GB1594672A - Radial and thrust-type hydrodynamic bearing capable of accommodating misalignment - Google Patents
Radial and thrust-type hydrodynamic bearing capable of accommodating misalignment Download PDFInfo
- Publication number
- GB1594672A GB1594672A GB1949/78A GB194978A GB1594672A GB 1594672 A GB1594672 A GB 1594672A GB 1949/78 A GB1949/78 A GB 1949/78A GB 194978 A GB194978 A GB 194978A GB 1594672 A GB1594672 A GB 1594672A
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- GB
- United Kingdom
- Prior art keywords
- bearing
- face portion
- pad
- swing
- point
- 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.)
- Expired
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/02—Sliding-contact bearings for exclusively rotary movement for radial load only
- F16C17/03—Sliding-contact bearings for exclusively rotary movement for radial load only with tiltably-supported segments, e.g. Michell bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C23/00—Bearings for exclusively rotary movement adjustable for aligning or positioning
- F16C23/02—Sliding-contact bearings
- F16C23/04—Sliding-contact bearings self-adjusting
- F16C23/043—Sliding-contact bearings self-adjusting with spherical surfaces, e.g. spherical plain bearings
- F16C23/045—Sliding-contact bearings self-adjusting with spherical surfaces, e.g. spherical plain bearings for radial load mainly, e.g. radial spherical plain bearings
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Sliding-Contact Bearings (AREA)
- Support Of The Bearing (AREA)
Description
(54) RADIAL AND THRUST-TYPE HYDRODYNAMIC BEARING
CAPABLE OF ACCOMMODATING MISALIGNMENT
(71) I, JEROME GREENE of 1241
Barclay Court, Westlake Village, California 91361, United States of America; a citizen of the United States of America, do hereby declare the invention, for which I pray that a patent may be granted to me, and the method by which it is to be performed, to be particularly described in and by the following statement:- This invention relates to the field of hydrodynamic bearings, and proposes to solve a problem in prior art combined radial and thrust-type bearings using compound curved surfaces, particularly spherically curved bearing surfaces. In addition to being able to handle both radial and thrust loads, the bearing constructed in accordance with the present invention can accommodate angular misalginment between the rotational axis of the moving part of the bearing and the axis of the fixed part of the bearing.
The bearing of the present invention utilizes the principles of operation disclosed in my UX. Patent No. 1463032 entitled "SWING PAD BEARING" and that disclosure is incorporated herein by reference.
In UX. Patent No. 1463032 there is described and claimed a hydro-dynamic bearing arrangement for supporting a movable load applying member in low-friction relationship in the presence of a lubricating fluid medium, said bearing arrangement comprising at least one bearing pad disposed between said movable load applying member and a relatively stationary support structure, the bearing pad including a swingable face portion disposed adjacent said movable member, and means for supporting said face portion for swinging motion about an axis of swinging motion spaced from said face portion and on the same side of said face portion as said movable member, said face portion of each pad being swingable to a dynamically stable inclined position under the combined influences of friction and load forces acting thereon in the presence of a lubricant fluid.
In essence, that patent discloses a hydrodynamic bearing pad including a movable face portion that is adjacent to a relatively movable load applying or supporting surface in the presence of a lubricant, the face portion of the bearing pad being mounted for swinging motion relative to a base element underlying the surface portion about a swinging axis or center located toward the relatively movable load applying or supporting surface and away from the face portion of the bearing pad to enable generation of the lubricant wedge. Motion of the movable face portion of the pad relative to the load applying or supporting surface under operational conditions as described in that patent, causes the face portion to swing in minute amounts to an inclined position relative to the load applying or supporting surface under the combined influences of load and friction forces to produce a wedge-shaped gap that converges in the direction of motion of the load applying or supporting surface relative to the face portion of the pad. Multiple such bearing pads are normally provided in a typical bearing installation for supporting a relatively moving load apply or supporting member. Lubricant is drawn into the multiple gaps as a result of relative motion between the bearing surfaces and hydrodynamic action maintain the face portions of the pads and the adjacent relatively moving surface out of contact with each other virtually instantaneously upon onset of relative motion, and during the operation of the bearing.
The shape of the lubricant wedge associated with each bearing pad self-adjusts during operation of the bearing under varying load and speed conditions due to its unique design. Specifically, the face portion of each pad is joined to an underlying base element along an arcuate interface having a center of curvature located substantially at the desired center of swinging motion of the face portion. A curved, laminated, elastomernonelastomeric material is disposed between the face portion and the underlying base element of each pad, and is bonded on each side to both elements. The laminate material is compliant in the shear direction (parallel to the arcuate interface between the face portion and the underlying base element) but is essentially rigid in a radial sense (perpendicular to the arcuate interface).
