WO2004010431A1 - Unite d'ecriture de servocommande de guidage avec palier a helium - Google Patents

Unite d'ecriture de servocommande de guidage avec palier a helium Download PDF

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Publication number
WO2004010431A1
WO2004010431A1 PCT/US2003/023036 US0323036W WO2004010431A1 WO 2004010431 A1 WO2004010431 A1 WO 2004010431A1 US 0323036 W US0323036 W US 0323036W WO 2004010431 A1 WO2004010431 A1 WO 2004010431A1
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WO
WIPO (PCT)
Prior art keywords
bearing
disc
actuator
servo
helium
Prior art date
Application number
PCT/US2003/023036
Other languages
English (en)
Inventor
Mark A. Toffle
Xu Zuo
Brent M. Weichelt
Louis J. Fioravanti
Original Assignee
Seagate Technology Llc
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 Seagate Technology Llc filed Critical Seagate Technology Llc
Publication of WO2004010431A1 publication Critical patent/WO2004010431A1/fr

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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
    • F16C32/00—Bearings not otherwise provided for
    • F16C32/06—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
    • F16C32/0629—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a liquid cushion, e.g. oil cushion
    • F16C32/064—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a liquid cushion, e.g. oil cushion the liquid being supplied under 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
    • F16C32/00—Bearings not otherwise provided for
    • F16C32/06—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
    • F16C32/0681—Construction or mounting aspects of hydrostatic bearings, for exclusively rotary movement, related to the direction of load
    • F16C32/0696—Construction or mounting aspects of hydrostatic bearings, for exclusively rotary movement, related to the direction of load for both radial and axial load
    • G—PHYSICS
    • G11—INFORMATION STORAGE
    • G11B—INFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B19/00—Driving, starting, stopping record carriers not specifically of filamentary or web form, or of supports therefor; Control thereof; Control of operating function ; Driving both disc and head
    • G11B19/20—Driving; Starting; Stopping; Control thereof
    • G11B19/2009—Turntables, hubs and motors for disk drives; Mounting of motors in the drive
    • G—PHYSICS
    • G11—INFORMATION STORAGE
    • G11B—INFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B5/00—Recording by magnetisation or demagnetisation of a record carrier; Reproducing by magnetic means; Record carriers therefor
    • G11B5/48—Disposition or mounting of heads or head supports relative to record carriers ; arrangements of heads, e.g. for scanning the record carrier to increase the relative speed
    • G11B5/58—Disposition or mounting of heads or head supports relative to record carriers ; arrangements of heads, e.g. for scanning the record carrier to increase the relative speed with provision for moving the head for the purpose of maintaining alignment of the head relative to the record carrier during transducing operation, e.g. to compensate for surface irregularities of the latter or for track following
    • G11B5/596—Disposition or mounting of heads or head supports relative to record carriers ; arrangements of heads, e.g. for scanning the record carrier to increase the relative speed with provision for moving the head for the purpose of maintaining alignment of the head relative to the record carrier during transducing operation, e.g. to compensate for surface irregularities of the latter or for track following for track following on disks
    • G11B5/59633—Servo formatting
    • 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
    • F16C2370/00—Apparatus relating to physics, e.g. instruments
    • F16C2370/12—Hard disk drives or the like

