CA2109249A1 - Magnetic disk drive unit - Google Patents

Magnetic disk drive unit

Info

Publication number
CA2109249A1
CA2109249A1 CA 2109249 CA2109249A CA2109249A1 CA 2109249 A1 CA2109249 A1 CA 2109249A1 CA 2109249 CA2109249 CA 2109249 CA 2109249 A CA2109249 A CA 2109249A CA 2109249 A1 CA2109249 A1 CA 2109249A1
Authority
CA
Canada
Prior art keywords
spindle shaft
disk drive
bearing
stator
drive assembly
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.)
Abandoned
Application number
CA 2109249
Other languages
French (fr)
Inventor
David W. Richard
Christopher E. Staehly
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raymond Engineering Inc
Original Assignee
Raymond Engineering Inc
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 Raymond Engineering Inc filed Critical Raymond Engineering Inc
Publication of CA2109249A1 publication Critical patent/CA2109249A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B33/00Constructional parts, details or accessories not provided for in the other groups of this subclass
    • G11B33/12Disposition of constructional parts in the apparatus, e.g. of power supply, of modules
    • G11B33/121Disposition of constructional parts in the apparatus, e.g. of power supply, of modules the apparatus comprising a single recording/reproducing device
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B19/00Driving, 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
    • G11B19/02Control of operating function, e.g. switching from recording to reproducing
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B19/00Driving, 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
    • G11B19/20Driving; Starting; Stopping; Control thereof
    • G11B19/2009Turntables, hubs and motors for disk drives; Mounting of motors in the drive
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B20/00Signal processing not specific to the method of recording or reproducing; Circuits therefor
    • G11B20/10Digital recording or reproducing
    • G11B20/18Error detection or correction; Testing, e.g. of drop-outs
    • G11B20/1816Testing
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B33/00Constructional parts, details or accessories not provided for in the other groups of this subclass
    • G11B33/02Cabinets; Cases; Stands; Disposition of apparatus therein or thereon
    • G11B33/08Insulation or absorption of undesired vibrations or sounds
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B5/00Recording by magnetisation or demagnetisation of a record carrier; Reproducing by magnetic means; Record carriers therefor
    • G11B5/48Disposition 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
    • G11B5/4806Disposition 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 specially adapted for disk drive assemblies, e.g. assembly prior to operation, hard or flexible disk drives
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B5/00Recording by magnetisation or demagnetisation of a record carrier; Reproducing by magnetic means; Record carriers therefor
    • G11B5/48Disposition 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
    • G11B5/58Disposition 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
    • G11B5/60Fluid-dynamic spacing of heads from record-carriers
    • G11B5/6005Specially adapted for spacing from a rotating disc using a fluid cushion

Abstract

MAGNETIC DISK DRIVE UNIT

Abstract of the Invention:
A high capacity, high speed memory system is presented. The system comprises a disk drive cartridge and an electronics unit. The disk drive cartridge comprises five magnetic hard disks having 300 megabytes of usable capacity housed in a hermetically sealed, self-contained unit suitable for use in extreme environments of vibration, shock and temperature. The electronics unit comprises a metal structure wherein the electronics for the system are housed. The disk drive cartridge has a stationary spindle to which a motor stator assembly is attached. A motor rotor assembly is constituted by a rotary hub mounted around the stator, the hub having a motor magnet mounted therein. Upper and lower bearing assemblies are positioned between the stator and the rotor. This assembly is preloaded by a pair of canted springs which are disposed about the spindle and bear against the floating race of the upper bearing assembly.
Preloading the assembly in this manner avoids abrupt contact between the bearing and the spindle shaft during vibrations. These abrupt contacts have been found to generate head position errors during vibration. These head position errors are outside the bandwidth of typical prior art closed loop servos.
However, due to the increased capacity of the present invention a higher bandwidth is utilized. Accordingly, the canted springs of the present invention prohibit the abrupt contacts, thereby eliminating the head errors that would otherwise result.

Description

~: -~ 2109~9 :

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MAGNETIC DISK DRIVE UNIT

~ Backaround of the Invention:
`l This invention relates to the field of magnetic disc memory units. More particularly, this invention relates to a ruggedized magnetic disc memory unit ~
~1 5 suitable for use in hostile or severe environments and - ~;
capable of withstanding loads or stresses, such as -~¦ shock, vibration, and temperature extremes and which is capable of operation at any attitude. The unit of the present invention is particularly suitable for use in military applications, but it may also find use in ~; ~ other demanding environments, such as, for e~ample, oil and gas well drilling and seismic exploration.
~ Both magnetic tape recorder units and magnetic ; disc memory units have been known in the art for many ~ -i~ 15 years. Tape units suitable for use in demanding -~, ~ applications are available, but a need exists for an ` ~ improved disc unit. Examples of such prior art disk units are disclosed in U.S. Patent Nos. 4,791,508;
4,870,703 and 4,965,686 all of which are assigned to ` 20 the assignee hereof and are expressly incorporated herein by reference.

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SummarY of the Invention:
The above-discussed and other problems and deficiencies of the prior art are overcome or ,j , ~. .
`~ alleviated by the high capacity, high speed memory system of the present invention. In accordance with ! the present invention the system comprises a disk drive cartridge and an electronics unit. The disk drive - -~
cartridge comprises five magnetic hard disks having 300 megabytes of usable capacity housed in a hermetically sealed, self-contained unit suitable for use in extreme environments of vibration, shock and temperature. The electronics unit comprises a metal structure wherein ~-the electronics for the system are housed.
The disk drive cartridge has a stationary spindle to which a motor stator assembly is attached. A motor rotor assembly is constituted by a rotary hub mounted around the stator, the hub having a motor magnet ~ mounted therein. Upper and lower bearing assemblies ; -i are positioned between the stator and the rotor. This assembly is preloaded by a pair of canted springs which are disposed about the spindle and bear against the `~ floating race of the upper bearing assembly.
Preloading the assembly in this manner avoids abrupt contact between the bearing and the spindle shaft during vibrations. These abrupt contacts have been ~ found to generate head position errors during `~ vibration. These head position errors are outside the bandwidth of typical prior art closed loop servos.
However, due to the increased capacity of the present -~
invention a higher bandwidth is utilized. Accordingly, ~! the canted springs of the present invention prohibit ~ the abrupt contacts, thereby eliminating the head ---~ errors that would otherwise result.