Therefore, the face portion of each bearing pad can readily and is actually forced to swing to a slightly inclined position about the center or axis of swing under the influence of friction and load forces applied to its surface by the load supporting member while still maintaining its basic position in the bearing assembly.
My earlier patent referenced above discloses radial and thrust bearing embodiments utilizing the swing pad concept. However, the present invention is intended to utilize the same principle in a combined radial and thrust bearing that utilizes compound curved bearing surfaces, the swing pad bearing overcoming problems encountered in the prior art in situations where it is desired to use such a bearing for supporting high radial loads.
More specifically, it is well known that the rotary part of plain journal radial bearings with lubricated continuous sliding surfaces actually runs slightly eccentric with respect to the longitudinal axis of the bearing, and this eccentricity permits the generation of a wedge of lubricant between the relatively moving bearing surfaces. The wedge of lubricant, through pressures generated by hydrodynamic action, in turn keeps the bearing surfaces apart so that surface-to-surface contact is avoided and frictional resistance to motion is minimized.
In situations where a sliding bearing having both radial and thrust capacity is desired, it has been proposed to use compound curved surfaces of various forms (e.g., a ball in a socket). The problem here is that the symmetrical compound curvature of the continuous bearing surfaces tends to prevent the moving element of the bearing from assuming its eccentric loaded rotating position at which the lubricant wedge is formed when the bearing is loaded in a thrust sense. The thrust bearing surface, being uniformly curved about the rotation axis, tends to hold the rotating element at the center of the bearing and therefore a radial load supporting lubricant wedge cannot be developed by the bearing because hydrodynamic pressures are not generated in the lubricant film to the extent necessary to keep the bearing surfaces apart.
A hydrodynamic tilting pad arrangement could be envisioned for such an application, but the required compound curvature of the bearing surface of the tilting pad, along with the variable nature of the radial and thrust loads, results in the position of the center of pressure acting on the tilting pad elements to be unpredictable. Since the center of pressure in a tilting pad bearing arrangement must be virtually in line with the tilt pivot point to prevent instability of the tilting segment of the bearing, clearly a tilting pad bearing has deficiencies which limit its application in a bearing of the type presently under consideration.
According to the present invention there is provided a fluid film bearing assembly comprising:
(a) a plurality of bearing pads disposed in a cylindrical array about a longitudinal axis;
(b) support means for each pad;
(c) a movable face portion on each pad;
(d) the face portions having spherically curved bearing surfaces having a common center of curvature lying at a point on said longitudinal axis;
(e) each face portion being mounted on its respective support means by means positively restricting it to swing to an inclined position relative to the support means in any direction about a center of swinging motion or swing point located outside of the bearing pad between said longitudinal axis and the said surface of the face portion of the pad, the swing point also lying on the radius extending from said common center of curvature to the said surface when said face portion is in its normal at-rest position, said face portion also being restricted against any other motion relative to said support means.
Also in accordance with the present invention there is provided a fluid film bearing assembly comprising:
(a) a plurality of bearing pads disposed in a cylindrical array about a longitudinal axis;
(b) support means for each pad;
(c) a movable face portion on each pad;
(d) the face portions having spherically curved bearing surfaces having a common center of curvature lying at a point on said longitudinal axis;
(e) each face portion being mounted on its respective support means by means positively restricting it to swing to an inclined position relative to the support means in any direction about a center of swinging motion or swing point located outside of the bearing pad between said longitudinal axis and the said surface of the face portion of the pad, the swing point also lying on the radius extending from said common center of curvature to the said surface when said face portion is in its normal at-rest position, said face portion also being restricted against any other motion relative to said support means, and said support being arranged to elastically urge said face portion towards its at-rest position when it is swung from such position.
The present invention utilizes the principle of operation of the hydrodynamic swing pad bearing disclosed in the patent identified previously in the radial and thrust bearing construction using compound curved bearing surfaces that are arranged so that the bearing can accommodate misalignment between the moving parts. The face portions of the pads can swing about a point (swing point) under friction and load forces to enable generation of lubricant wedge films by the relative motion of the bearing surfaces. The relative position of the center of pressure acting on each bearing pad with respect to the face of the pad is uncritical within wide design limits, because friction and pressure forces acting on each pad stabilize the position of the face portion of the pad about its respective swing point to maintain the lubricant wedge during operation of the bearing.
