GB2537378A - Bearing system and method - Google Patents

Bearing system and method Download PDF

Info

Publication number
GB2537378A
GB2537378A GB1506277.1A GB201506277A GB2537378A GB 2537378 A GB2537378 A GB 2537378A GB 201506277 A GB201506277 A GB 201506277A GB 2537378 A GB2537378 A GB 2537378A
Authority
GB
United Kingdom
Prior art keywords
bearing
shaft
split ring
collar
bearing system
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB1506277.1A
Other versions
GB201506277D0 (en
GB2537378B (en
Inventor
Hetherington Adrian
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Primetals Technologies Ltd
Original Assignee
Primetals Technologies Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Primetals Technologies Ltd filed Critical Primetals Technologies Ltd
Priority to GB1506277.1A priority Critical patent/GB2537378B/en
Publication of GB201506277D0 publication Critical patent/GB201506277D0/en
Priority to CN201680021817.4A priority patent/CN107429749B/en
Priority to US15/561,092 priority patent/US10184516B2/en
Priority to KR1020177032832A priority patent/KR102572161B1/en
Priority to PCT/EP2016/057528 priority patent/WO2016165995A1/en
Priority to EP16714449.2A priority patent/EP3283781B1/en
Publication of GB2537378A publication Critical patent/GB2537378A/en
Application granted granted Critical
Publication of GB2537378B publication Critical patent/GB2537378B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B31/00Rolling stand structures; Mounting, adjusting, or interchanging rolls, roll mountings, or stand frames
    • B21B31/07Adaptation of roll neck bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C19/00Bearings with rolling contact, for exclusively rotary movement
    • F16C19/02Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows
    • F16C19/14Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load
    • F16C19/18Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load with two or more rows of balls
    • F16C19/181Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load with two or more rows of balls with angular contact
    • F16C19/182Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load with two or more rows of balls with angular contact in tandem arrangement
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C13/00Rolls, drums, discs, or the like; Bearings or mountings therefor
    • F16C13/02Bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C19/00Bearings with rolling contact, for exclusively rotary movement
    • F16C19/02Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows
    • F16C19/14Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C19/00Bearings with rolling contact, for exclusively rotary movement
    • F16C19/22Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings
    • F16C19/34Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load
    • F16C19/36Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load with a single row of rollers
    • F16C19/364Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load with a single row of rollers with tapered rollers, i.e. rollers having essentially the shape of a truncated cone
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C3/00Shafts; Axles; Cranks; Eccentrics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/063Fixing them on the shaft
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2226/00Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/50Positive connections
    • F16C2226/60Positive connections with threaded parts, e.g. bolt and nut connections
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2226/00Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/50Positive connections
    • F16C2226/70Positive connections with complementary interlocking parts
    • F16C2226/74Positive connections with complementary interlocking parts with snap-fit, e.g. by clips
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2322/00Apparatus used in shaping articles
    • F16C2322/12Rolling apparatus, e.g. rolling stands, rolls

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Mounting Of Bearings Or Others (AREA)
  • Rolling Contact Bearings (AREA)

Abstract

A bearing system having a shaft 100 including a circumferential channel100c, the profile of the channel being inclined relative to the longitudinal axis of the shaft. A bearing 200 is configured to be disposed around the shaft when in use and a split ring 300 is located in the channel so as to be in contact with the inclined surface. The split ring includes a first part 300a having an outer diameter and a second part 300b having a greater diameter than the first part, thereby providing a thrust surface 300c. A collar 400 accommodates the first part of the split ring and a locator 500 exerts an axial force between split ring and bearing to locate the bearing on the shaft. In use, an axial thrust load exerted on the split ring by the shaft is transmitted to the collar by the thrust surface, and the split ring is urged along the inclined profile surface so as to produce a radial load on the split ring which is resisted by the collar. A method for assembling the system is provided.

