WO1997025543A1 - Grooved hydrodynamic thrust bearing - Google Patents
Grooved hydrodynamic thrust bearing Download PDFInfo
- Publication number
- WO1997025543A1 WO1997025543A1 PCT/US1996/016155 US9616155W WO9725543A1 WO 1997025543 A1 WO1997025543 A1 WO 1997025543A1 US 9616155 W US9616155 W US 9616155W WO 9725543 A1 WO9725543 A1 WO 9725543A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- bearing
- continuous
- grooved
- thrust
- hydrodynamic
- Prior art date
Links
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
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/10—Construction relative to lubrication
- F16C33/1025—Construction relative to lubrication with liquid, e.g. oil, as lubricant
- F16C33/106—Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid
- F16C33/107—Grooves for generating pressure
-
- 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
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/10—Construction relative to lubrication
-
- 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
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
-
- 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
- F16C17/10—Sliding-contact bearings for exclusively rotary movement for both radial and axial load
- F16C17/102—Sliding-contact bearings for exclusively rotary movement for both radial and axial load with grooves in the bearing surface to generate hydrodynamic pressure
-
- 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
- F16C17/10—Sliding-contact bearings for exclusively rotary movement for both radial and axial load
- F16C17/102—Sliding-contact bearings for exclusively rotary movement for both radial and axial load with grooves in the bearing surface to generate hydrodynamic pressure
- F16C17/107—Sliding-contact bearings for exclusively rotary movement for both radial and axial load with grooves in the bearing surface to generate hydrodynamic pressure with at least one surface for radial load and at least one surface for axial load
Definitions
- the present invention relates to hydrodynamic thrust bearing configuration for a spindle motor assembly. More specifically, the invention relates to the groove configuration of a hydrodynamic thrust bearing for use in a computer hard disc drive spindle motor assembly.
- Computer hard disc drives generally comprise an array of magnetic discs mounted to a spindle motor assembly. Data is written to, and read from, each magnetic disc by means of a read/write head located at the end of an arm which extends between the discs. Positioning of the arm is accomplished by means of a voice coil motor under the control of disc drive control electronics.
- the array of magnetic discs is mounted to a hub of the spindle motor assembly.
- the hub is mounted for rotation with respect to a base of the spindle motor assembly by means of a bearing arrangement. In use, the hub is rotated by means of an electromagnetic motor.
- the bearing arrangement In order to facilitate the accurate positioning of the read/write heads between the magnetic discs, the bearing arrangement is required to run substantially vibration- free and to have a small deflection under the application of external loads (i.e., have a high bearing stiffness).
- The-bearing arrangement is also expected to have a long, maintenance-free service life.
- the continuous trend of miniaturization in the computer industry has meant that the above functions have to be accomplished by a bearing arrangement which occupies as little volume as possible.
- the bearing arrangements used in computer disc drive spindle motor assemblies are often hydrodynamic bearing arrangements, which include at least one hydrodynamic thrust bearing.
- the thrust bearing comprises a thrust plate and an opposed counter plate, each of which define a bearing surface. Either one of the bearing surfaces is formed with a pattern of grooves. The two bearing surfaces are separated in use by a film of lubricant. Pressures generated in the lubricant by the relative rotation of the bearing surfaces keep the bearing surfaces apart and ensure smooth rotation of the bearing arrangement.
- the axial load bearing capacity and other static and dynamic characteristics of the thrust bearing depend on the pressure rise in the lubricant film and on the distribution of pressure across the thrust bearing.
- the pressure rise and distribution in turn depend on the design of the grooving pattern, e.g. the angle of the grooves, the groove pitch ratio, the groove depth and the center radius of the thrust or counter plate.
- the present invention provides a grooved hydrodynamic thrust bearing comprising first and second bearing surfaces.
- the first and second bearing surfaces are rotatable relative to one another and are separated by a bearing fluid.
- the first bearing surface defines a plurality of continuous lands extending from an inner radius to an outer radius. Adjacent continuous lands define between them a continuous groove having, an approximately constant depth and extending in unbroken fashion between the inner radius and the outer radius.
- the continuous groove has an undivided portion in an inner annulus of the first bearing surface and a divided portion in an outer annulus of the first bearing surface, and is divided in the divided portion by an intermediate land located between the two adjacent continuous lands.
- the divided portion of the continuous groove communicates in unbroken fashion with the undivided portion of the continuous groove.