Specifically, a cylindrical array or group of swing pad bearing elements is provided adjacent the spherical outer surface portion of a load applying or supporting member, the array of bearing pads and the load applying or supporting member being relatively rotatable with respect to each other about a longitudinal axis of rotation. The bearing surfaces of the face portions of the bearing pads correspond in curvature to the outer curvature of the load carrying part of the load applying or supporting member, and the bearing pad surfaces have centers of curvature that are common with each other and with the center of curvature of the bearing surface of the load applying or supporting member. The face portions of the pads are joined to supporting base elements along spherically curved, low friction interfaces that limit motion of the face portion of the pads td swinging motion, preferably through a metallic-elastomer laminate material that is relatively soft and compliant in the shear direction (parallel to the arcuate interface) but rigid in the radial direction (normal to the arcuate interface). The radius of curvature of the interface is shorter than the radius of curvature of the outer periphery of the load applying or supporting member, and likewise shorter than the radius of curvature of the bearing surface of the bearing pad.
Thus, the face portions of each bearing pad can swing about a swing point or center that
corresponds essentially to the center of curvature of the interface between the face portion of the pad and the underlying base element. The center of curvature of the interface of each pad assembly lies at a point located along the radius of the spherical bearing surfaces of the bearing pad, somewhere between the center of curvature of that surface and the surface itself, preferably approximately mid-way along the radius that intersects the pad surface, preferably at approximately its center. The center of swinging motion of the face portions of each group of bearing pads thus lie on radii extending between the common centers of curvature referred to above and the bearing surfaces of the pads.
The bearing surfaces of the pads are immersed in a suitable lubricant so that when relatively motion occurs between the load applying or supporting member and the bearing pads, the face portions, under the influence of friction and load forces acting thereon, swing to dynamically stable positions in any direction to generate wedge-shaped lubricant film gaps between the relatively moving surfaces. Due to the arrangement of the mating spherical bearing surfaces, thrust loads as well as radial loads can be supported by the swing pads, and misalignment between the rotational axis of the load applying or supporting member and the longitudinal axis of the cylindrical array of bearing pads can be accommodated. The wedge-shaped lubricant films are maintained at all times regardless of the direction of loading on the bearing surfaces.
Figure 1 is a diagrammatic plan view of part of a bearing assembly embodying my invention;
Figure 2 is an elevational view taken generally along lines Il-Il of Figure 1, with the central load supporting member removed for clarity;
Figure 3 is an enlarged detail view of a bearing pad assembly; and
Figure 4 is a diagrammatic representation of the bearing in operation.
With reference to the drawings, a bearing assembly 10 is shown in Figure 1 connected to a load applying or supporting member 12 which extends along a longitudinal axis 14.
The bearing assembly 10 includes an outer casing 16 and a set of connected base elements 18 which underlie a cylindrical array of face portions 20 of the bearing assembly spaced about the longitudinal axis 14. The connected base elements 18 preferably are constructed as a pair of split sleeves joined along lines 22 for enabling assembly of the bearing about the load applying or supporting member 12. Each face portion 20 is connected to its respective underlying base section 18 through an elastomeric-inelastic interface comprising, in the preferred mode, a metal-elastomer laminate, as shown in Figure 3, where the metal layers are shown as 24 and the elastomeric layers, i.e., rubber, are shown as 26. The combination of the face portion 20, the underlying base element 18 and the intermediate laminate material 24, 26 is referred to herein as a bearing pad.
The base element 18 could be made up of individual segments (not illustrated) attached to a casing such as 16 connected to individual face portions 20 through individual laminations 24, 26. However, the illustrated embodiment shows a common member 18 having spaced curved interface areas for receiving individual face portions 20 and intermediate laminations 24, 26 bonded on either side to the face portions and the base element. The face portions 20 each have concave spherically curved bearing surfaces 30 that conform in curvature to a spherical portion 32 of the load applying or supporting member 12 (see Figure 1). The surfaces 30 have a common center of curvature 33 lying on axis 14, and center 33 corresponds to the center of curvature of the peripheral surface portion 32 of member 12. The casing 16 and the bearing pads usually are held fixed against rotation and they support load member 12 for rotation about an axis generally coincidental with axis 14, in which case member 12 is a "load applying" member. However, it will be readily understood that this invention is not limited in any sense to such an arrangement, and member 12 could just as well be fixed for supporting load carrying bearing pads for rotation relative thereto about axis 14. Thus, the term "load applying or supporting member" with reference to member 12 is not intended to be an alternative recitation in the specification and claims constituting this application, but rather a singular expression relating to the structure corresponding to member 12, irrespective of its specific function in a particular application.
