valve element 14 in a clockwise direction may constrict the valve area and decrease the mass flow rate of fluid, while counterclockwise rotation may open the valve area to increase the fluid mass flow rate (or vice versa). In this example, valve element 14 features a hybrid butterfly and segmented ball component 22, a reinforcement disk 24, an inlet flow tube 26, and a valve seat 28. This design is particularly well-suited for fluid metering applications, providing fluid-tight shutoff ability, high flow capacity, high differential pressure capability, and ability to operate in elevated pressure and temperature ranges. However, various other types of valve elements may also be used without departing from the scope of the present disclosure.
(9) In this example, valve element 14 is mounted on the distal end of an elongated drive shaft 30 housed in a primary stem 32 of valve body 12. Valve element 14 is operatively coupled to drive shaft 30 (e.g., via mating splines, mechanical fasteners, or other attachment techniques), such that rotation of the drive shaft effects substantially identical rotation of the valve element 14. Drive shaft 30 can be manually, hydraulically, pneumatically, or electrically actuated to operate valve element 14. An idle support shaft 34 housed in a secondary stem 36 of valve body 12 bears the weight of valve element 14 and suspends the valve element 14 in place within interior chamber 20. A base plate 37 coupled to valve body 12 locates the support shaft 34 relative to the valve element 14. Drive shaft 30 and the support shaft 34 are mounted in the respective valve-body stems 32,36 by radial bearing devices 100a,b. As discussed herein, bearing devices 100a,b are specifically configured to simultaneously withstand and accommodate high radial and torsional loads caused by angular deflection of shafts 30, 34.
(10) Angular shaft deflection is caused by high fluid pressure forces F.sub.P acting against valve element 14 in the direction of fluid flow leading from inlet port 16 to outlet port 18. The fluid pressure force urges valve element 14 in a direction substantially perpendicular to the coaxial drive and support shafts 30, 34. In certain industrial applications (e.g., combustion turbine fuel metering implementations), the magnitude of the fluid pressure force may exceed tens of thousands of pounds (e.g., 22,000 lb.sub.f or more). These exceedingly high forces can overwhelm the structural integrity of shafts 30, 34 and their associated mounting hardware, causing the shafts to twist or deflect angularly off of the vertical axis V. Severe angular deflection of shafts 30, 34 may cause the misalignment of radial bearings 100a, 100b, which leads to a risk that the balls secured between the inner and outer races of the bearings will ride up and over the shoulder of the raceway grooves, causing irreparable damage (e.g., structural failure, such as cracking). The particular features discussed below are combined and properly balanced to mitigate this risk.
(11) Referring next to
(12) As shown, outer race 102 includes an annular body 108 having an inner face 110 and an outer face 112. As shown in
(13) Inner race 104 is appropriately configured with a variety of features that renders bearing device 100 resilient to angular shaft deflection. One such feature is the crowned inner face 120. In this example, inner face 120 has an axially convex surface that engages the exterior surface of shaft 30 (see
(14) In the illustrated example, the convex surface of inner face 120 is symmetrically curved, placing crown 128 at the axial midpoint of inner race 104. This symmetrical curvature profile provides equal angular play in both directions of shaft direction. However, other configurations are also contemplated by this disclosure. For example, a non-symmetrical profile may be used where shaft deflection is expected to occur in only a single direction. In some examples, the convex surface defines a degree of curvature of between about 0.5? of 5.0? (e.g., between about 1.0? and 4.0?, or between about 2.0? and 3.0?). The degree of curvature defines the amount of angular play between shaft 30 and inner race 104. The amount of angular play increases with increasing degree of curvature. There is, however, an upper limit to the degree of curvature, because at some point the narrowed crown becomes a stress concentration point that can cause structural failure of the inner race.
(15) Because the amount of angular play provided by the crowned inner face 120 is limited, inner race 104 also includes various compensatory features to further mitigate the risk of structural failure with shaft deflection. That is, when the angular play has been expended by severe shaft deflection, the effect of the compensatory features is to lessen the likelihood of failure as the torsional twisting forces are imparted on the bearing device. One such compensatory feature of inner race 104 is axial and radial clearance, which allows inner race 104 to rotate or tilt in the direction T relative to outer race 102 in response to shaft deflection. In some examples, the degree of relative tilt between the inner and outer races is between about 0.5? and 2.0? (e.g., between about 1.0? and 1.5?, or about 1.3?). Another compensatory feature working in tandem with the axial and radial clearance is the enlargement of radial shoulders 126. Enlargement of radial shoulders 126 decreases the likelihood of structural failure (e.g., ball fracture) by placing the shoulder edge closer to the center of bearing balls 106. That is, the enlarged shoulder height renders the bearing balls more resistant to rolling up on the shoulders during severe torsional twisting (i.e., movement in direction T).
(16) Similar to the degree of curvature on crowned inner face 120, the extent to which the shoulder height (indicated as H.sub.s in
(17) Yet another compensatory feature of inner race 104 is provided in the form of a rounded or filleted lip 132 extending along an edge of its ball-receiving groove 124. The filleted feature of lip 132 effectively reduces the contact stress on bearing balls 106 and inner race 104 in the event that the bearing balls 106 ride up along radial shoulders 126. In some examples, the filleted lip defines a degree of curvature of at least about 70.0?.
(18) The various inner race features discussed throughout the present disclosure are specifically designed to mitigate the risk of structural failure in low-friction deep-groove angular ball bearings that are likely to endure significant shaft deflection during use. While these features may be implemented independently in certain applications, there appears to be a synergistic effect in deploying them in combination. As discussed above, the crowned inner face of the race introduces angular play between the shaft and inner race, and the axial/radial clearance, enlarged shoulder height, and filleted lip provide compensatory relief of contact stress when shaft deflection is severe enough to overwhelm the angular play. In fact, a particular configuration achieved surprisingly superior results during testing. The testing was initially performed at 900? F. with a radial load of 11,000 lb.sub.f. The initial testing was followed by additional testing at 500? F. with a radial load of 22,000 lb.sub.f. Each test was performed for 2,000 full open and close cycles. The design parameters for the tested bearing configuration is provided in the table below.
(19) TABLE-US-00001 Inner Race Design Feature Value Degree of Curvature - Inner Face 2.2? Degree of Clearance 0.0035 inch Shoulder Height Ratio 1.165 Degree of Curvature - Filleted Lip 70.7?
(20) A number of embodiments of the invention have been described. Nevertheless, it will be understood that various modifications may be made without departing from the spirit and scope of the inventions.