Definitions

  • This application relates generally to data storage systems, such as magnetic disc drives, and more particularly to a method and apparatus for recording servo patterns on information storage discs.
  • Disc drives are data storage devices that store digital data in magnetic form on a rotating disc.
  • Modern disc drives comprise one or more rigid information storage discs that are coated with a magnetizable medium and mounted on the hub of a spindle motor for rotation at a constant, high speed.
  • Information is stored on the discs in a plurality of concentric, circular tracks typically by an array of transducers (known as "heads"), which are mounted to a radial actuator for movement of the heads relative to the discs.
  • heads transducers
  • sequential data is written onto a selected one of the disc tracks.
  • the head senses the data previously written onto the disc track and transfers the information to an external environment.
  • Head positioning within a desired track is dependent on head- positioning servo patterns, i.e., magnetic patterns recorded onto the disc surface and used to maintain optimum track spacing and sector timing.
  • Servo patterns or servo information can be located between the data sectors on each track of a disc (known as “embedded servo” information), or on only one surface of one of the discs within the disc drive (known as “dedicated servo” information). Regardless of whether a manufacturer uses "embedded” or “dedicated” servo information, the servo patterns are typically recorded on the disc or discs during the manufacturing process of the disc drive.
  • Servo patterns are typically recorded on the magnetizable medium of the disc by a servo-track writer ("STW") assembly during the manufacture of the disc drive.
  • STW servo-track writer
  • One conventional servo track writer assembly records servo patterns on the discs following installation of the discs into the disc drive.
  • the servo track writer assembly attaches directly to a disc drive having a disc pack, where the mounted discs on the disc pack have not been prerecorded with servo patterns.
  • the servo track writer essentially uses the drive's own read/ write heads to record the requisite servo patterns directly to the mounted discs.
  • An alternative method for servo pattern recording utilizes a separate apparatus having dedicated servo-recording transducers or heads for recording the servo patterns onto one or more of the discs prior to the discs being assembled into the disc drive.
  • the dedicated servo recording heads can be used to record servo patterns to a number of discs simultaneously, which are subsequently loaded into the disc drive for use.
  • the servo track writer assembly includes a spindle assembly, an actuator assembly and a servo recording head.
  • the spindle assembly has a hub, which supports the disc, and a spindle motor for rotating the hub.
  • the actuator assembly has an actuator arm supported by an actuator bearing for positioning the actuator arm relative to the disc.
  • At least one of the spindle motor and the actuator bearing has a gas- lubricated bearing with a working fluid, which includes helium.
  • the servo recording head is supported by the actuator arm relative to the disc to record the servo pattern information on the disc as the spindle motor rotates the disc and the actuator bearing positions the actuator arm.
  • Another embodiment of the present invention is directed to a method for recording servo pattern information on a disc.
  • the method includes: (a) positioning the disc on a hub of a spindle motor; (b) activating the spindle motor to rotate the disc; (c) positioning a servo recording head relative to a desired radial position on the disc with an actuator having an actuator bearing; (d) signaling the servo recording head to record servo pattern information on the disc; and (e) maintaining separation of opposing bearing surfaces with a working fluid in a gas-lubricated bearing within at least one of the spindle motor and the actuator bearing during (d), wherein the working fluid comprises helium.
  • the data storage system includes a data storage disc, a spindle assembly, an actuator assembly and a head.
  • the spindle assembly has a hub, which supports the data storage disc, and a spindle motor for rotating the hub.
  • the ictuator assembly has an actuator arm supported by an actuator bearing for positioning the actuator arm relative to the data storage disc.
  • At least one of the spindle motor and the actuator bearing has a gas-lubricated bearing with a vorking fluid, which includes helium.
  • the head is supported by the actuator arm relative to the data storage disc.