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2 ~ 9 _3_ The disk drive cartridge also includes a temperature sensor mounted on a circuit board of the ~ spindle assembly. The temperature sensor measures 1 internal temperature of the disk drive cartridge. This temperature information is used to modify a seek algorithm. More specifically, to modify drive current ; levels to the voice coil (since voice coil resistance changes with temperature), to modify head load/unload operation, to modify temperature drift for readings of Hall effect devices, and to better account for flex '~ bias of capton flex circuits.
The disk drive cartridge further includes a head -~
loading sensor assembly. A magnetic flux sensor is disposed on a circuit board which extends over a ~i 15 portion of an arm assembly. The arm assembly has a permanent magnet therein position to pass under the magnetic flux sensor (e.g., a Hall effect sensor).
Accordingly, as the arm assembly moves the magnetic flux from the permanent magnet detected by the flux sensor will vary. This has been determined to be a generally linear relationship. Therefore, the position of the arm assembly (more particularly, the permanent magnet in the arm assembly) is tracked by the flux sensor. Further, the arm assembly as does prior art arm assemblies has a park or stop position. However, unlike the prior art arm assemblies, the arm assembly of the present invention is completely moved away (fully retracted) from the disk in its park position.
In this fully retracted position the heads and disk are immune to induced shock and vibration.
The electronics unit has a novel peak detection ~!, circuit. In the prior art individual peak detectors were used to recover each servo burst (for head positioning, i.e., track location and center). The use of a single peak detector, as in the present invention, requires high speed operation. With a single circuit, ., ~3 ,, '~ ,! , 21~9~9 temperature induced variations are consistent for each servo. The circuit comprises a precision rectifier for rectifying a servo burst. The rectified signal is then integrated by an ;ntegrator. The integrated signal 5 passes through a multiplexer and is converted to an eight bit word by a high speed A/D converter.
The above-discussed and other features and advantages of the present invention will be appreciated , and understood by those skilled in the art from the -4 lo following detailed description and drawings. ~ ~-`! Brief DescriPtion of the Drawinas ;~ Referring now to the drawings wherein like j elements are numbered alike in the several FIGURES:
FIGURE l is a perspective view of a disk drive 15 cartridge and associated electronics unit in accordance with the present invention;
FIGURE 2 is a block diagram illustrating interconnection of the disk drive cartridge and the electronics unit of FIGURE l;
FIGURE 3 is an exploded perspective view of the disk drive cartridge of FIGURE l with the cover removed;
FIGURE 4A is a top view of the disk drive cartridge of FIGURE l with the cover removed;
FIGURE 4B is a side elevational view partly çut 25 away of the disk drive cartridge of FIGURE l;
` ! FIGURE 4C is a rear elevational view partly cut ~ away of the disk drive cartridge of FIGURE l;
j FIGURE 4D is a view taken along the line 4D-4D
with the arm and sensor removed for clarity;
~ 30 FIGURE 4E is a top diagramatic view of flexible circuitry used in the disk drive cartridge of FIGURE l;
FIGURE 5 is a side e3evational view partially in cross-section of the spindle motor assembly used in the -,i disk drive of FIGURE l;
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. -5-FIGURES 6A-B are views of a canted spring used in the spindle motor assembly of FIGURE 5 wherein, FIGURE
6A is a top view thereof and FIGURE 6B is a cross-sectional view taken along the line 6B-6B in.
FIGURE 6A;
~ FIGURES 7A-B are views of a circuit board assembly i used in the spindle assembly of the disk drive i cartridge of FIGURE l wherein, FIGURE 7A is a top view 1 thereof and FIGURE 7B is a cross-sectional view taken ~ 10 along the line 7B-7B in FIGURE 7A;
i FIGURE 8 is a block diagram of the spindle servo i circuit used in the electronics unit of FIGURE l;
FIGURES 9A-B are views of the arm assembly used in the disk drive cartridge of FIGURE 1 wherein, FIGURE 9A
is a top view thereof and FIGURE 9B is a side elevational view thereof;
FIGURES lOA-B are views of the magnet assembly in the arm assembly of FIGURES 9A-B wherein, FIGURE lOA is a top view thereof and FIGURE lOB is an elevational view thereof;
¦ FIGURES llA-D are views of the sensor assembly used in the disk drive cartridge of FIGURE l wherein, FIGURE llA is a bottom view thereof, FIGURE llB is an end view thereof, FIGURE llC is a top view thereof and FIGURE llD is a view taken along the line llD-llD in :~ FIGURE llA;
FIGURE 12 is a block diagram of a closed loop system used by the electronics unit of FIGURE l; !
FIGURE 13 is a block diagram of the circuitry of ~ 30 the electronics unit of FIGURE l;
:~ FIGURE 14 is a diagram of embedded servo bust -information used for track centering and location in accordance with the present invention;
FIGURE 15 is a timing diagram for the embedded servo burst information of FIGURE 14;

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: ! --6--, FIGURES 16A-C are a schematic diagram of the servo recovery circuit in accordance with the present invention; and FIGURE 17 is a top level structure chart of the ~
, 5 software in accordance with the present invention. - ;

-,l, Description of the Preferred Embodiment:
Referring to FIGURES l and 2, a disk memory system ~i, is shown generally at 50. Disk memory system is a high l, capacity, high speed memory system which is designed to `l~ 10 operate in severe environments (e.g., a military ' aircrat). Disk memory system 50 comprise a disk drivè
cartridge 52 and an electronics unit 54. Disk drive cartridge 52 comprises five magnetic hard disks providing 300 megabytes of usable capacity. The disks utilize Winchester disk technology and are housed in a hermetically sealed, self-contained unit which is ~l configured as a plug-in module. Accordingly, disk ~ drive cartridge 52 is fully interchangeable and capable -,- of rough handling, transportation and operation in ~`t 20 extreme environments of vibration, shock and temperature.
l Disk drive cartridge 52 comprises a housing 58 J which has a main housing section 60 with a removable cover plate 62 which is fastened to main housing ;~ 25 section 60 with a plurality of screw fasteners 64.
Housing section 60 and cover plate 62 are of metal, , preferably aluminum. A front cover 66 has a release latch mechanism 68 for locking the housing into or ~, releasing it from a vibration cradle (not shown) equipped with shock mounts in which the unit would be mounted. Housing section 60 has a mounting slot 70 along the length of its two opposite sides, and these grooves mate with corresponding runners or guides in the cradle. To insure that the unit is properly .; :......................................................................... .