- Fig. 1 is a cross section through a spindle motor assembly incorporating a hydrodynamic thrust bearing according to the invention
- Fig. 2 is a schematic perspective view of one of the surfaces of a prior art hydrodynamic thrust bearing
- Fig. 3 is a perspective view of the pressure distribution created in the bearing fluid by the rotation of the hydrodynamic thrust bearing surface of Fig. 2;
- Fig. 4 is a graph illustrating the general relationship between the number of grooves formed in a hydrodynamic bearing surface, the ease of manufacture of the bearing surface, and bearing performance;
- Figs. 5(a), (b) and (c) show the stress distributions created in solid materials under certain loading conditions, to illustrate the stresses caused in punch features when forming grooved surfaces;
- Fig. 6 is a schematic perspective view of one of the surfaces of a second prior art hydrodynamic thrust bearing
- Fig. 7 is a perspective view of the pressure distribution created in the bearing fluid by the rotation of the hydrodynamic thrust bearing surface of Fig. 6;
- Fig. 8 is a schematic perspective view of one of the surfaces of a hydrodynamic thrust bearing according to the invention
- Fig. 9 is a plan view of one of the bearing surfaces of the best mode hydrodynamic thrust bearing according to the invention.
- Fig. 10 is a perspective view of the pressure distribution created in the bearing fluid by the rotation of the hydrodynamic thrust bearing surface of Fig. 8;
- Fig. 11 is a graph illustrating the relationship between groove angle and bearing performance for a hydrodynamic bearing according to the invention.
- Fig. 12 is a graph illustrating the relationship between groove ratio and bearing performance for a hydrodynamic bearing according to the invention.
- Fig. 13 is a graph illustrating the relationship between groove depth and bearing performance for a hydrodynamic bearing according to the invention.
- Fig. 14 is a graph illustrating the relationship between center radius and bearing performance for a hydrodynamic bearing according to the invention.
- Fig. 15 is a graph illustrating the relationship between the pressure differential across a hydrodynamic bearing according to the invention and the flow rate across the bearing;
- Fig. 16 is a graph illustrating the pressure distributions created by the bearing surfaces illustrated in Figs. 2, 6, and 8.
- FIG. 1 illustrates a cross section through a spindle motor assembly incorporating a hydrodynamic thrust bearing according to the invention.
- the spindle motor assembly generally indicated by the numeral 10, comprises a base 12 and a hub assembly 13.
- a shaft 14 is mounted to the base 12 by means of a nut 16.
- the outer surface of the shaft 14 and the adjacent bore of a journal 18 together form a hydrodynamic journal bearing 20.
- the hydrodynamic journal bearing 20 includes a grooved surface provided on the shaft 14 or on the bore of the journal 18.
- the journal bearing 20 supports the journal 18 for rotation relative to the shaft 14 about axis 22.
- a thrust plate 24 is press-fitted to one end of the shaft 14 and extends transversely to the shaft 14.
- the thrust plate 24 defines a first thrust surface which, together with an adjacent thrust surface on the journal 18, defines a first hydrodynamic thrust bearing 26.
- a counter plate 28 is press-fitted to the journal 18 adjacent to the thrust plate 24.
- the counter plate 28 defines a counter plate thrust surface which, together with a second thrust surface defined by the thrust plate 24 , forms a second hydrodynamic thrust bearing 30.
- the counter plate 28 is sealed to the journal 18 by means of an O-ring 32.
- the first and second hydrodynamic thrust bearings 26, 30 each include a grooved bearing surface as described below with reference to Fig. 9. In this embodiment of the hydrodynamic bearing arrangement, these grooved surfaces are provided on the thrust plate 26. They could however alternatively be provided on the counter plate 30 and/or the adjacent surface of the journal 18.
- a hub 34 is fitted around the journal 26. The hub 34 supports an array of magnetic discs (not shown).
- the hub assembly 13 is rotated with respect to the base 12 in use by means of an electromagnetic motor.
- the electromagnetic motor comprises a stator assembly 36 mounted to the base 12, and a magnet 38 mounted to the journal 18.
- the hydrodynamic thrust bearings 26 and 30 prevent any substantial linear movement of journal 18 relative to shaft 14 along axis 22.
- a hydrodynamic bearing can best be understood by reference to Fig. 2, which illustrates a schematic perspective view of one of the surfaces of a prior art hydrodynamic thrust bearing.
- the illustrated hydrodynamic bearing surface generally indicated by the numeral 60, comprises a series of alternating grooves 62 and lands 64.
- the diameter of the hydrodynamic bearing surface 60 and the depth of the grooves 62 have been greatly exaggerated.