Description

BEARING SYSTEM AND METHOD
The present invention relates to a bearing system and a method of assembling a bearing system.
In a rolling mill, work roll shafts are rotatably supported by bearings. Once bearings have been fitted to a work roll shaft they must be located axially and the axial location must be able to withstand the anticipated axial thrust forces from the shaft. As shown in Figure 1, a conventional arrangement for the bearing 1 axial location on a work roll shaft 2 having a longitudinal axis X is a circumferential rectangular groove 3 which is cut into the shaft, with radii in the corners, into which a split ring 4 is inserted. The two halves of the split ring 4 are connected together, for example by a pivot at one side and by a bolt at the other side so that the assembly can be slipped over the shaft 2 and then the bolt inserted to hold the split ring 4 together. A bearing retaining sleeve 5 having a threaded end 5a is tightened against the side of the split ring 4 by a threaded collar 6, forcing the split ring 4 axially against the outer face of the groove 3, whilst simultaneously holding the inner race of the axial bearing 1 against an abutment face 7, which may be a spacer or a neck ring of the shaft 2. This securely locates the bearing 1 onto the roll shaft 2.
One unintended consequence of this arrangement is to weaken the work roll shaft. Not only is the shaft cross-section reduced but also the shape of the profile gives rise to stress concentrations. This can lead to premature failure due to fatigue. As the market moves toward wider rolling mills with correspondingly greater torque values this is a growing problem.
The present invention aims to alleviate at least to some extent this problem of the prior art.
The invention is set out in the accompanying claims.
According to an aspect of the invention, there is provided a bearing system, comprising: a shaft, having a longitudinal axis about which the shaft can rotate, the shaft including a circumferential channel comprising an axially extending profile surface at least part of which is inclined relative to the longitudinal axis; a bearing, configured to be disposed around the shaft in use; a split ring, configured to be located in the circumferential channel in use so as to be in contact with the inclined profile surface, the split ring including a first part having an outer diameter, and a second part having a greater outer diameter than the first part so as to provide a thrust surface; a collar, including an internal bore configured to accommodate the first part of the split ring in use; and a bearing locator, configured to exert an axial locating force between the split ring and the bearing in order to locate the bearing on the shaft; wherein in use an axial thrust load exerted on the split ring by the shaft is transmitted to the collar by the thrust surface, and the split ring is urged along the inclined profile surface so as to produce a radial load on the split ring which is resisted by the collar.
In use, the axial thrust load, exerted on the split ring by the channel of the shaft, is transmitted to the collar by the thrust surface. Since the channel has an axially-extending profile surface, at least part of which is inclined to the longitudinal axis of the shaft, the split ring is urged to ride over the inclined profile surface and so experiences a radial force which attempts to expand the split ring radially. The surrounding collar provides radial containment of the split ring, thereby preventing the split ring from moving axially, or at least limiting its axial movement, and keeping the bearing correctly located on the shaft. Thus, the collar transmits the axial load to secure the bearing and simultaneously contains the radial expansion force imposed on it by the split ring. The provision of the inclination or slope in the profile surface of the circumferential channel is beneficial because it reduces the overall stress concentrations in the shaft in the vicinity of the channel. Depending on the shape of the inclined surface, the peak stress may be reduced by 50% in comparison with a conventional, substantially square-section channel.
The part of the profile surface of the channel, which is in contact with the split ring and takes the thrust load and provokes radial expansion of the split ring, is inclined or sloping in the sense that it is not at right angles to or parallel with the longitudinal axis of the shaft. Other parts of the profile surface of the channel, that is the non-contact/non-thrust parts which do not cause the radial expansion, may be parallel with or at right angles to the longitudinal axis. A part of the profile surface which is parallel with the longitudinal axis might or might not be in contact with the split ring -but either way this part could not transmit any thrust load.