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mounted in the cradle (and to insure proper alignment with electrical connectors on the back end of the unit), the grooves are offset on the two sides of the unit (as are the mating guides in the cradle). Since the grooves and mating guides are asymmetric, the unit can only be mounted in one position (i.e., the proper one) in the cradle.
Electronics unit 54 comprises a sealed metal structure 72 wherein the electronics for the system are housed. Structure 72 comprises a main housing section 74 with a removable cover plate 76 which is fastened to housing section 74 with a plurality of screw fasteners '73. Housing section 74 and cover plate 76 are of metal, preferably aluminum. A plurality of connectors 78 are mounted at a front end of housing section 74 to ~ provide a means for interfacing electranics unit 54 j with disk drive cartridge 52, a host computer 85 (FIGURE 2) and a power source. Electronics unit 54 li ,also includes an elapsed time indicator 75, a bit initiate switch 77 and bit indicator 79.
Disk drive cartridge 52 is interconnected with ~',.J3 electronics unit 54, more particularly disk drive i~ control electronics 80, by signal lines 82 (i.e., cables). Disk drive control electronics 80 communicates with interface electronics 84 (described ~i .
hereinafter) within electronics unit 54 by signal lines 86. Electronics unit 54, more particularly interface electronics 84, communicates with host computer 85 via a small computer system interface (SCSI) bus 88 (i.e., cables).
Referring to FIGURES 3 and 4A-E, disk drive ~ cartridge 52 includes a spindle assembly 90 (described `"3 hereinafter). Spindle assembly 90 includes a circuit 3, board 96 at its lower end. An actuator plate 100 is ~`
mounted within housing section 60 adjacent spindle }~

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assembly 90. An arm pivot shaft 102 extends upwardly from actuator plate 100. A field assembly 104 h?ving a head loading assembly 106 mounted thereon is mounted on l actuator plate 100. Field assembly comprises a core Z 5 104a, an upper field 104b and a lower field 104c. A
pair of adjustable arm stroke limiters 108 are mounted at opposing ends of field assembly 104 by fasteners 109.
A first bearing assembly 110 is disposed on shaft 102 and is supported by plate 100. An arm assembly 111 ~i 10 comprises a center arm 112 having upper and lower arms 114, 116 attached thereto by fasteners 117. Arm l assembly 111 is disposed on shaft 102 and is supported - -¦ by bearing 110 to allow the arm assembly 111 to rotate i, relative to shaft 102. Center arm assembly 112 , 15 includes a housing portion 118 wherein a voice coil unit 120 is housed. Voice coil 120 includes a central opening 120a wherein motor core 104a is disposed. The current through voice coil unit 120 in cooperation with ~ field assembly 104 drives the arm assembly in a linear ~
;~ 20 fashion. A landing zone flag 117 and landed position -~, flag 119 are mounted to housing 118. Flags 117 and 119 ~`¦ are detected by an optical assembly 115. Each arm 112, ,Z 114, 116 includes a plurality of flextures 121.
Flextures 121 have a raised or button feature 122 on at ~i 25 least one surface thereof and a head assembly 124 disposed at one end thereof. A second bearing assembly m~
126 is disposed on shaft 102 ;above the arm assembly.
~ut and preload washer~s 128 are secured to shaft 102 to retain and provide a preloading force on the arm assembly. A clock plate 130, preferably comprised of -metal, is secured to housing section 60, spindle ~ -~` assembly 90 and shaft 102 by a plurality of screw -~
~, fasteners 132. ~

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A landing pad and ramp bracket 134 is mounted to l actuator plate 100. A landing pad and ramp slide 136 l is mounted to bracket 134 by fasteners 137. Landing pad and ramp slide 136 includes a plurality of landing ramps 138 and landing pads 142. Landing ramps 138 include recesses 140 which are configured to accept buttons 122 on flextures 120.
~ A voice coil flex circuit 144 is secured to a flex mounting bracket 146 by a pair of fasteners 148.
~ 10 Bracket 196 is mounted to plate 100 by fasteners 150.
;-~ Circuit 144 provides connection to voice coil 120.
¦ A hybrid circuit board 152 is mounted on a mounting bracket 154 which is secured to the inside surface of housing section 60. A head flex circuit 151 is connected to board 152 and is retained by a flex retainer 154 attached to board 152 by fasteners lS6.
Circuit 151 is connected at the other end to the arm assembly. Fasteners 156 also secure one end of board 152 to bracket 154. The other end of board 152 is secured to bracket 154 by fasteners 158. Flex circuit 151 includes a stiffener 1600 Another flex circuit 162 provides connection between board 152 and a connector -164 through a rear end of housing section 60. A
spindle motor flex circuit assembly 166 provides connection between board 96 and connector 164.
, Spindle assembly 90 comprises a plurality of magnetic recording disk 168 (e.g., five disk) disposed about a spindle motor a~ssembly 170. Disk 168 are ! `
spaced apart by a plurality of disk spacers 172. Disk ~ 30 168 and spacers 172 are retained on assembly 170 by a !~ disk retainer 174.
~ Spindle motor assembly 170 spins the disks 168 in `ij a precise rotary path so that the magnetic tracks on ` ~ the disks remain in an established concentric location through the operating environment of extreme ;.
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:~ ~ ' ~ ` 21~249 , temperature and vibration. This degree of accuracy ultimately limits the minimum track width that can be ¦ used and the related maximum tracks per inch which is directly related to data capacity (described hereinafter).
, Prior art commercial disk drives are susceptible to vibration and temperature. For example, during exposure to low levels of vibration, the disk platters begin to wobble as the spindle bearings are overloaded ll 10 by g forces and, in some instances, the shaft itself J can bend and contribute to this effect. Displacements ;I as small as 300 minches will cause track mispositioning and data errors. Further, when exposed ~ -, to the temperature range of -55C to +71C, severe `, 15 track mispositioning occurs due to both the design of -~l the disk clamp and the disk media itself. In the case -~
`J of the disk clamp, a mismatch of temperature ~5 coefficients resulting from a steel spindle shaft , (re~uired for the bearing load) and an aluminum platter -- -causes the platter to expand and contract around one of i the clamp fastening screws, rather than the center line - -, of the spindle. This causes a 'one time around' wobble ;~ of the platter resulting in track mispositioning and -, data errors. Also, a second temperature induced effect ~; 25 is caused by the non-uniform coefficient of thermal ~! expansion around the circumference of the platter. -This lack of concentric expansion and contraction over temperature of anisotropy also caused track -~
1 mispositioning and data errors. The spindle assembly `~ 30 90 of the present invention has resolved these ~;
vibration problems.
Referring now to FIGURE 5, spindle motor assembly 170 comprises a hub 176 with a shaft 178 at about the center thereof. Shaft 178 (preferably a steel shaft) is mounted on a support plate 180. Spindle shaft 178 ~i .::