- Each groove 62 and land 64 comprises a leg which extends outward from the inner radius 66 of the hydrodynamic bearing surface 60 and a leg which extends inward from the outer radius 68 of the hydrodynamic bearing surface 60.
- the two legs meet in a point at an intermediate radius 70 which is referred to in the art as the center radius.
- the plurality of grooves 62 and lands 64 together form a curved herringbone pattern as illustrated in the figure.
- a hydrodynamic thrust bearing is formed when the bearing surface 60 is placed adjacent to an opposed bearing surface with a film of lubricant between the two surfaces.
- the bearing surface 60 is then rotated in the direction 72, that is, against the herringbone pattern, the grooves 62 and lands 64 tend to draw lubricant from the inner and outer radii 66 and 68 towards the points of the herringbone pattern at the center radius 70. This creates a pressure distribution within the lubricant and across the bearing surface 60 which serves to keep the two bearing surfaces apart under external loading.
- Fig. 3 The pressure distribution created across a hydrodynamic bearing incorporating the hydrodynamic bearing surface 60, which has eight grooves, is illustrated in Fig. 3.
- the bearing arrangement has been loaded with 14.2 N, and provides an axial bearing stiffness of 4260 kN/m and a bearing rocking stiffness of 14.27 Nm/rad.
- Fig. 5(a) illustrates the stress distribution across a flat surface 90 when a sphere 92 is pressed against the surface 90 with a force F.
- the stress distribution 94 has an inverted bell shape, with a peak directly under the center of the sphere 92.
- Fig. 5(b) illustrates the stress distribution when a sphere 96 is pressed against the corner of a block 98 with a force F.
- the stress distribution follows the previous inverted bell shape in the block as indicated by the reference numeral 100, with a sha ⁇ increase in the stress distribution near the edge 102, as indicated by the reference numeral 104.
- the stress distribution in the punch can be approximated as the sum of two mirror images of the stress distributions 104 and 100 in Fig. 5(b).
- the resulting stress distribution is illustrated in Fig. 5(c) by the reference numeral 106.
- the width "d" of the punch 108 decreases, as would be required to form narrower grooves, the average stress across the punch increases rapidly as the edge stress distribution 104 becomes dominant.
- the narrow grooves require narrower punch (or die) features to form them.
- the narrower punch features experience much greater stresses, which reduces punch life. This in turn decreases the ease of manufacturing of the grooved bearing surface.
- FIG. 6 Another prior art hydrodynamic bearing surface having twelve grooves is shown schematically in Fig. 6, and the pressure distribution created by this bearing surface is shown in Fig. 7.
- the bearing arrangement has also been loaded with 14.2 N, and provides an axial bearing stiffness of 4560 kN/m and a bearing rocking stiffness of 14.95 Nm rad, an increase over the Fig. 2 configuration.
- the bearing surface of a hydrodynamic thrust bearing according to the invention is shown in schematic perspective view in Fig. 8, and in plan view in Fig. 9.
- Fig. 8 For purposes of convenience, features which are common to the bearing surfaces of Figs. 8 and 9 have been indicated by the same reference numeral.
- the continuous lands 122 extend from an inner radius 124 of the bearing surface 120, to an outer radius 126. Adjacent ones of the continuous lands 122 define between them a continuous groove 128 having an approximately constant depth, and extending in unbroken fashion between the inner radius 124 and the outer radius 126.
- each continuous groove 128 comprises an undivided portion 130 in an inner annulus of the bearing surface 120 , and a divided portion 132 in an outer annulus of the bearing surface 120.
- the continuous groove is divided in the divided portion 132 by an intermediate land 134 located between the two adjacent continuous lands 122.
- the divided portion 132 of the continuous groove 128 communicates in unbroken fashion with the undivided portion 130 of the continuous groove 128. This ensures that bearing lubricant can flow substantially unrestricted along the continuous groove between the inner and outer radii 124, 126. This smooth flow is believed to improve bearing performance, and ensures that there is not an undesirably high buildup of pressure or the occurrence of cavitation at any location across the bearing surface, which could increase the stresses experienced by the continuous lands 122 or the intermediate lands 134.
- the continuous lands 122 each comprise a first leg 136 located in an outer annulus of the bearing surface 120, and a second leg 138 located in an inner annulus of the bearing surface 120, the first and second legs meeting at a center radius 140.
- the first and second legs 136, 138 are angled with respect to each other, and the continuous lands 122 define together with adjacent continuous lands 122, a curved herringbone pattern as illustrated in the figures.
- Fig. 10 The pressure distribution created by the Fig. 8 bearing surface is shown in Fig. 10.