  • FIG. 1 is a top plan view of a disc drive assembly manufactured using an smbodiment of the present invention.
  • FIG. 2 is a top view of a servo-track writer illustrating an actuator assembly and a spindle motor rotatably supporting a plurality of discs in accordance with an embodiment of the present invention.
  • FIG. 3 is a perspective view of the servo-track writer shown in FIG. 2, which illustrates the actuator assembly and the spindle motor in a disc load/ unload position.
  • FIG. 4 is a perspective view of the actuator assembly of FIG. 2 engaging the plurality of discs on a spindle motor hub assembly, wherein the spindle motor has been removed for purposes of clarity.
  • FIGS. 5-7 are graphs illustrating power spectral density of PES signals, AC squeeze and DC squeeze, respectively, as measured at an outermost servo track while using air as the lubricating fluid in the spindle bearing and in the actuator bearing during servo writing.
  • FIGS. 8-10 are graphs illustrating power spectral density of PES signals, AC squeeze and DC squeeze, respectively, as measured at an innermost servo track while using air as the lubricating fluid in the spindle bearing and in the actuator bearing during servo writing.
  • FIGS. 11-13 are graphs illustrating power spectral density of PES signals, AC squeeze and DC squeeze, respectively, as measured at an outermost servo track while using helium as the lubricating fluid in the spindle bearing and in the actuator bearing during servo writing.
  • FIGS. 14-16 are graphs illustrating power spectral density of PES signals, AC squeeze and DC squeeze, respectively, as measured at an innermost servo track while using helium as the lubricating fluid in the spindle bearing and in the actuator bearing during servo writing.
  • FIG. 17 is a graph illustrating the effect of helium concentration on disc mode vibrations in a gas-lubricated spindle bearing.
  • FIG. 18 is a block diagram illustrating a system for pumping helium into bhe spindle bearing and actuator bearing of the servo track writer assembly shown in FIGS. 2-4, according to one embodiment of the present invention.
  • FIG. 19 is a perspective view of bearing portion of a helium gas-lubricated actuator motor, which can be used in the servo track writer assembly shown in FIGS. 2-4 according to one embodiment of the present invention.
  • FIG. 20 is a cross-sectional view of the actuator bearing shown in FIG. 19, taken along lines 20—20.
  • FIG. 21 is a cross-sectional view of a helium gas-lubricated spindle motor, which can be used in the servo track writer assembly shown in FIGS. 2-4 according to one embodiment of the present invention.
  • FIG. 22 is a flow diagram showing the steps for writing servo patterns on discs in accordance with one embodiment of the present invention.
  • FIG. 23 is a flow diagram showing the steps for writing servo patterns on discs in accordance with another embodiment of the present invention.
  • FIG. 1 A disc drive 100 manufactured in accordance with an embodiment of the present invention is shown in FIG. 1.
  • the disc drive 100 includes a base 102 to which various components of the disc drive are mounted.
  • a top cover 104 shown partially cut away, cooperates with the base 102 to form an internal, sealed environment for the disc drive 100 in a conventional manner.
  • the components include a spindle motor 106, which rotates one or more discs 108 at a constant high speed. Information is written to and read from tracks, as illustrated by broken line 109, on the discs 108 through the use of an actuator assembly 110, which rotates about a bearing shaft assembly 112 positioned adjacent the discs 108.
  • the actuator assembly 110 includes a plurality of actuator arms 114 which extend towards the discs 108, with one or more flexures 116 extending from each of the actuator arms 114.
  • a head 118 mounted at the distal end of the flexures 116 is a head 118, which includes an air bearing slider (not shown) enabling the head 118 to fly in close proximity above (or in light contact with) the corresponding surface of the associated disc 108.
  • Radial positioning of the heads 118 is controlled through the use of a voice coil motor 120, which typically includes a coil 122 attached to the actuator assembly 110, as well as one or more permanent magnets 124, which establish a magnetic field in which the coil 122 is immersed.
  • the controlled application of current to the coil 122 causes a magnetic interaction between the permanent magnets 124 and the coil 122 so that the coil 122 moves in accordance with the well-known Lorentz relationship.
  • the actuator assembly 110 pivots about the bearing shaft assembly 112 and the heads 118 are caused to move across the surfaces of the discs 108.