The bearing locator and the collar may comprise a single element. Alternatively, the bearing locator and the collar may comprise separate elements. The bearing locator may comprise: a threaded spacer, configured to be disposed between the bearing and the circumferential channel; and a nut, configured to be screwed on the threaded spacer into abutment with the collar so as to exert the axial locating force. The threaded spacer may be configured such that the nut and the collar can be disposed on the threaded spacer within the axial length of the threaded spacer, so that the split ring can be located in the circumferential channel adjacent the threaded spacer on the shaft.
The inclined profile surface of the circumferential channel may be straight. Alternatively, the inclined profile surface of the circumferential channel may be curved. Alternatively, the inclined profile surface of the circumferential channel may be partly straight and partly curved. The radius of curvature may be constant. Alternatively, the radius of curvature may be varied. The profile surface, or a tangent to the profile surface, may be inclined from the longitudinal axis of the shaft by about 1 to 80 degrees, preferably about 1 to 45 degrees, more preferably about 1 to 30 degrees.
It will be understood that the profile of the channel may take any general shape, provided that the profile is configured such that the split ring will experience a radial force when it is subjected to the shaft axial load. This will be the case as long as the profile surface has some inclination or slope in the axial direction relative to the longitudinal axis of the shaft and the split ring is in contact with the inclined surface. That is, at least some part of the profile (or a tangent to the part of the profile) forms an angle with the longitudinal axis of the shaft which has a value which is greater than 0 and less than 90 degrees. Put another way, the profile comprises a surface which is inclined both to the longitudinal axis of the shaft, and to an imaginary line which is normal to the longitudinal axis of the shaft. Accordingly, the profile of the channel may be entirely curved, or partly curved, or comprise at least one straight and inclined portion, or comprise a series of straight portions which together comprise a general curve.
According to another aspect of the invention, there is provided a method of assembling a bearing system as described herein above, comprising: positioning the bearing onto the shaft; positioning the bearing locator onto the shaft; positioning the collar over the bearing locator; positioning the split ring at least partially in the circumferential channel; positioning the collar over the first part of the split ring; and adjusting the bearing locator so as to exert the axial locating force between the split ring and the bearing in order to locate the bearing on the shaft.
Embodiments will now be described, by way of example, with reference to the accompanying figures in which: Figure 1 shows a simplified sectional view of a conventional bearing system in an assembled condition; Figure 2 shows a simplified sectional view of a bearing system according to the invention in an assembled condition; Figures 3 to 5 show various stages of assembly of the bearing system of Figure 2; Figure 6 illustrates a method of assembly of the bearing system of Figure 2; and Figures 7a and 7b illustrate stress distributions in the conventional and inventive bearing systems respectively.
Referring to Figure 2, an assembled bearing system comprises: an elongate shaft 100 (only a portion of which is shown); a bearing 200; a split ring 300; a collar 400; and a bearing locator 500 including a spacer 500a and a nut 500b.
The shaft 100 is supported by the bearing 200 in a rolling mill 600 such that the shaft 100 can rotate about its longitudinal axis X. A forward portion of the shaft 100 comprises a shoulder 100a which defines a forward circumferential region of the shaft 100. A central region of the shaft 100 adjacent to the shoulder 100a comprises a shaft journal 100b which is surrounded by an inner surface 200a of the bearing 200. In this embodiment the bearing 200 is a double row angular contact ball bearing, for taking an axial thrust of the shaft 100, but could be a taper roller thrust bearing, or any other type of thrust bearing. A forward face of the bearing 200 is in contact with an abutment face 600a, for example of a spacer or a radial bearing (not shown).