- the bearing arrangement has been loaded with 13.91 N, and provides an axial bearing stiffness of 4810 kN/m and a bearing rocking stiffness of 15.37 Nm rad, an increase over both the Fig. 2 and Fig. 6 configurations.
- first and second legs 136, 138 of the continuous lands 122 each have leading edges 144, 146 and trailing edges 148, 150.
- the trailing edges 148, 150 form a smooth curve.
- the smooth curve is a circular arc 152 having a radius of approximately 50 ⁇ m. It can also be seen that where the leading edge 146 of a second leg 138 meets the trailing edge 150 of an adjacent second leg at the inner radius 124, a smooth curve is also formed.
- the smooth curve is a circular arc 154 having a radius of approximately 25 ⁇ m.
- the improvement in ease of manufacturability of the bearing surface 120 can best be appreciated by considering a punch used to form the bearing surface 120. Such a punch or die will be the inverse of the illustrated bearing surface 120. In other words, the punch will have raised surfaces corresponding to the continuous grooves 128, and grooves corresponding to the lands 122, 134. Viewing Fig. 9 from this perspective, it can be seen that the raised surfaces of the punch are unbroken between the inner radius 124 and the outer radius 126.
- the raised surfaces of the punch are also seen to be more uniformly broad between the outer radius 126 and the inner radius 124. Narrow areas on the raised surfaces of the punch, which would be subjected to undesirably high stresses as described above, are substantially illuminated by providing the smooth curves 152, 154.
- Hydrodynamic bearing performance is also dependent on the groove angle ( ⁇ ).
- Groove angle is defined as the angle between the tangent to the groove and the tangent to the circle at that point. Usually, the groove angle is kept constant for the inner grooves 130 and the outer grooves 132.
- the pumping action of the hydrodynamic bearing on the bearing fluid depends greatly on the groove angle, which in turn affects bearing performance.
- the groove angle may vary from approximately 19° to approximately 29° depending on the particular bearing characteristics required, but is preferably approximately 23.5°. The relationship between groove angle and bearing performance is illustrated in Fig. 11.
- the groove ratio is another parameter which affects the pumping action of the hydrodynamic bearing on the bearing fluid, and hence bearing performance.
- Groove ratio is defined as the ratio of the width of the groove to the width of the land, and may also be varied in a grooved hydrodynamic bearing according to the invention, from approximately 0.32 to approximately 0.6.
- the groove ratio is preferably approximately 0.5.
- the relationship between groove ratio and bearing performance is illustrated in Fig. 12.
- the depth of the grooves 128 in the Fig. 9 bearing surface may also vary between approximately 9 ⁇ m and approximately 13 ⁇ m and is preferably 1 1 ⁇ m.
- the relationship between groove depth and bearing performance is illustrated in Fig. 13.
- Another parameter which affects bearing performance is the location of the center radius 140.
- the inner and outer grooves 130, 132 Because of the way the inner and outer grooves 130, 132 are arranged, they pump bearing fluid towards each other, i.e. towards the center radius 140.
- the location of the center radius determines the relative lengths of the of the inner and outer grooves 130, 132 and hence their relative pumping capacities. Bearing performance depends on the location of the center radius as shown in Fig. 14.
- ⁇ P difference in pressure
- Fig. 15 shows a comparison of the pressures generated in the bearing fluid by the hydrodynamic bearing surfaces illustrated in Fig. 2 (eight undivided grooves), Fig. 6 (twelve undivided grooves) and Fig. 8 (eight divided grooves).
- the hydrodynamic thrust bearing of the invention has an improved minimum pressure over the Fig. 2 embodiment and the highest peak pressure of the three bearing surfaces, while the overall pressure distribution has also improved.