  • Servo patterns provide information that specifies the radial positions of the heads.
  • the heads 118 sense the servo patterns, and the resulting servo information is used to generate a position error signal (PES), which represents the distance from which the heads 118 are positioned relative to a desired position.
  • PES position error signal
  • Dedicated servo patterns are recorded on a dedicated servo disc or disc surface that is used exclusively for servo information.
  • Embedded servo patterns are embedded at regular intervals within normal data tracks. As will be clear from the discussion that follows, either type of servo patterns can be recorded onto a target disc using the methods and apparatus of the present invention.
  • servo track writer assemblies can either be stand-alone devices that record the servo patterns onto the disc surfaces before the discs are installed into a disc drive or devices that record the servo patterns through the disc drive's own read/ write heads, after the discs have been installed into the disc drive.
  • FIGS. 2-4 illustrate a dedicated servo track writer assembly 200 in accordance with one embodiment of the present invention.
  • servo track writer assembly 200 includes an actuator assembly 202 for positioning one or more servo recording heads 204 (shown in FIG.
  • a spindle motor hub assembly 206 for supporting and rotating the discs 108; a vacuum chuck 208 for rigidly securing the actuator assembly 202 in a desired position for servo track writing; and a laser interferometer 210 for measuring the angular displacement and consequent positioning of the servo-recording heads 204 of the actuator assembly 202 during servo pattern recording.
  • Servo track writer assembly 200 sits upon a substantially immobile and horizontally positioned platform or base 212.
  • the platform 212 is substantially resistant to movements from impact-type collisions and is preferably a granite slab or other like material having sufficient size to support all the components of the servo track writer assembly 200.
  • Actuator assembly 202 is connected to the platform 212 via a slide mechanism 214 for lateral movement (as indicated by arrow 216) over platform 212 between a servo recording position 218 and a disc loading and unloading position 220, as is discussed in greater detail below.
  • Spindle motor hub assembly 206 and vacuum chuck 208 are directly and non- moveably secured to platform 212.
  • actuator assembly 202 and spindle hub assembly 206 are both vertically oriented. That is, the plurality of discs 108, when secured to spindle hub assembly 206, are vertically positioned relative to platform 212.
  • actuator assembly 202 includes an E-block 222 (shown in FIG. 3) having a plurality of actuator arms 224 (FIG. 4) that are also arranged for movement in substantially vertical planes relative to the platform 212.
  • Each actuator arm 224 includes one or more flexures 226 connecting a distal end of the actuator arm to a corresponding one of the servo-writing heads 204.
  • the actuator assembly and spindle hub assembly can have other orientations, such as horizontal, in alternative embodiments of the present invention.
  • FIG. 3 illustrates servo track writer assembly 200 in the load/ unload position 220, where actuator assembly 202 has been moved away from the spindle hub assembly 206 via the slide mechanism 214. In this position, a stack of discs 108 can be loaded onto spindle hub assembly 206 to start the servo writing process.
  • spindle hub assembly 206 includes a detachable spindle hub 228 (shown in FIG. 4), which allows hub 228 and the stack of discs 108 to be detached from spindle motor hub assembly 206, thereby easing the process of loading and unloading discs 108 from spindle hub 228.
  • discs 108 are secured to spindle hub assembly 206 by means of a clamp ring 230 (shown in FIG. 3).
  • Actuator assembly 202 is then moved laterally along platform 212 (in the direction of arrow 216) toward the spindle hub assembly 206 to load servo heads 204 onto the disc surfaces.
  • a comb 232 (shown in FIG. 4) can be used to maintain a separation between heads 204 so that actuator assembly 202 and the disc stack 108 can merge without unintentional contact between heads 204 and the discs 108.
  • Comb 232 preferably moves together with actuator assembly 202 as shown in FIG.4 and acts to separate heads 204 against the bias force of the flexures 226.
  • actuator assembly 202 is locked into the servo writing position 218 so that the heads 204 are positioned within the gaps between the adjacent discs 108
  • comb 232 is rotated away from E-block 222 to allow the heads 204 to engage their respective discs as a result of the bias force provided by the flexures 226.