Axially spaced from the journal 100b there is a groove or circumferential channel 100c. The channel 100c comprises an axially-extending profile surface which is generally inclined with respect to the longitudinal axis X of the shaft 100. In this embodiment, a forward part 100d of the profile surface (at the left part of the channel 100c in the sense of Figure 2) is curved, and a rearward part 100e of the profile surface (at the right part of the channel 100c in the sense of Figure 2) is linear or straight. In this embodiment, the straight, rearward part 100e of the profile surface is inclined at an angle of 30 degrees to the longitudinal axis X of the shaft 100.
The split ring 300 includes a first part 300a having a first outer diameter, and a second part 300b having a second outer diameter which is greater than the first diameter, so as to provide a flange having a forward face, referred to hereinafter as a thrust surface 300c. The split ring 300 surrounds the circumference of the shaft 100 in the region of the channel 100c. In this embodiment, the split ring 300 comprises two halves which are attached to one another to provide an interior surface which defines a through-bore of the split ring 300 whose diameter varies in the axial direction. In this embodiment, a first portion of the interior surface of the split ring 300 comprises a slope which is shaped to complement the inclined rearward part 100e of the profile surface of the channel 100c and is seated thereon, ensuring a good surface contact between the first portion of the interior surface of the split ring 300 and the rearward part 100e of the profile surface of the channel 100c for transmitting the axial thrust. It will be understood that the first portion of the interior surface of the split ring 300 can take any general shape and need not conform entirely with the profile surface, as long as contact with at least part of the inclined profile surface is sufficient for transmission of the axial thrust. Thus, in this embodiment, part of the first portion of the interior surface of the split ring 300 extends forwardly to overhang part of the profile surface. A second portion of the interior surface of the split ring 300 is in contact with a rearward region of the shaft 100 immediately adjacent the channel 100. Thus, the split ring 300 is partially disposed, or located, in the channel 100c.
The ring-like collar 400 includes a through-bore having a diameter which is substantially the same as the outer diameter of the first part 300a of the split ring 300. Accordingly, the collar 400 is seated snugly over the first part of the split ring 300 and a rearward face of the collar 400 is in abutment with the thrust surface 300c of the second part 300b of the split ring 300. In this embodiment the collar 400 is of single-piece construction. Also in this embodiment the collar 400 is solid.
In this embodiment, the halves of the split ring 300 are joined together in a conventional manner by screws, or a circumferential clamp, or a pivot and bolt arrangement, as described herein above. Alternatively, since the split ring 300 may experience a small radial expansion as it is assembled on the profile surface of the channel 101c, a circumferential clamp or holding mechanism, which can be removed once the collar 400 is positioned around the split ring 300, may be preferred.
The spacer 500a is disposed around the central region of the shaft 100 and extends axially between the bearing 200 and the channel 100c. A forward face of the spacer 500a is in abutment with a rearward face of the bearing 200 and a rearward face of the spacer 500a is located at the region of the channel 100c. In this embodiment, the rearward face of the spacer 500a slightly overhangs the channel 100c. Alternatively, the rearward face of the spacer 500a may extend to the edge of the channel 100c or stop short of the edge. The spacer 500a includes an outer thread on which the nut 500b is threadably engaged. As shown in Figure 2, the nut 500b has been screwed along the spacer 500a such that a rearward face of the nut 500b is in abutment with a forward face of the collar 400. The nut 500b has been tightened against the collar 400 so that the spacer 500a has been urged axially (leftwards in the sense of Figure 2) to locate the bearing 200 on the journal 100b against the abutment face 600a.