- the hydrodynamic bearing surface of the invention not only provides an improvement in performance over the illustrated prior art bearing arrangements, but is also easier to manufacture. It will be appreciated that the invention is not limited to the embodiment of the invention described above, and many modifications are possible without departing from the spirit and the scope of the invention. For example, additional intermediate lands 134 may be provided between adjacent continuous lands 122 to divide continuous groove 128 further.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Sliding-Contact Bearings (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9810766A GB2323133B (en) | 1996-01-08 | 1996-10-08 | Grooved hydrodynamic thrust bearing |
DE19681719T DE19681719T1 (en) | 1996-01-08 | 1996-10-08 | Grooved hydrodynamic thrust bearing |
JP52517697A JP3461357B2 (en) | 1996-01-08 | 1996-10-08 | Grooved hydrodynamic thrust bearings |
US08/750,486 US5795074A (en) | 1996-10-08 | 1996-10-08 | Grooved hydrodynamic thrust bearing |
KR1019980704890A KR100343273B1 (en) | 1996-01-08 | 1996-10-08 | Grooved hydrodynamic thrust bearings and grooved hydrodynamic thrust bearing mechanisms |
HK99100790A HK1015857A1 (en) | 1996-01-08 | 1999-02-26 | Grooved hydrodynamic thrust bearing |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US976496P | 1996-01-08 | 1996-01-08 | |
US60/009,764 | 1996-01-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1997025543A1 true WO1997025543A1 (en) | 1997-07-17 |
Family
ID=21739570
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1996/016155 WO1997025543A1 (en) | 1996-01-08 | 1996-10-08 | Grooved hydrodynamic thrust bearing |
Country Status (7)
Country | Link |
---|---|
JP (1) | JP3461357B2 (en) |
KR (1) | KR100343273B1 (en) |
CN (1) | CN1083070C (en) |
DE (1) | DE19681719T1 (en) |
GB (1) | GB2323133B (en) |
HK (1) | HK1015857A1 (en) |
WO (1) | WO1997025543A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002519204A (en) * | 1998-06-30 | 2002-07-02 | シーゲイト テクノロジー エルエルシー | Machining process of fluid bearing |
WO2012036684A1 (en) * | 2010-09-16 | 2012-03-22 | Stein Seal Company | Intershaft seal system for minimizing pressure induced twist |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100357620C (en) * | 2004-08-14 | 2007-12-26 | 鸿富锦精密工业(深圳)有限公司 | Hydrodynamic bearing |
US9777597B1 (en) * | 2016-03-30 | 2017-10-03 | Borgwarner Inc. | Turbocharger bearing fluid film surface and method |
CN110594288B (en) * | 2019-09-29 | 2024-03-08 | 中国矿业大学 | Magnetic control flexible tile thrust sliding bearing based on nano magnetic liquid |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2201732A5 (en) * | 1972-09-29 | 1974-04-26 | Philips Nv | |
FR2201514A1 (en) * | 1972-09-29 | 1974-04-26 | Philips Nv | |
US5433529A (en) * | 1994-08-02 | 1995-07-18 | Synektron Corporation | Fluid bearing construction employing thrust plate with pressure compensation ports |
-
1996
- 1996-10-08 CN CN96199566A patent/CN1083070C/en not_active Expired - Fee Related
- 1996-10-08 WO PCT/US1996/016155 patent/WO1997025543A1/en active IP Right Grant
- 1996-10-08 JP JP52517697A patent/JP3461357B2/en not_active Expired - Fee Related
- 1996-10-08 KR KR1019980704890A patent/KR100343273B1/en not_active IP Right Cessation
- 1996-10-08 GB GB9810766A patent/GB2323133B/en not_active Expired - Fee Related
- 1996-10-08 DE DE19681719T patent/DE19681719T1/en not_active Withdrawn
-
1999
- 1999-02-26 HK HK99100790A patent/HK1015857A1/en not_active IP Right Cessation
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2201732A5 (en) * | 1972-09-29 | 1974-04-26 | Philips Nv | |
FR2201514A1 (en) * | 1972-09-29 | 1974-04-26 | Philips Nv | |
US5433529A (en) * | 1994-08-02 | 1995-07-18 | Synektron Corporation | Fluid bearing construction employing thrust plate with pressure compensation ports |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002519204A (en) * | 1998-06-30 | 2002-07-02 | シーゲイト テクノロジー エルエルシー | Machining process of fluid bearing |
WO2012036684A1 (en) * | 2010-09-16 | 2012-03-22 | Stein Seal Company | Intershaft seal system for minimizing pressure induced twist |
US8408555B2 (en) | 2010-09-16 | 2013-04-02 | Stein Seal Company | Intershaft seal system for minimizing pressure induced twist |
Also Published As
Publication number | Publication date |
---|---|
KR100343273B1 (en) | 2002-10-25 |
CN1083070C (en) | 2002-04-17 |
GB2323133B (en) | 1999-11-03 |
GB2323133A (en) | 1998-09-16 |
HK1015857A1 (en) | 1999-10-22 |
CN1207797A (en) | 1999-02-10 |
DE19681719T1 (en) | 1999-04-01 |
JP3461357B2 (en) | 2003-10-27 |
JP2000503101A (en) | 2000-03-14 |
KR19990076767A (en) | 1999-10-15 |
GB9810766D0 (en) | 1998-07-15 |
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