  • spindle hub assembly 206 is activated to spin the discs 108 at a predetermined rate prior to disengaging the comb 232 to prevent the heads from contacting the disc surfaces.
  • the rotational motion of discs 108 generates wind so that the heads 204 ride an air bearing in lieu of actually contacting the disc surface.
  • This air bearing counters the bias force applied by the flexures 226 and protects the fragile magnetic coatings on the disc surfaces.
  • E-block 222 is rotated about a horizontal axis by an actuator motor and bearing assembly within the actuator assembly 202 so that the heads 204 move radially across the surface of their respective discs 108.
  • the position of heads 204 is determined by the laser interferometer 210, which utilizes interferometric techniques to track movement of the heads along the disc radius, and interferometer 210 sends position signals back to control the operation of actuator assembly 202 and thus the radial position of heads 204.
  • the E-block 222 Upon completion of the servo writing process, the E-block 222 is rotated outwardly to position heads 204 adjacent an outer diameter of the discs 108, while comb 232 is rotated into contact with flexures 226 to disengage heads 204 from discs 108.
  • the actuator assembly 202 is then moved laterally away from the spindle hub assembly 206 to the load/ unload position 220 so that the discs 108 (complete with their newly written servo patterns) can be removed from the spindle hub assembly 206 and ultimately installed in the disc drive 100.
  • FIGS. 5-10 are graphs illustrating the power spectral density, AC squeeze and DC squeeze as measured at the outermost servo track (servo track 1900) on the surfaces of discs 108 using air in the spindle bearing and in the actuator bearing.
  • FIG. 5 is a graph, which illustrates the power spectral density of the FFT spectra as a function of frequency when heads 204 (FIG. 4) were positioned at the outermost servo track.
  • the FFT spectra were obtained from PES signals that were demodulated from read signals generated by individual heads 204.
  • Each line in FIG. 5 represents the power spectral density from one of the read heads.
  • frequency range 300 from about 600 Hz to about 900 Hz
  • the power spectral density of each PES signal showed a low-level asynchronous vibration, which is generally known as a mechanical "busy signal". This busy signal represents inaccuracy in the positions of the servo patterns that were written on the surfaces of discs 108.
  • FIG. 6 is a bar chart illustrating AC squeeze in microinches at the outermost servo tracks for the plurality of the individual heads.
  • the AC squeeze is relatively large (from about 0.18 uin. to about 0.28 uin.) due to the busy signals shown in FIG. 5.
  • FIG. 7 is a bar chart illustrating DC squeeze in microinches at the outermost servo tracks for the plurality of the individual heads. Again, the DC squeeze is relatively large (from about 0.05 uin. to almost 0.15 uin.)
  • FIGS. 8-10 illustrate the power spectral density, AC squeeze and DC squeeze, respectively, when heads 204 were positioned at the innermost servo track and air was again used as the lubricating in the spindle bearing and in the actuator bearing. Similar to the results shown in FIGS. 5-7, the power spectral density includes a large busy signal in the low frequency ranges, and the AC and DC squeeze are relatively high and in about the same range as at the outermost servo track. b. Helium as Lubricating Fluid
  • FIGS. 11-13 illustrate the resulting power spectral density, AC squeeze and DC squeeze, respectively, at the outermost servo track
  • FIGS. 14-16 illustrate the resulting power spectral density, AC squeeze and DC squeeze, respectively, at the innermost servo track.
  • FIGS. 11-16 show that the power spectral density in the 600 Hz to 900 Hz frequency range is much lower with the use of helium as a lubricating fluid. Also, the AC squeeze was reduced by about 30% to 45%, and the DC squeeze was reduced by about 20% to 30%. Therefore, by using helium as the lubricating fluid or the spindle and actuator bearings during servo track writing, low-level isynchronous vibrations can be reduced, which allows the servo tracks to be vritten onto the disc surfaces more accurately.
  • Helium can therefore be used as the lubricating fluid in the spindle and Lctuator bearings of a dedicated servo track writer assembly such as that shown in TGS. 2-4 or in the spindle and actuator bearings of the disc drive with in-situ lervo track writing assemblies. If desired, the helium can then be pumped out of he bearings and replaced with a different gas, such as air, once the servo track vriting process has been completed.