The surfaces 34 (see Figure 1) of base elements 18 underlying each face portion 20 and the underlying surface 35 of each face portion 20 are called interface surfaces and are spherically curved about a center of curvature 40 located along a radius Rl extending from the point 33 to the approximate center of bearing surface 30 of each face portion 20 of the bearing pads when the face portion is at its at rest position. Thus, for example, the radius R2 of the surface 35 is shorter than the radius R1 of the surface 30.
The centers of curvature 40 of interfaces 34 and 35 of the bearing pads are disposed preferably about a locus that is equidistant from the axis of rotation 14, so that the radius R2, for example, of each surface 35 is identical for all of the bearing pads, although this is not an absolute requirement. As illustrated, the surfaces 34 and 35 are curves that are concentric about point 40, which represents the swinging axis of each face portion 20 of the bearing pads. As shown, metal lamina 24 are likewise curved so that they are parallel to the surfaces 34 and 35.
Upon relative movement between member 12 and the face portions 20, the latter, because of friction forces, will immediately tend to swing about their respective swing axes 40 to an inclined position relative to the base 18 and the outer surface of the spherical portion 32, as shown in Figure 4.
The laminates 24, 26 being compliant in shear but substantially rigid in a radial sense readily accommodate the swinging motion of the face portions 20 of each pad. In actuality, the swinging motion is quite miniscule so that the space between the load applying or supporting member 12 and the bearing pads is maintained despite the very slight swinging movement of each face portion 20. In addition, eccentric loads (non-radial to interface 34, 35) applied to the face portion 20 cause them to swing in a direction tending to cause the load vector to be radially aligned with the interface surface curvature. The total swinging motion is small and is always towards the adjacent bearing surface in the direction of swinging motion.
Swinging motion stabilizes the face portion so that the net forces acting thereon are in balance continuously, as explained in United
States Patent No. 3,939,691.
In Figure 4, a fluid lubricant is provided between the load applying or supporting member portion 32 and the bearing pads so that a hydrodynamic lubricant wedge is maintained between the face portions 20 and the member 32 in the manner of a hydrodynamic fluid film bearing. Since the face portions 20 are supported upon spherical underlying surfaces, each face portion 20 can swing to a stable, balanced position under the combined radial and thrust components of friction and load forces. The ball joint-like relationship between spherical portion 32 of load applying or supporting member 12 and each bearing pad allows the bearing to handle thrust loads and to accommodate angular misalignment between the axis 14 of the cylindrical array of bearing pads and the longitudinal axis of load applying or supporting member 12. The latter axis, of course, will pass through point 33.
It should be understood that the relative sizes of the thickness of the laminations 24, 26, as well as the wedge-shaped gaps 42 in
Figure 4 all have been exaggerated for the sake of clarity.
It is thus evident that the swing pad elements of the present invention will automatically swing to stable positions to generate wedge films of lubricant regardless of radial and thrust load forces. Radial loads cause the bearing surfaces to swing about their swing points in directions parallel to the direction of motion of the adjacent bearing surface of the load applying or supporting member, while thrust loads cause the movable bearing face elements to swing back towards the source of the thrust load so that the fluid film pressures between the moving surfaces are in balance. Most importantly, thrust loads do not disturb the ability of the bearing to generate the desired lubricant wedge.
Various modifications of the illustrated embodiment of the invention are possible, and only an exemplary, presently preferred construction has been disclosed. For example, as described in my previous patent relating to the swing pad bearing, the interface between the face portions 20 and the underlying base elements 18 could comprise contiguous mating surfaces separated by a low friction film, as as long as the face portion was limited strictly to swinging motion about the swing point. The principle of operation of the bearing pads would still be the same for purposes of the present invention. Likewise, the construction of the load applying or supporting member 12 could be varied in numerous manners while still providing a spherical portion 32 adjacent the cylindrical array of bearing pads. It is furthermore envisioned that multiple circular arrays of bearing pads could be provided about a single spherical load supporting member portion 32 or a single set of pads could be located in an area other than about a diameter of the spherical portion of the member 32.
More laminations 24, 26 could be provided in the interface area. However, all of these modifactions are envisioned as being fully within the scope of my invention disclosed in the present application, which invention is to be limited only by the scope of the claims appended hereto.