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. ' ' " ' ' ' ~ , ' ,, ~, ' ' ~ ' . ' ' , ' ., ' ' ': . ' ' ' , ' '' , ; ~ ` 21~2~9 ;', is attached to support plate 180 by screw threads 182, and spindle shaft 178 has a hollow interior defining a central passageway 185. Support plate 180 is, in turn, fastened to the bottom of outer case 60 by a plurality of screws (not shown). The upper end of spindle shaft 178 is held by plate 130 via screw 132' (FIGURE 4B).
- Thus, both the upper and lower ends of spindle shaft 178 are rigidly held.
An annular motor winding 184, which forms the stator of an electric motor is mounted on shaft 178 via .l upper and lower sleeves 186, 188. Sleeves 186 and 188 are secured about shaft 178. Sleeve 186 is secured to shaft 178 by a locking bar 189 and set screw 190. A
washer 191 sits on a shoulder 192 of shaft 178. Washer ~; 15 191 and shoulder 192 support sleeve 188 and stop it from downward movement along the axis of spindle shaft 178.
The rotor structure of the motor has an annular magnet 194 which is adhesively bonded to a steel sleeve 196 which, in turn, is locked to rotary outer steel hub 176. An annular cap 198 is fit within the inside -~.
diameter of hub 176 at the upper end thereof.
I Magnet 194, sleeve 196, hub 176 and cap 198 constitute a rotor structure which rotates around the stator structure mounted on the spindle shaft 178, so `~1 this rotor structure must be mounted on bearings.
According, the rotor structure is mounted on lower and upper bearings 200 and 202. The inner race of lower bearing 200 is trapped and locked against rotation between a shoulder 204 on spindle shaft 178 and a shoulder 206 on base plate 180. A radially inwardly extending flange 208 from hub 176 engages the rotating outer race of bearing Z00.
'~ The floating inner race 209 of upper bearing 202 ~s 35 is held at spindle shaft 178 by a pair of canted , .' ?
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, -12-~, springs 210 which are disposed within a recess or groove 211 about shaft 178. Canted springs 210 are preferably comprised of 302 stainless steel wire per ASTM-A580. Canted springs 210 eliminate abrupt metal ~ 5 to metal contact (due to external vibration/shock ;~ environments) between race 209 of bearing 202 and spindle shaft 178. The abrupt contact generates head position errors which are outside the bandwidth of typical closed loop servos (e.g., a normal bandwidth ~ 10 for a closed loop servo is 250 Hz). However, the i present invention has track densities of about 2075 tracks per inch with center spacing of about 476 minches. This is a much higher capacity than taught j by the prior art (e.g., about 875 tracks per inch).
The abrupt contact does cause head errors within the bandwidth of the closed loop servo of the present invention. Accordingly, the canted springs 210 avoid the abrupt contact and, therefore, eliminate head position errors caused by such contact. The canted springs 210 are aniimportant feature of the present invention, since they provide a high axial and radial stiffness in the spindle motor assembly which, in turn, provides high vibration/shock/temperature resistant performance. The canted springs 210 also provide ~ ;
adequate axial movement allowing for bearing preload.
This movement is requi-red for a constant bearing ~, preload to be applied as materials expand and contract ~-with temperature variations. One of the two identical canted springs 210 is shown in FIGURES 6A-B. Spring 210 comprises a plurality of continuous coils 212 configured to form a ring shape having an .nner diameter for engaging the recessed portion of shaft 178. The inner race 209 of bearing 202 is also held by a washer 213.

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~ 210~2~9 ::j Washer 213 is held in place by a spring washer 214, a washer 215 and a nut 216 which is threaded onto 3 the top of spindle shaft 178. The rotary outer race of bearing 202 engages a radially inwardly projecting.
¦ 5 flange 218 on cap 198. Thus, the rotor structure of , magnet 194, sleeve 196, hub 176 and cap 198 are supported for rotation by bearings 200 and 202.
'!' A preload force also is imposed on bearings 202 by . nut 216 acting through washer 210, spring washer 214 :
and washer 213 to impose a lead on the inner race which, in turn, is transferred through to the balls of i~
~! bearing 202 to load the outer race against the flange :l 218 on cap 198. The preload is also imposed on bearing 200 by being transmitted from cap 198 through sleeve 196 and outer hub 176 to load the outer race of bearing 200, and thence through the balls of bearing 200 to react against plate 180. The preload operates to ~, maintain contact throughout the bearing pack to reduce l~ the effects of shock load and vibration.
Wires 220 from the windings of stator 184 pass into central passage 185 in spindle shaft 178 through a . pair of opposed openings 222 in spindle shaft 178. The wires 220 pass through a passage 224 in plate 180 and are connected to printed circuit board 96. Board 96 is spaced from and attached to plate 180 by a plurality of spacers 226 and screws 22~ which thread into plate 180. Current is delivered through wires 220 to the windings of stator 184 to drive the rotor and discs 168.
; Referring to FIGURES 7A-B, spindle motor circuit ~ 30 board 96 includes a plurality of Hall effect circuits :~ 230, 232 and 234, each comprising a Hall effect sensor 236, resistors 238, 240 and a concentrator 241.
Circuit 234 also includes a capacitor 242. Sensors 236 and capacitor 242 are secured to board 96 by a suitable adhesive. Circuit board 96 is generally round and has ~,.
'' : , ~ .2~092ll9 ~ -14-'' an outside diameter about the same as disks 168. ~oard 96 also has an opening 244 at about the center thereof where shaft 178 passes. Hall effect sensors 236 are used to provide rotating magnet position information which is fed into a spindle servo circuit 245 (FIG~RE
8). The disk spindle rotation speed is controlled by the closed-loop velocity servo circuit 245 and the motor (described hereinbefore). A phase-locked loop 246 on the spindle servo circuit uses the Hall signals to lock the spindle speed. The spindle servo circuit ~ -~
245 includes a predriver 247 which regulates the amount ~
of drive current set regardless of temperature induced ~ ~-gain variations. This results in predictable and ' repeatable spindle start times throughout the operating temperature extremes. , A temperature sensor ~47 is mounted on circuit board 96. A mounting pad 248 is disposed between ... i .
sensor 247 and board 96. Temperature sensor 246 is an ~ important feature of the present invention. The output `,j 20 of temperature sensor 247 is used to modify the seek algorithm. More specifically; drive current levels to the voice coil 120 are adjusted for temperature '~
,~i variations (since voice coil resistance changes with ~ -~
'~i te,mperature), to adjust head load/unload operation, to ,~ 25 modify temperature drift for readings of Hall effect ',~ devices, and to better account for flex bias of capton flex circuits.
` The output of temperature sensor 247 is used to --modify servo parameters during head load/unload and seeking operations. The output of temperature sensor ~ 247 is converted by an A/D converter 456 (FIGURE 13 `, described hereinafter in conjunction with the novel peak detection circuitry) which is controlled by the ~1 ~`, drive controller 350. The corresponding temperature ,`, 35 dependent servo parameters are stored in a RO~ lookup . ~ . " , .