  • a different gas such as air
  • Helium can be used in a variety of concentrations.
  • the orking fluid comprises helium at a concentration of at least 70% by volume.
  • the working fluid comprises helium at a concentration of ibout 99% by volume.
  • FIG.17 is a graph illustrating the effect of helium :oncentration on disc mode vibrations in a gas-lubricated spindle bearing. The ?rror motions of the disc were measured with an LDV pointing at a 65 mm iiameter x .025 thick glass disk spinning at 7200 RPM and 0 RPM (for :omparison).
  • the graph shows the disk mode peak amplitudes in millivolts mV) at 120, 1.1, 1.082, 1.12, and 1.202 KHz.
  • the amplitudes at some frequencies, such as 1.202 KHz in this example, increases as the percentage of helium is reduced. Above a concentration of about 70%, the amplitudes are relatively :onstant.
  • FIG. 18 is a block diagram illustrating a system for pumping helium into the spindle bearing and actuator bearing of servo track writer assembly 200 (shown in FIGS. 2-4), according to one embodiment of the present invention.
  • a gas lubricant source tank 500 is coupled to the gas bearing in spindle motor assembly 206 through a pressure regulator 502 and conduits 503 and 504.
  • Source tank 500 is also coupled to the gas bearing in actuator assembly 202 through a pressure regulator 505 and conduits 503 and 506.
  • source tank 500 includes helium having a concentration of 99% by volume. However, other concentrations can also be used in alternative embodiments of the present invention.
  • a recovery tank 510 can be used to recover helium from the bearings in assemblies 202 and 206 through conduits 512 and 514, respectively. This allows the helium to be recycled for subsequent servo track writing operations.
  • FIGS. 19 and 20 illustrate an example of a bearing portion of a helium gas- lubricated actuator motor 600, which can be used in actuator assembly 202 (shown in FIGS. 2-4) in one embodiment of the present invention.
  • FIG. 19 is a perspective view of bearing portion 600.
  • Bearing portion 600 includes a stator 602 and a rotor 604.
  • Rotor 604 rotates within stator 602 about axis of rotation 606.
  • Stator 602 has a gas inlet 608 and an exhaust port 610 through which helium gas can be supplied to and retrieved from the gas bearing within bearing portion 600.
  • FIG. 20 is a cross-sectional view of bearing portion 600 shown in FIG. 19, taken along lines 20—20.
  • Stator 602 has an annular shape, with a central cavity 612.
  • Rotor 604 includes a pair of opposing disc-shaped thrust flanges 614 and 616, which are coupled together through a cylindrical sleeve 618 extending through central cavity 612.
  • Flanges 614 and 616 are coupled to sleeve 618 with bolts (not shown), which are inserted through bores 619, for example.
  • Flanges 614 and 616 and sleeve 618 rotate about axis 606.
  • the mating surfaces between stator 602 and the elements of rotor 604 form radial bearing surfaces 620 and axial bearing surfaces 622 and 624. These bearing surfaces are separated from one another by a small gap. During operation, the gap is maintained by the lubricating gas.
  • Inlet 608 is coupled to conduit 506 (shown in FIG. 19) for receiving helium gas at a desired pressure from source tank 500.
  • the helium gas passes from inlet 608 into passageway 625 and then along bearing surfaces 620, 622 and 624, as indicated by arrows 626. Some of the helium gas can then be collected through exhaust port 610 (shown in FIG. 19), which is coupled to the bearing surfaces through the passageway similar to passageway 625.
  • Stator 602 further includes a passageway 626, which is capped with a plug 628.
  • the gas lubricated bearing shown in FIG. 19 and 20 is provided as an example only. Any other gas lubricated bearing design can be used in alternative embodiments of the present invention.
  • FIG. 21 is a cross-sectional view of a helium gas lubricated spindle motor 700 according to one embodiment of the present invention.
  • Spindle motor 700 can be used within spindle motor hub assembly 206 (shown in FIGS. 2-4) for driving spindle hub 228 and the plurality of discs 108 with reduced asynchronous vibrations during the servo track writing process.
  • Spindle motor 700 includes a 3tator 702 and a rotor 704.
  • Rotor 704 rotates within stator 702 about axis of rotation 706.
  • Rotor 704 has a receiver 708 for receiving spindle hub 228.
  • a ball Latch mechanism 710 locks hub 228 within receiver 708.
  • Rotor 704 has a main body portion 712 and a thrust flange 714, which rotate about axis 706.