WHAT I CLAIM IS:
1. A fluid film bearing assembly comprising:
(a) a plurality of bearing pads disposed in a cylindrical array about a longitudinal axis;
(b) support means for each pad;
(c) a movable face portion on each pad;
(d) the face portions having spherically curved bearing surfaces having a common center of curvature lying at a point on said longitudinal axis;
(e) each face portion being mounted on its respective support means by means positively restricting it to swing to an inclined position relative to the support means in any direction about a center of swinging motion or swing point located outside of the bearing pad between said longitudinal axis and the said surface of the face portion of the pad, the swing point also lying on the radius extending from said common center of curvature to the said surface when said face portion is in its normal at-rest position, said face portion also being restricted against any other motion relative to said support means.
2. A bearing assembly as claimed in Claim 1, wherein the swing point of each face portion lies on the radius extending from said common point to the said surface and intersecting said surface at approximately its at-rest center point.
3. A bearing assembly as claimed in Claim 1, wherein the swing points of the bearing pads are located radially equidistant from said longitudinal axis.
4. A bearing assembly as claimed in Claim 1, wherein each face portion is connected to its respective support means along parallel arcuate interface surfaces which have their centers of curvature at substantially the swing point of the bearing face portions.
5. A bearing assembly as claimed in Claim 4, wherein said restricting means comprises an elastomer-inelastic curved laminate material provided between the interface surfaces and bonded to them on either side, the laminate being compliant in the shear direction parallel to the interface surfaces but substantially rigid in a direction radially normal to said interface surfaces.
6. A bearing assembly as claimed in Claim 5, wherein the surface portions of said bearing pads are immersed in a fluid lubricant and including a load applying or supporting member cooperating with the bearing assembly, said member having a continuous spherically curved surface portion contiguous to the bearing surfaces of the bearing pads, and corresponding in curvature to said bearing surfaces.
7. A bearing assembly as claimed in Claim 6, wherein said load applying or supporting member is rotatable about a longitudinal axis passing through said common point and the supports for said bearing pads are non-rotative relative to said longitudinal axis.
8. A bearing assembly as claimed in Claim 7, wherein the bearing pads are located about a diameter of the spherically curved surface portion of the load supporting member.
9. A fluid film bearing assembly comprising:
(a) a plurality of bearing pads disposed in a cylindrical array about a longitudinal axis;
(b) support means for each pad;
(c) a movable face portion on each pad;
(d) the face portions having spherically curved bearing surfaces having a common center of curvature lying at a point on said longitudinal axis;
(e) each face portion being mounted on its respective support means by means positively restricting it to swing to an inclined position relative to the support means in any direction about a center of swinging motion or swing point located outside of the bearing pad between said longitudinal axis and the said surface of the face portion of the pad, the swing point also lying on the radius extending from said common center of curvature to the said surface when said face portion is in its normal at-rest position, said face portion also being restricted against any other motion relative to said support means, and said support being arranged to elastically urge said face portion towards its at-rest position when it is swung away from such position.
10. A bearing assembly as claimed in Claim 5, wherein the swing point of each face portion lies on the radius extending from said common point to the said surface and intersecting said surface at approximately its at-rest center point.
11. A bearing assembly as claimed in Claim 5, wherein the swing points of the bearing pads are located radially equidistant from said longitudinal axis.
12. A bearing assembly as claimed in Claim 5, wherein each face portion is connected to its respective support means along parallel arcuate interface surfaces which have their centers of curvature at substantially the swing point of the bearing face portions.
13. A fluid film bearing assembly as claimed in any preceding claim substantially as herein before described and illustrated.
**WARNING** end of DESC field may overlap start of CLMS **.
Claims (13)
1. A fluid film bearing assembly comprising:
(a) a plurality of bearing pads disposed in a cylindrical array about a longitudinal axis;
(b) support means for each pad;
(c) a movable face portion on each pad;
(d) the face portions having spherically curved bearing surfaces having a common center of curvature lying at a point on said longitudinal axis;
(e) each face portion being mounted on its respective support means by means positively restricting it to swing to an inclined position relative to the support means in any direction about a center of swinging motion or swing point located outside of the bearing pad between said longitudinal axis and the said surface of the face portion of the pad, the swing point also lying on the radius extending from said common center of curvature to the said surface when said face portion is in its normal at-rest position, said face portion also being restricted against any other motion relative to said support means.