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table. The foliowing servo parameters are temperature ;1 dependent for head load/unload operation:
(l) Hall effect position sensor gain; and (2) driving current necessary to drive the actuator arm in an open loop fashion at a constant acceleration.
The following servo parameters are temperature il dependent for seeking operation:
(l) flexible head cable compliance; and ~3 10 (2) driving current necessary to accelerate ~l actuator arm at constant acceleration.
~', Typical commercial disk drives are susceptible to what is commonly known as 'head crashes' when e~posed to vibration. The flying head is supported by an air bearing which is stable and stiff enough to resist contact with the disk surface due to the exponential '~, nature of the air bearing force vs. displacement i~ curve. It has been determined that head crashes and media damage generally occur when the disk drives are exposed to vibration during the following operations.
~apidly positioning the head laterally track to track which tends to tilt or roll the head causing the air bearing to become unstable, particularly under vibration. By optimizing~the head flexure attachment point to the center of gravity of the head the tendency to tilt or roll the head under rapid positioning is eliminated, whereby air bearing stability is increased and tolerance to operating vibration is improved.
Crashes also occur when the disk is spinning up or down, whereby the head air bearing is weakened and, under vibration, the head may come into contact with the disk. Also when the disk is stopped, the head will rest on the disk surface. Normally, during spin down, most commercial disks allow the head to come in contact wi~h the disk surface until the disk is spun up again '~'1 .
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:
and the air bearing re-established. This condition is not suitable in a military type product which is subject to operational shock, vibration and rough handling.
Accordingly, at the first onset of spin down, the head must be removed away from the disk surface. The arm assembly 111 of the present invention provides for ~ the heads to be completely removed away from the disk. -; Referring to FIGURES 9A-s~ the actuator arm -l 10 assembly is shown generally at 111. Arm assembly ~` comprises center arm assembly 112, upper arm 114 and lower arm 116. Center arm assembly includes housing ~ portion 118. Arm assembly 111 is dynamically balanced ; around its pivot axis so that inputs of shock, ~ -~
~ 15 vibration and load factors to the cartridge do not`~ induce torsional effects in the arm. This results in the head staying on track during high acceleration ~ input disturbances. Housing 118 has a cylindrical ;! opening 250 therethrough having a diameter sufficient for accepting bearings 110 and 126. Housing 118 also ; has opposing pairs of rectangular opening 252, 254~ which define a cavity within housing 118 wherein voice 3 coil 120 is mounted. Housing 118 further includes yet -~, another opening 256 wherein a magnet assembly 258 is mounted by fasteners 260 to housing 118. Also, ~;
referring to FIGURES lOA-B magnet assembly 258 comprises a block assembly 262 having an accurate front ~ , surface 264, opposing side surfaces 266, 268, a rear `~ surface 270 including extensions 272 at each side 266, 268 and opposing top and bottom surfaces 274, 276. A
mounting hole 278 is provided at each extension 272.
Fasteners 260 pass through mounting holes 278. Surface , .
`1 274 includes a platform 280 having a channel or slot 282 therein. A permanent magnet 284 is secured in -¦ 35 channel 282 by a suitable adhesive. Magnet 284 ~ 3 .:. , ,.1 -`,'1`

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~ -17-;'' , includes opposing accurate front and rear surfaces 286,287, side surfaces 288, 290, and top and bottom surfaces 292, 294. Magnet 284 has a north pole 296, `~ designated (N), at end 288 and an opposing south pole 'tj 5 298, designated (S), at end 290.
; Referring to FIGURES 4A and llA-D, head loading sensor assembly is shown at 106. Assembly 106 1 comprises a printed wiring board 300 having opposing bottom and top surfaces 302 and 304. A magnetic flux ~ 10 sensor 306 (i.e., a Hall effect sensor) having leads "~3 308 is mounted at surface 302 by a suitable adhesive.
Sensor 306 is positioned over a Hall effect ~ concentrator 310 disposed within an opening 312 through;~ board 300. A plurality of contact pins 314 extend through board 300. Pins 314 provide connection means with spindle motor flex circuit assembly 166.
Resistors 316, 318 and a capacitor 320 are mounted at surface 304 of board 300. Sensor 306 is preferably a Hall effect type magnetic flux sensor having a ceramic substrate with a hermetically sealed element. Sensor 306 senses magnetic flux from magnet 284 in the actuator arm assembly 111. Assembly 111 is shown in the parked or fully retracted position in FIGURE 4A, whereby buttons 122 on flextures 121 are disposed within recesses 140 of landing ramps 138 with heads 124 disposed between corresponding landing pads 142. In this position the heads and disks are immune to induced shock and vibration. This fully retracted position of the arm/head assembly is an important feature of the present invention. In this fully retracted position the magnetic flux from magnet 284 sensed by sensor 306 is greatest. As the arm assembly 111 is rotated to position heads 124 over corresponding disks 168, magnet 284 will move away from sensor 306 reducing the magnetic flux from magnet 284 sensed by sensor 306. It .. .!
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has been determined that the output of sensor 306 relates to arm assembly lll posi~ion (i.e., head - ~-position) in a linear manner. Accordingly, sensor 306 senses magnetic flux from magnet 284 to determine head , 5 position.
Also, automatic head retraction is accomplished in both the normal and abnormal operating situations. For normal operation, the heads are retracted off the media whenever the spindle is turned off. Retraction is accomplished in less than lO0 m seconds so it does not add appreciable time to an orderly shutdown. The -~-abnormal operations occur when the primary system power is lost or when the operator inadvertently removes the cartridge while the spindle is still spinning. In response to a primary power failure which would cause the disk to stop rotating, electronics senses power failure and utilizes the back E~F of the spinning spindle motor to generate the power required for retracting the heads off the disk and onto the resting pads. Thus the energy in the rotating inertia of the motor and disk assembly is converted to retraction motion unloading the heads, and protecting both them and the media from exposure to shock and vibration.
The second abnormal sequence occurs if the operator removes the cartridge while the spindle is spinning.
~, In this case a sensor in the cartridge handle senses ! that the handle release has been activated. The - electronics respond to this signal by rapidly retracting the heads to the resting pad. Here again, 3~ this is accomplished in less than lO0 m seconds, which ` is before the cartridge has disengaged the connector.
The use of magnetic flux sensor 308 and magnet 284 as a position sensor is an important feature of the present invention. This position information can be used to correct position errors.