  • the outer surfaces of rotor 704 and the opposing surfaces of stator 702 are spaced from one another by a small gap, which forms a gas- lubricated bearing having radial bearing surfaces 720 and 722 and axial bearing surfaces 724 and 726.
  • Rotor 704 carries one or more magnets 730, which are driven by a rotating magnetic field supplied by a stator winding 732 and a stator core 734. Winding 732 and core 734 are carried by stator 702. As is well-known in the art, commutation pulses supplied to winding 732 generate a rotating magnetic field along core 734, which drives magnets 730 and thus rotor 704.
  • Spindle motor 700 further includes a gas inlet 740 for receiving helium gas from conduit 504 (shown in FIG. 18).
  • Inlet 740 is coupled to the gaps between bearing surfaces 720, 722, 724 and 726 through an inlet passageway 742.
  • Spindle motor 700 further includes exhaust pick-up passageways 744, which recover helium gas from the gaps.
  • Exhaust passageways 744 direct the pressurized gas from the bearing gaps through winding cavity 746 and out exhaust port 748.
  • Exhaust port 748 can be coupled to conduit 512 (shown in FIG. 18) for recovering the helium gas.
  • the spindle motor and actuator motor are configured with hydrostatic gas-lubricated bearings, which use an external pressurized fluid source to maintain bearing surface separation.
  • either or both of the spindle motor and the actuator motor can be configured as a hydrodynamic bearing, which generates a self- pumping pressure internal to the bearing in order to maintain the bearing surface separation.
  • Other configurations can also be used.
  • the desired gas pressure within the gas-lubricated bearings is a function of the individual bearing design and its application.
  • FIG. 22 is a flow chart illustrating a process 800 of writing servo information on a data storage disc according to one embodiment of the present invention.
  • the disc is positioned on a hub of a spindle motor of a dedicated servo track writing assembly, prior to installation into a disc drive.
  • the servo track writer assembly activates the spindle motor to rotate the disc.
  • the servo track writing assembly positions a servo recording head relative to a desired radial position on the disc with an actuator.
  • the actuator has an actuator motor.
  • the servo track writing assembly then signals the servo recording head to record the servo pattern information on the disc, at step 804.
  • the servo track writing assembly maintains separation of opposing bearing surfaces with a working fluid in a gas-lubricated bearing within one or both of the spindle motor and the actuator motor, at step 805, wherein the working fluid includes helium.
  • the servo track writing assembly recovers the helium from the gap through an exhaust port in the gas- lubricated bearing.
  • the disc, with its newly written servo pattern information is installed within a disc drive.
  • FIG. 23 is a flow chart illustrating a process 900 of writing servo information on a data storage disc according to an alternative embodiment of the present invention.
  • the disc is installed on a hub of a spindle motor and assembled into a disc drive. If the spindle motor has a gas-lubricated bearing, then helium is pumped into the spindle motor bearing at step 902.
  • the spindle motor is activated to rotate the disc.
  • a servo recording head is positioned relative to a desired radial position on the disc with an actuator.
  • the actuator can be an actuator installed in the disc drive or a separate actuator of a servo track writing assembly onto which the disc drive is mounted.
  • the actuator that is used to position the servo recording head has a gas-lubricated bearing, which also uses helium gas as a lubricating fluid.
  • the servo track writing assembly (or the product disc drive) then signals the servo recording head to record the servo pattern information on the disc, at step 905.
  • the helium maintains separation of opposing bearing surfaces in the gas-lubricated bearings within one or both of the spindle motor and the actuator motor, at step 906.
  • the helium is recovered from an exhaust port in the gas-lubricated bearings.
  • helium gas can be used in various concentrations as the working fluid in a gas-lubricated spindle motor and/ or actuator motor during the writing of servo patterns to the disc surfaces or during normal operation of a data storage system having any type of storage media.
  • the spindle and actuator motors can have any suitable physical configuration.
  • helium gas can be used in other gas-lubricated bearing applications, such as precision grinders, cutting tools, gyroscopes and mirror polishing equipment, for reducing asynchronous vibrations. Other applications also exist.