When in use in the rolling mill 600, the shaft 100 produces an axial thrust which is transmitted to the first part 300a of the split ring 300 by the rearward part 100e of the profile surface of the circumferential channel 100c. Accordingly an axial force Fa is applied to the thrust face 300c which in turn transmits the force to the collar 400. The axial force Fa urges the interior surface of the first portion 300a of the split ring 300 to ride up along the inclined rearward part 100e of the profile surface of the channel 100c, potentially causing the split ring 300 to move axially along the shaft 100 (rightwards in the sense of Figure 2) and causing a radial force in the split ring 300. Accordingly, the first part 300a of the split ring 300 exerts an outward radial force Fr on the collar 400. The snug-fitting collar 400 counters this radial force Fr to resist or contain radial displacement of the split ring 300, thereby preventing or restricting the split ring 300 from riding along the profile surface of the channel 100c. In this way, axial movement of the split ring 300 along the shaft 100 is prevented, or at least limited, and the bearing 200 remains correctly located on the shaft 100.
In conventional bearing arrangements, the contact face between the split ring and the groove in the shaft is 90 degrees to the longitudinal axis of the shaft and therefore there is no radial load on the split ring and so the bolts (or other devices) which hold the split ring halves together do not need to be particularly strong. In the invention, the radial load on the split ring 300 could not be contained by conventional bolts and the collar 400 is provided for this function.
The stages of assembly of the bearing system will now be described, with particular reference to Figures 3 to 6.
Referring to Figure 3, in a first assembly step 800a the bearing 200 is slid (from right to left in the sense of Figure 3) onto the central region of the shaft 100 such that the forward face of the bearing 200 is brought into abutment with the abutment face 600a. In this condition the inner surface 200a of the bearing 200 encircles the shaft journal 100b. In a further assembly step 800b, the spacer 500a is slid onto the central region of the shaft 100 such that the front face of the spacer 500a is brought into abutment with the rearward face of the bearing 200. In a further assembly step 800c, the nut 500b is screwed fully onto the spacer 500a so as to abut a rearward flange surface of the spacer 500a. (Of course, the nut 500b could already have been screwed onto the spacer 500a before the spacer 500a was slid onto the shaft 100).
Referring now to Figure 4, in a further assembly step 800d the collar 400 is positioned over the thread of the spacer 500a. In a further assembly step 800e, the two halves of the split ring 300 are positioned around the channel 100c and attached together such that the first portion of the interior surface of the split ring 300 is in contact with the rearward part 100e of the profile surface of the channel 100c, and the second portion of the interior surface is in contact with the rearward region of the shaft 100 immediately adjacent the channel 100. Thus, the split ring 300 is partially disposed, or located, in the channel 100c.
Referring now to Figure 5 and also Figure 2, in a further assembly step 800f the collar 400 is slid over the first part 300a of the split ring 300 and the nut 500b is screwed toward the collar 400 so that the rearward face of the nut 500b is brought into abutment with the forward face of the collar 400. As the nut 500b is then tightened, the split ring 300 may move a short axial distance (rightwards in the sense of Figure 2) as the first portion of the interior surface of the split ring 300 is urged to ride along the rearward part 100e of the profile surface of the channel 100c. The axial movement of the split ring 300 is limited by the snug-fitting collar 400, which reacts against the radial expansion force applied to it by the first part 300a of the split ring 300 as the split ring 300 moves along the rearward surface 100e, thereby containing the split ring 300 and limiting its advance along the shaft 100. Further tightening of the nut 500b produces a reaction force which drives the spacer 500a axially along the shaft 100 toward the bearing 200, thereby pressing the forward face of the bearing 200 against the abutment face 600a to locate the bearing 200 in the correct position on the journal 100b. Accordingly, the bearing system is brought into the fully assembled condition shown in Figure 2.
Referring now to Figures 7a and 7b, Finite Element Analysis (FEA) shows that the maximum von-Mises stress in a conventional bearing arrangement (Figure 7a) is 353.64 MPa, whereas in an exemplary bearing arrangement according to the invention (Figure 7b) the maximum is 177.48 MPa. Thus, the invention provides a stress reduction of about 50%, and thereby an improvement in the fatigue life of the shaft.
It will be understood that the invention has been described in relation to its preferred embodiments and may be modified in many different ways without departing from the scope of the invention as defined by the accompanying claims.