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~., Referring to FIGURE 12, an example of such a ~,1 closed-loop system is shown generally at 322. A
-' commanded position signal is presented on a line 324 to a summing junction 326. The output of junction 326 on a line 328 is a position error and is utilized by l actuator arm dynamics 330 to position the heads. The - position of the heads is sensed by a position sensor -j (i.e., sensor 308 and magnet 284) at 332. A signal indicative of head position is presented on a line 334 to junction 326, The actuator arm position 322 ",`,! determined by the Hall efect sensor 332 (e.g. sensor ~1 ~
l 306) is fed back at 334 and subtracted from the j commanded position at 324 to provide the position error j signal at line 328.
Referring to FIGURE 13, controller interface electronics 84 comprises an I/O controller 336, e.g., an Intel 80C186 microprocessor (operating at 12.5 MHz) as the main control element. The Intel 80C186 is a highly integrated 16 bit microprocessor with chip select logic, two channel DMA controllers, three timers and an interrupt controller contained on-board. A
control program is stored in memory 338 of electronics 84, e.g., a 64K x 16 bit EPROM or E PROM. There are also two 32K x 8 static RAMs (SRAM) 340 for scratch pad and variable storage. Further, twelve discrete system input signals and sixteen discrete output signals are used for various functions from control of the ready -~
~`~ light, to I/O controller, to drive controller communications. A combination I/O an disk data controller 342 (e.g. an 8496 from National Semiconductor) is in electronics 84. The I/O section -~
344 of this device is implemented as a state machine sequencer that receives commands from the processor.
These commands execute various functions such as data in phase and status phase. When an operation is , .
~, ~ ' ": ' ' 2~2~
, , complete an interrupt to the I/O controller is activated. Various control status registers are used to store error status conditions. The disk data ~
controller 346 section is also a state machine --~, 5 sequencer that executes commands issued by the I/O
-, controller. The commands control the reading and writing to the disk. Again, various control, status -~, and error registers give the ability to correct errors or determine if a retry is necessary. The com~ination I/O and disk data controller utilizes its own dedicated data buffer which consists of two high speed 32K x 8 SRAMs. Three disk channels into the data buffer are , controlled by the I/O and disk data controller. The ,~ three channels are I/O, disk and processor. The disk ~! 15 channel has the highest priority and the processor ~ channel the lowest. This scheme allows for concurrent -, data transfer between the I/O and disk interfaces.
Thirty-one analog voltage channels monitor various ` system functions for self test. An eight bit A/D 348 measures these channels and the BIT software determines , if there is a fault in the system.
~ Disk drive cartridge 52 utilizes both a dedicated ^~ surface and embedded servo system. This means that one of the five media platters is totally dedicated to ;! 2s track servo information. Servo information is also embedded on all other surfaces at the beginning of every sector on every track. This servo system provides the best combination of coarse and fine positioning necessary for high speed operations in extreme environments.
~;, Disk drive circuitry 80 implements the critical drive level functions necessary for high speed disk drive operations. Disk drive circuitry provides read/write head positioning (control of the rotary actuator motor, i.e., movement of voice coil 120 in ,. ~
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field assembly 104), read/write head selection, spindle ~ motor start/stop, BIT functions, and power interruption ,!l and transient recovery control.
' A drive controller 350 is the main controlling , element of the disk drive circuitry 80. The drive ;j controller utilizes a high speed digital signal processor (e.g., Texas Instruments TMS 320C30 ~ state-of-the-art 32 bit digital signal processor) to i control the position of the heads through the implementation of a closed-loop digital control algorithm.
The disk drive control scheme utilizes a I complimentary system of dedicated and embedded servo information to insure optimum control of read/write head position during track seek, read and write operations.
Track acquisition is accomplished via closed loop control 352 of the rotary actuator. Coarse position information is written on a dedicated surface (i.e., ~ 20 one surface of one of the five disks 168) and is ?"~ comprised of alternating tracks 0.70 MHz and 1.00 MHz signals. The mid point between each of these tracks defines the center of each cylinder and consequently the data tracks located on the remaining disk surfaces. When a seek command is received, the drive controller utilizes the coarse position information to control head actuator acceleration and velocity during the seek operation.
Once track acquisition is complete, the embedded servo 354 information on the acquired track is utilized to perform track centering and following. Referring to FIGURES 14 and 15 a novel peak detector (described hereinafter) is utilized to recover amplitude information for each of four servo bursts, designated ~s 35 A, B, C, D respectively. This information is processed ,~

2 ~
:, , by the drive controller 350 to determine exact head position and the amount of current to apply to the rotary actuator (i.e., voice coil 120) to correct and maintain head position.
Tracks Al, Bl, A2, B2, A3 3 shown in FIGURE 14. The embedded servo information is designated A, B, C and D respectively. The amplitude peak information indicated at 356 is detected by the novel peak detector circuitry described hereinafter.
This servo information is a quad burst of time displaced pulses (e.g., a burst may compromise a 2.5 MHz sine wave for 4 m sec.). The heads can be maintained on track centers by equalizing, the amplitude between overlapping servo burst. For example, burst 358 designated A and burst 360 , designated B overlap track center line 362 of track `~ Al. Line 362 corresponds to equal amplitudes for both A and B as designated by VA and VB (i.e., ~l VA=VB). Accordingly, the heads can be maintained `~, 20 on track center by adjusting head position so that amplitudes between overlapping servo bust are equal (e.g., VA = VB). The quad burst provides for linear track-to-track positioning with a tolerance of +/- one track. Also, these embedded servo burst are used for track to track positioning and fine `~, positioning, as described hereinbefore.
Each sector (0-54, FIGURE 15) includes a data segment 364 which is preceded by the embedded servo burst A, B, C and D. The timing sequence for the i 30 embedded servo/sector is provided in FIGURE 15. This ` includes timing or the following operations: zero;
3 dedicated surface index; sector mark detection window;
read signal, data head; sector mark detected;
~i multiplexers Ao, Al, and A2; servos CS, WR, INT
~ 35 and RD; and embedded servo reset.