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  • Moving Of The Head To Find And Align With The Track (AREA)

Abstract

L'invention concerne un assemblage d'unité d'écriture de servocommande de guidage (200) et un procédé (800, 900) destinés à enregistrer une information de schéma d'asservissement sur un disque (108). L'assemblage d'unité d'écriture de servocommande de guidage comprend un assemblage d'axe (206), un assemblage d'actionneur (202) et une tête d'enregistrement asservie (204). L'assemblage d'axe comporte un moyeu (228), supportant le disque et un moteur d'axe (700) servant à faire tourner le moyeu. L'assemblage d'actionneur comprend un bras supporté par un palier d'actionneur (600) permettant de positionner le bras par rapport au disque. Le moteur à axe et le palier d'actionneur, ou au moins l'un des deux, comprend un palier à lubrifiant gazeux contenant de l'hélium. La tête d'enregistrement asservie, supportée par le bras de l'actionneur, permet d'enregistrer l'information de schéma d'asservissement sur le disque alors que le moteur à axe tourne et que le palier d'actionneur positionne le bras.
PCT/US2003/023036 2002-07-23 2003-07-23 Unite d'ecriture de servocommande de guidage avec palier a helium WO2004010431A1 (fr)

Applications Claiming Priority (2)

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US39784902P 2002-07-23 2002-07-23
US60/397,849 2002-07-23

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WO2004010431A1 true WO2004010431A1 (fr) 2004-01-29

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7355811B1 (en) 2004-05-04 2008-04-08 Maxtor Corporation Hermetically sealed housing with interior capture plate
US7398590B1 (en) 2004-06-02 2008-07-15 Maxtor Corporation Applying mechanical shock to a data storage device with an enclosed low-density gas
US7570454B1 (en) 2004-05-04 2009-08-04 Maxtor Corporation Fill valve with a press-fit member for a sealed housing
US7914858B1 (en) 2004-05-04 2011-03-29 Maxtor Corporation Process to seal housing components to contain low density gas
US8059364B1 (en) 2004-05-04 2011-11-15 Maxtor Corporation Hermetically sealed connector interface
US9293169B2 (en) 2004-05-04 2016-03-22 Seagate Technology Llc Seal-type label to contain pressurized gas environment

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JPH01320312A (ja) * 1988-06-20 1989-12-26 Nippon Seiko Kk 軸受ユニット
JPH02102915A (ja) * 1988-10-11 1990-04-16 Tokyo Electric Co Ltd 動圧流体軸受装置
WO2000051112A2 (fr) * 1999-02-22 2000-08-31 Seagate Technology Llc Procede perfectionne d'ecriture de servo-informations, destine a des unites de disque dur
WO2001022410A1 (fr) * 1999-09-20 2001-03-29 Westwind Air Bearings Ltd. Fabrication de dispositifs de memorisation de donnees
JP2001146915A (ja) * 1999-11-19 2001-05-29 Nsk Ltd ディスク装置用流体軸受装置
US20020181160A1 (en) * 2001-06-01 2002-12-05 Buske Lon Richard Multi-disc servo track writer vibration isolation method and apparatus

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Publication number Priority date Publication date Assignee Title
JPH01320312A (ja) * 1988-06-20 1989-12-26 Nippon Seiko Kk 軸受ユニット
JPH02102915A (ja) * 1988-10-11 1990-04-16 Tokyo Electric Co Ltd 動圧流体軸受装置
WO2000051112A2 (fr) * 1999-02-22 2000-08-31 Seagate Technology Llc Procede perfectionne d'ecriture de servo-informations, destine a des unites de disque dur
WO2001022410A1 (fr) * 1999-09-20 2001-03-29 Westwind Air Bearings Ltd. Fabrication de dispositifs de memorisation de donnees
JP2001146915A (ja) * 1999-11-19 2001-05-29 Nsk Ltd ディスク装置用流体軸受装置
US20020181160A1 (en) * 2001-06-01 2002-12-05 Buske Lon Richard Multi-disc servo track writer vibration isolation method and apparatus

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Title
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PATENT ABSTRACTS OF JAPAN vol. 014, no. 311 (M - 0994) 4 July 1990 (1990-07-04) *
PATENT ABSTRACTS OF JAPAN vol. 2000, no. 22 9 March 2001 (2001-03-09) *

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7355811B1 (en) 2004-05-04 2008-04-08 Maxtor Corporation Hermetically sealed housing with interior capture plate
US7570454B1 (en) 2004-05-04 2009-08-04 Maxtor Corporation Fill valve with a press-fit member for a sealed housing
US7914858B1 (en) 2004-05-04 2011-03-29 Maxtor Corporation Process to seal housing components to contain low density gas
US8059364B1 (en) 2004-05-04 2011-11-15 Maxtor Corporation Hermetically sealed connector interface
US9293169B2 (en) 2004-05-04 2016-03-22 Seagate Technology Llc Seal-type label to contain pressurized gas environment
US7398590B1 (en) 2004-06-02 2008-07-15 Maxtor Corporation Applying mechanical shock to a data storage device with an enclosed low-density gas

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