Claims (16)

  1. CLAIMS1. A bearing system, comprising: a shaft, having a longitudinal axis about which the shaft can rotate, the shaft including a circumferential channel comprising an axially extending profile surface at least part of which is inclined relative to the longitudinal axis; a bearing, configured to be disposed around the shaft in use; a split ring, configured to be located in the circumferential channel in use so as to be in contact with the inclined profile surface, the split ring including a first part having an outer diameter, and a second part having a greater outer diameter than the first part so as to provide a thrust surface; a collar, including an internal bore configured to accommodate the first part of the split ring in use; and a bearing locator, configured to exert an axial locating force between the split ring and the bearing in order to locate the bearing on the shaft; wherein in use an axial thrust load exerted on the split ring by the shaft is transmitted to the collar by the thrust surface, and the split ring is urged along the inclined profile surface so as to produce a radial load on the split ring which is resisted by the collar.
  2. 2. A bearing system according to claim 1, wherein the bearing locator and the collar comprise a single element.
  3. 3. A bearing system according to claim 1, wherein the bearing locator and the collar comprise separate elements.
  4. 4. A bearing system according to claim 3, wherein the bearing locator comprises: a threaded spacer, configured to be disposed between the bearing and the circumferential channel; and a nut, configured to be screwed on the threaded spacer into abutment with the collar so as to exert the axial locating force.
  5. 5. A bearing system according to claim 4, wherein the threaded spacer is configured such that the nut and the collar can be disposed on the threaded spacer within the axial length of the threaded spacer, so that the split ring can be located in the circumferential channel adjacent the threaded spacer on the shaft.
  6. 6. A bearing system according to any one of claims 1 to 5, wherein the inclined profile surface of the circumferential channel is straight.
  7. 7. A bearing system according to any one of claims 1 to 5, wherein the inclined profile surface of the circumferential channel is curved.
  8. 8. A bearing system according to any one of claims 1 to 5, wherein the inclined profile surface of the circumferential channel is partly straight and partly curved.
  9. 9. A bearing system according to claim 7 or 8, wherein the radius of curvature is constant.
  10. 10. A bearing system according to claim 7 or 8, wherein the radius of curvature is varied.
  11. 11. A bearing system according to any one of claims 6 to 10, wherein the profile surface, or a tangent to the profile surface, is inclined from the longitudinal axis of the shaft by about 1 to 80 degrees, preferably about 1 to 45 degrees, more preferably about 1 to 30 degrees.
  12. 12. A method of assembling a bearing system according to any one of claims 1 to 11, comprising: positioning the bearing onto the shaft; positioning the bearing locator onto the shaft; positioning the collar over the bearing locator; positioning the split ring at least partially in the circumferential channel; positioning the collar over the first part of the split ring; and adjusting the bearing locator so as to exert the axial locating force between the split ring and the bearing in order to locate the bearing on the shaft.
  13. 13. A bearing system, substantially as herein described with reference to figures 2 to 7.
  14. 14. A method of assembling a bearing system, substantially as herein described with reference to figures 2 to 7.Amendments to the claims have been made as followsCLAIMS1. A bearing system, comprising: a shaft, having a longitudinal axis about which the shaft can rotate, the shaft including a circumferential channel comprising an axially extending profile surface at least part of which is inclined relative to the longitudinal axis; a bearing, configured to be disposed around the shaft in use; a split ring, configured to be located in the circumferential channel in use so as to be in contact with the inclined profile surface, the split ring including a first part having an outer diameter, and a second part having a greater outer diameter than the first part so as to provide a thrust surface; a collar, including an internal bore configured to accommodate the first part of the split ring in use; and a bearing locator, configured to exert an axial locating force between the (r) 15 split ring and the bearing in order to locate the bearing on the shaft; wherein in use an axial thrust load exerted on the split ring by the shaft is transmitted to the collar by the thrust surface, and the split ring is urged along the inclined profile surface so as to produce a radial load on the split ring which 00) is resisted by the collar.C\I 20 2. A bearing system according to claim 1, wherein the bearing locator and the collar comprise a single element.3 A bearing system according to claim 1, wherein the bearing locator and the collar comprise separate elements.4. A bearing system according to claim 3, wherein the bearing locator comprises: a threaded spacer, configured to be disposed between the bearing and the circumferential channel; and a nut, configured to be screwed on the threaded spacer into abutment with the collar so as to exert the axial locating force.5. A bearing system according to claim 4, wherein the threaded spacer is configured such that the nut and the collar can be disposed on the threaded spacer within the axial length of the threaded spacer, so that the split ring can be located in the circumferential channel adjacent the threaded spacer on the shaft.6. A bearing system according to any one of claims 1 to 5, wherein the inclined profile surface of the circumferential channel is straight.7. A bearing system according to any one of claims 1 to 5, wherein the inclined profile surface of the circumferential channel is curved.8. A bearing system according to any one of claims 1 to 5, wherein the inclined profile surface of the circumferential channel is partly straight and partly curved.9. A bearing system according to claim 7 or 8, wherein the radius of curvature is constant.00) 10. A bearing system according to claim 7 or 8, wherein the radius of C\I 20 curvature is varied.11. A bearing system according to any one of claims 6 to 10, wherein the profile surface, or a tangent to the profile surface, is inclined from the longitudinal axis of the shaft by about Ito 80 degrees.12. A bearing system according to any one of claims 6 to 10, wherein the profile surface, or a tangent to the profile surface, is inclined from the longitudinal axis of the shaft by about 1 to 45 degrees.13. A bearing system according to any one of claims 6 to 10, wherein the profile surface, or a tangent to the profile surface, is inclined from the longitudinal axis of the shaft by about 1 to 30 degrees.14. A method of assembling a bearing system according to any one of claims 1 to 13, comprising: positioning the bearing onto the shaft; positioning the bearing locator onto the shaft; positioning the collar over the bearing locator; positioning the split ring at least partially in the circumferential channel; positioning the collar over the first part of the split ring; and adjusting the bearing locator so as to exert the axial locating force between the split ring and the bearing in order to locate the bearing on the shaft.
  15. 15. A bearing system, substantially as herein described with reference to figures 2 to 7.
  16. 16. A method of assembling a bearing system, substantially as herein (r) 15 described with reference to figures 2 to 7.CDa) C\I
GB1506277.1A 2015-04-14 2015-04-14 Bearing system and method Active GB2537378B (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB1506277.1A GB2537378B (en) 2015-04-14 2015-04-14 Bearing system and method
PCT/EP2016/057528 WO2016165995A1 (en) 2015-04-14 2016-04-06 Bearing system and method
US15/561,092 US10184516B2 (en) 2015-04-14 2016-04-06 Bearing system and method
KR1020177032832A KR102572161B1 (en) 2015-04-14 2016-04-06 Bearing systems and methods
CN201680021817.4A CN107429749B (en) 2015-04-14 2016-04-06 Bearing arrangement and method
EP16714449.2A EP3283781B1 (en) 2015-04-14 2016-04-06 Bearing system and method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1506277.1A GB2537378B (en) 2015-04-14 2015-04-14 Bearing system and method