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-~`` 2~ ~9%~9 ., A rotary actuator drive circuit 365 comprises a ;1 twelve bit D to A converter 366 and an amplifier 368.
;~ The actuator drive 365 receives positioning data from the drive controller 350 which is converted to analog voltage for the rotary actuator motor drive. Velocity ii profiles and rotary actuator drive currents are kept constant regardless of variation in resistance to ~ provide optimum performance throughout the severe '? environments.
The drive controller 350 is supported by a drive controller memory which utilizes both RAM 370 and PROM
372. The RAM 370 is a 64 Kbit CMOS static RAM
;~ organized as 2K x 32 and is on-board the drive ¦ controller. It is used to temporarily store and manipulate program data elements. The PROM 372 is a l Mbit CMOS EPROM organized as 32K x 32 which stores the drive controller operating program.
The drive controller 350 communicates with the disk data processor through a parallel communications port. Input/output ports for discrete signals are also .~ provided. The discrete signals come from other parts Y of the disk electronics 80 and cartridge 52 and include . 'heads retracted", "handle closed", communication port t. flag, A/D converter status and power status. Output L~ 25 signals are also incorporated and include spindle motor !;', enable, rotary actuator enable, head selection, A/D and~; D/A converters. -~
The closed-loop spindle control circuit 374, described hereinbefore utilizes a Hall signal feedback 376 to control spindle speed.
Read/Write analog signal processing circuitry 378 provides the high density encoding/decoding for disk data read/write operations. The data is encoded from NRZ and clock to run length limited by an encoder 380. `
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During the write process, NRZ formatted data and clocking information is encoded and supplied to the write drivers. During the read operation, encoded data stored on the disk is recovered by analog amplification and detection with subsequent clock recovery and decoding via a data synchronizer, phase lock loop (PLL) 381 and a run length limited (RLL) to NRZ decoder 382.
The first stage of the analog circuitry includes an automatic gain control amplifier, which maintains a constant signal amplitude at the output of a Bessel ; filter in the read string. The Bessel filter band ~! limits the read signal supplied to the equalizer and detector. The equalizer restores critical amplitude I and phase information for detection of the data , transitions by the detector circuitry.
, The output of the data detector is supplied to the ~ phase comparator o~ the phase-locked loop via a data .Z synchronizer. The synchronizer is utilized to insure , fast acquisition of phase lock by running the PLL on a reference clock when the system is not in the read mode. The synchronized run length limited data and `~
phase-locked clock are supplied to a decoder 382 for ~ conversion to NRZ data and clock.
Y Write interlocks and cartridge file protectioncapabilities are incorporated into the circuits at 384 to allow for user-selectable protection against loss of stored information due to an inadvertant overwrite.
Referring to FIGURES 16 A-C, the novel peak ~, detection circuit is shown generally at 386. FIGURE 16 -~
.`Z 30 A-C are a schematic diagram of the track following servo electronics 354 and the course position servo 352. Accordingly, the schematic also shows a dedicated servo detection circuit 388, an index detection circuit -390 and a sector mark detection circuit 392. The peak detection circuit 386 comprises a precision rectifier `
.' ~, ï 2 l ~ 9 ~ ~5 9 .. ! i `

394 having an input on line 396 to an amplifier 398.
Amplifier 398 has a feed back loop comprising resistors 400, 402 and a diode 404. The output of amplifier 398 i i is connected to a diode 406. A capacitor 410 and an ,~ 5 inductor 412 are also connected to amplifier 398. An ¦ output of rectifier 394 is presented on a line 408.
This output is a precision rectified signal of the input signal (i.e., servo burst) presented at line -~
396. An integrator 414 receives the signal presented at line 408. This signal is presented through a resistor 416 to an input of an amplifier 418. A
resistor 420 is connected between ground and the other input of amplifier 418. A capacitor 422 and an inductor 424 are also connected to amplifier 418. The output of amplifier 418 is presented on a line 426.
~'3 Thi~s output is an integrated signal of the signal input at line 408.
An integration dump 428 receives the signal presented at line 426. Dump 428 comprises a pair of high speed analog switches 430, 432 and a resistor 434. The integrated signal is then presented on a line s 436 to an amplifier 438 having a feed back resistor ~ 440. The other input of amplifier 438 is connected hy ;~ a resistor 442 to ground. The output of amplifier 438 on line 444 is presented to a multiplexer 446.
Capacitors 448 and inductors 450 are also connected to multiplexer 446. A selected input of multiplexer 446 is presented at its output on a line 452. The signal at line 452 is presented to an amplifier 454. The output of amplifier 454 is converted from an analog ¦ signal to a digital sigral (i.e., an eight bit word) by an A~D converter 456. A voltage regulator 458 provides a reference voltage to converter 456. Capacitors 460, 462 and resistor 464 are connected to regulator 458.
Capacitors 466, 468 and inductor 470 are connected to converter 456.

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This single high speed peak detection circuit 386 is utilized in conjunction with high speed A/D
converter 456 to recover the magnetically recorded, time division multiplexed, spacially displaced servo s information bursts. This method of recovery is in contrast to prior art commercial practice where individual detectors are utilized for recovery of each servo burst. The benefit of a single recovery circuit is in operation over e~treme temperatures, where parameter drift of individual circuits would have to be accounted for. The single recovery circuit parameter i variations over temperature will be identical for each`
~- servo burst, and would therefore cancel any negative . .
~, effects.
Referring to FIGURE I7, a top level structure chart of the software is provided. The software for -the I/O control 336 performs the following functions: -~
accepts commands from the I/O bus and generates the required control signals to execute the commands;
~, 20 controls data flow between the I/O bus and the disk 'l drive; monitors drive status and reports abnormalities on the I/O bus; and generates and transmits disk status on command. The software for drive control 350 ~;~ controls the following functions: read/write head -`-~
positioning; spindle motor starting and stopping; head -retraction on power loss or cartridge removal;
read/write head selection; power interruption and ~`
;' recovery control for both controllers; built-in-test functions; and drive status monitoring and reporting to the I/O controller. The functions performed by the software are illustrated here by describing the read operation, the write operation and the Built-In Test (BIT) function.
A command is received on the I/O bus and is decoded as a read command by the I/O control. The .' , ~ 21~249 ~, -27-'i ~, status of the drive is checked for cartridge installed and disk spinning.' If these conditions are met, the ' command is determined to be valid and the read operation is started. The address information received with the read command is translated into a head and cylinder number. This information is transmitted in a seek command to the drive control which decodes the seek command and selects the required head. The drive controller 350 then positions the heads on the required ~3 lo cylinder by driving the rotary actuator. This motion may involve acceleration and deceleration depending 3 upon the number of"cylinders the heads must be moved. '' `3 After completion of this open-loop move, the servo error voltage is read and used to center the heads on the track by means of a closed-loop digital control algorithm. After the heads are centered a command complete response is returned to I/O control.
The I/O control loads the disk data controller 346 registers with the proper information to perform a read operation. This information includes the starting sector number on the track and the number of sectors to -~ -be read. As part of the read operation, the I/O
control checks the header information to determine if '~
the heads were centered over the correct track by the ;' 25 open-'loop move. If the heads are on an incorrect track, the I/O control calculates the correction required to position the heads. The I/O control sends ~, another seek command to the drive controI to position the heads correctly. Upon completion of this 0 operation, a command complete is sent from the drive ~'~ control to the I/O control again. Another read operation is performed by the I/O control. During the data transfer from disk to RAM, under the control of the disk data controller 346, error detection is active. If a data error occurs, the disk data ..