2. A bearing assembly as claimed in Claim 1, wherein the swing point of each face portion lies on the radius extending from said common point to the said surface and intersecting said surface at approximately its at-rest center point.
3. A bearing assembly as claimed in Claim 1, wherein the swing points of the bearing pads are located radially equidistant from said longitudinal axis.
4. A bearing assembly as claimed in Claim 1, wherein each face portion is connected to its respective support means along parallel arcuate interface surfaces which have their centers of curvature at substantially the swing point of the bearing face portions.
5. A bearing assembly as claimed in Claim 4, wherein said restricting means comprises an elastomer-inelastic curved laminate material provided between the interface surfaces and bonded to them on either side, the laminate being compliant in the shear direction parallel to the interface surfaces but substantially rigid in a direction radially normal to said interface surfaces.
6. A bearing assembly as claimed in Claim 5, wherein the surface portions of said bearing pads are immersed in a fluid lubricant and including a load applying or supporting member cooperating with the bearing assembly, said member having a continuous spherically curved surface portion contiguous to the bearing surfaces of the bearing pads, and corresponding in curvature to said bearing surfaces.
7. A bearing assembly as claimed in Claim 6, wherein said load applying or supporting member is rotatable about a longitudinal axis passing through said common point and the supports for said bearing pads are non-rotative relative to said longitudinal axis.
8. A bearing assembly as claimed in Claim 7, wherein the bearing pads are located about a diameter of the spherically curved surface portion of the load supporting member.
9. A fluid film bearing assembly comprising:
(a) a plurality of bearing pads disposed in a cylindrical array about a longitudinal axis;
(b) support means for each pad;
(c) a movable face portion on each pad;
(d) the face portions having spherically curved bearing surfaces having a common center of curvature lying at a point on said longitudinal axis;
(e) each face portion being mounted on its respective support means by means positively restricting it to swing to an inclined position relative to the support means in any direction about a center of swinging motion or swing point located outside of the bearing pad between said longitudinal axis and the said surface of the face portion of the pad, the swing point also lying on the radius extending from said common center of curvature to the said surface when said face portion is in its normal at-rest position, said face portion also being restricted against any other motion relative to said support means, and said support being arranged to elastically urge said face portion towards its at-rest position when it is swung away from such position.
10. A bearing assembly as claimed in Claim 5, wherein the swing point of each face portion lies on the radius extending from said common point to the said surface and intersecting said surface at approximately its at-rest center point.
11. A bearing assembly as claimed in Claim 5, wherein the swing points of the bearing pads are located radially equidistant from said longitudinal axis.
12. A bearing assembly as claimed in Claim 5, wherein each face portion is connected to its respective support means along parallel arcuate interface surfaces which have their centers of curvature at substantially the swing point of the bearing face portions.
13. A fluid film bearing assembly as claimed in any preceding claim substantially as herein before described and illustrated.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1949/78A GB1594672A (en) | 1978-01-18 | 1978-01-18 | Radial and thrust-type hydrodynamic bearing capable of accommodating misalignment |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1949/78A GB1594672A (en) | 1978-01-18 | 1978-01-18 | Radial and thrust-type hydrodynamic bearing capable of accommodating misalignment |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1594672A true GB1594672A (en) | 1981-08-05 |
Family
ID=9730892
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1949/78A Expired GB1594672A (en) | 1978-01-18 | 1978-01-18 | Radial and thrust-type hydrodynamic bearing capable of accommodating misalignment |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1594672A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2273746A (en) * | 1992-11-12 | 1994-06-29 | Michael John Neale | A spherical plain bearing assembly with pads |
CN102691721A (en) * | 2012-06-07 | 2012-09-26 | 上海大隆机器厂有限公司 | Tilting pad thrust bearing for twin-screw compressor |
CN110131307A (en) * | 2019-05-16 | 2019-08-16 | 福建龙溪轴承(集团)股份有限公司 | A kind of moulding type self-lubricating knuckle bearing manufacturing method |
-
1978
- 1978-01-18 GB GB1949/78A patent/GB1594672A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2273746A (en) * | 1992-11-12 | 1994-06-29 | Michael John Neale | A spherical plain bearing assembly with pads |
CN102691721A (en) * | 2012-06-07 | 2012-09-26 | 上海大隆机器厂有限公司 | Tilting pad thrust bearing for twin-screw compressor |
CN110131307A (en) * | 2019-05-16 | 2019-08-16 | 福建龙溪轴承(集团)股份有限公司 | A kind of moulding type self-lubricating knuckle bearing manufacturing method |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19940118 |