Publications (3)

Publication Number Publication Date
GB201506277D0 GB201506277D0 (en) 2015-05-27
GB2537378A true GB2537378A (en) 2016-10-19
GB2537378B GB2537378B (en) 2017-04-26

Family

ID=53333728

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1506277.1A Active GB2537378B (en) 2015-04-14 2015-04-14 Bearing system and method

Country Status (6)

Country Link
US (1) US10184516B2 (en)
EP (1) EP3283781B1 (en)
KR (1) KR102572161B1 (en)
CN (1) CN107429749B (en)
GB (1) GB2537378B (en)
WO (1) WO2016165995A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3789294B1 (en) * 2019-09-04 2023-05-03 Goodrich Actuation Systems SAS Actuator

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3627388A (en) * 1970-09-08 1971-12-14 Morgan Construction Co Hydraulic locking and loosening device for bearing
US3782796A (en) * 1972-12-18 1974-01-01 Morgan Construction Co Retaining means for a bearing assembly
GB2118640A (en) * 1982-04-16 1983-11-02 Skf Kugellagerfabriken Gmbh A combination of a support body and a pulley body and a method of assembling them
WO1990014524A1 (en) * 1989-05-18 1990-11-29 The Broken Hill Proprietary Company Limited Adjustable locking cam assembly

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1754732U (en) * 1957-07-04 1957-10-24 Siemen & Hinsch Gmbh ROLLER BEARING WITH WITHDRAWAL SLEEVE.
US3413022A (en) * 1966-11-14 1968-11-26 Standard Locknut & Lockwasher Self-locking threaded ring assembly
US4012154A (en) * 1973-09-28 1977-03-15 United Technologies Corporation Threadless locking device
US4019824A (en) * 1976-02-03 1977-04-26 Percy Vernon L Positive ring retaining system
US4182578A (en) * 1978-03-24 1980-01-08 Caterpillar Tractor Co. Keeper assembly
US5411337A (en) * 1994-04-26 1995-05-02 Anlock Products And Machine Co. Axially guided locking ring assembly
SE509964C2 (en) * 1996-03-19 1999-03-29 Skf Ab Method and apparatus for axially fixing a ring on a shaft
US6132101A (en) * 1999-07-28 2000-10-17 Voest Alpine Industries, Inc. Roll bearing assembly having integral components
JP4667340B2 (en) * 2006-10-20 2011-04-13 富士機工株式会社 Steering shaft rotation resistance applying device
SE532159C2 (en) 2008-03-12 2009-11-03 Skf Ab A mounting sleeve for mounting a ring on a shaft and a bearing unit including such mounting sleeve
DE102009037273A1 (en) * 2009-08-12 2011-02-17 Sms Siemag Ag Roller bearing retainer
US9249782B2 (en) * 2012-01-31 2016-02-02 General Electric Company Snap ring retention assembly for a main shaft in a wind turbine
JP2013159137A (en) * 2012-02-01 2013-08-19 Ntn Corp Bearing device for wheel

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3627388A (en) * 1970-09-08 1971-12-14 Morgan Construction Co Hydraulic locking and loosening device for bearing
US3782796A (en) * 1972-12-18 1974-01-01 Morgan Construction Co Retaining means for a bearing assembly
GB2118640A (en) * 1982-04-16 1983-11-02 Skf Kugellagerfabriken Gmbh A combination of a support body and a pulley body and a method of assembling them
WO1990014524A1 (en) * 1989-05-18 1990-11-29 The Broken Hill Proprietary Company Limited Adjustable locking cam assembly

Also Published As

Publication number Publication date
EP3283781B1 (en) 2020-02-26
US20180119734A1 (en) 2018-05-03
WO2016165995A1 (en) 2016-10-20
US10184516B2 (en) 2019-01-22
CN107429749B (en) 2019-10-18
KR20170136625A (en) 2017-12-11
CN107429749A (en) 2017-12-01
GB201506277D0 (en) 2015-05-27
KR102572161B1 (en) 2023-08-28
GB2537378B (en) 2017-04-26
EP3283781A1 (en) 2018-02-21

Similar Documents

Publication Publication Date Title
US10086648B2 (en) Bearing device for a wheel
CA2565903C (en) Taper lock bearing assembly
US8757890B2 (en) Method and apparatus for setting rolling element bearings in rolling mills
US7637667B1 (en) Bearing assembly for a steering assembly
US10393252B2 (en) Pulley device for tensioner roller or winding roller
EP0967404B1 (en) Mounting device for a bearing unit
US20160236511A1 (en) Extended length bearing cone system
US4160608A (en) Preloading nut for wedge sleeve
EP3283781B1 (en) Bearing system and method
US20110129345A1 (en) Preloaded propeller blade assembly
US20210277940A1 (en) Rolling bearing precompression method, bearing precompression device, bearing assembly, machine, and vehicle
EP3043081B1 (en) Bearing limiting system and limiting method
GB1562779A (en) Universal joints
KR101990174B1 (en) Rolling-element bearing
EP2860416B1 (en) Ball bearing
KR101454905B1 (en) Wheel bearing and wheel bearing assembly using the same
US10369605B2 (en) Rolling mill roll
US7025185B2 (en) Torque releasing device
US11971072B2 (en) Bearing assembly
EP4092282A1 (en) Bearing assembly
CN212765476U (en) Wheel hub assembly and vehicle
JP2005188547A (en) Power transmitting mechanism
KR102341211B1 (en) Power transmission device
SU1123901A1 (en) Double main transmission of vehicle drive axle
JP2022071682A (en) Wheel bearing and wheel bearing device