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controller 346 supplies syndrome bytes to the I/O
; control to enable it to correct the error. The I/O
control performs an 'exclusive or' operation on the data with these syndrome bytes to correct the data error. After a sector of data has been loaded into ram, the I/O control signals the drive control so that , its disk controller can transfer data from RAM to the `I .
I/O bus. Thus~ data transfers occur concurrently from disk to RAM and RAM to the I/O bus.
` 10 It should be noted that the drive control cannot determine actual head position. Upon receipt of a seek command, it loads a cylinder address register with the cylinder number and makes an open loop move. If the -~`
` I/O control determines an incorrect positioning, it must send a special command to the drive control, which repositions the heads without changing the contents of its cylinder address register. This maintains synchronization between the two controllers. ~;
In the write operation, the same head positioning operations are performed as during the read operation. ;-Data transfers from the I/O bus to RAM are performed concurrently with the initial head positioning operation.
During the execution of BIT some visual indication is provided to indicate progress through the test.
Upon entering the test, both BIT indicators are set.
Next the disk drive cartridge ready led is lit to indicate that both processors are operational. The led is turned off upon completing the ROM checksum tests regardless of the result of the tests. Upon completion of the test, the I/O control processor will clear only those BIT indicators representing a fully functional line replaceable unit (LRU).
The system incorporates a BIT capability to provide failure detection and location functions for . both on-aircraft and off-aircraft levels of 2 1 0 ~ 2 4 9 ~s 1 maintenance. BIT features may be initiated by a combination of manual, automatic or remote commands;
self-monitoring of normal operating modes is also included. Fault status indication is provided remotely ~^
via the bus or locally via the fault indicators.
A BIT power controller is used to control the BIT
indicators. This controller powers the BIT indicator drivers directly from the +28V DC input and provides a power-up pulse to allow both BIT indicators to be set -' 10 upon power-up despite a power supply failure. The ¦ power controller is power sequenced to prevent normal "~ power-up and power-down routines from generating false ~ BIT indications.
i.~ .
Two BIT indicators 79 are provided to give a ~ 15 visual indication of the functional condition of the J LRU they represent. One indicator represents the electronics unit 54 and the other indicator represents the disk drive cartridge 52. Both indicators are magnetically latched so that the last tested functional ~ condition will remain displayed after powering down.
Once set, the indicators will remain set until the indicated LRU successfully passes execution of the BIT
program.
The BIT switch 77 is provided to allow manual initiation of the BIT routine. This switch only initiates BIT when the system is not performing a commanded function.
Wrap functions are provided to test the data path in expanding loops. These wrap tests loop the data locally at the controller, at the encoder/decoder and finally at the disk itself.
The system contains the capability to monitor test , points during the BIT routine. Built in test circuits consisting of an analog to digital converter with a ~1 35 multiplexed input performs discrete measurement of key '~ :
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.
circuit test points located in the read/write data channel, the spindle drive circuitry, the rotary ~i actuator drive and the power supply. The measured ,' values are compared to ROM stored values to determine , 5 signal validity.
. While preferred embodiments have been shown and described, various modifications and substitutions may "~! be made thereto without departing from the spirit and scope of the invention. Accordingly, it is to be ~ 10 understood that the present invention has been ; described by way of illustrations and not limitation.

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Claims (16)

  1. CLAIM 1. A disc drive assembly including:
    support plate means;
    spindle shaft means fixed to said support plate means at one end of said spindle shaft means;
    stator means positioned around said spindle shaft means;
    mounting means for mounting said stator means on said spindle shaft means;
    rotor means around said stator means;
    first bearing means positioned between said spindle shaft means and said rotor means to rotatably support said rotor means for rotation about said stator means and said spindle shaft means;
    loading means disposed between said spindle shaft means and said first bearing means; and a plurality of disc mounted in spaced apart relationship on said rotor means.
  2. CLAIM 2. The disc drive assembly of claim 1 wherein:
    said loading means comprises at least one canted spring disposed about said spindle shaft means.
  3. CLAIM 3. The disc drive assembly of claim 2 wherein said at least one canted spring comprises two canted springs, one of said canted springs longitudinally disposed above the other on said spindle shaft means.
  4. CLAIM 4. The disk drive assembly of claim 2 wherein:
    said spindle shaft means includes a recess wherein said at least one canted spring is disposed.
  5. CLAIM 5. The disk drive assembly of claim 1 wherein:
    said first bearing means includes a floating race which bears against said loading means.
  6. CLAIM 6. The disk drive assembly of claim 1 further includes:
    second bearing means disposed about one end of said spindle shaft means adjacent said support plate means, said second bearing means positioned between said spindle shaft means and said rotor means to rotatably support said rotor means for rotation about said stator means and said spindle shaft means; and wherein said first bearing means is disposed about the other end of said spindle shaft means.
  7. CLAIM 7. The disk drive assembly of claim 6 further includes:
    preload means for imposing a preload on said first and second bearing means.
  8. CLAIM 8. The disk drive assembly of claim 7 wherein said preload means comprises:
    a spring washer about said spindle shaft means; and retainer means at one end of said spindle shaft means for imposing a preloading force on said spring washer.
  9. CLAIM 9. The disk drive assembly of claim 1 wherein said mounting means comprises at least one sleeve attached to said stator means and secured about said spindle shaft means.
  10. CLAIM 10. A disk drive assembly including:
    support plate means;
    spindle shaft means fixed to said support plate means at a first end of said spindle shaft means;
    stator means positioned around said spindle shaft means;
    mounting means for mounting said stator means on said spindle shaft means;
    rotor means around said stator means;
    first bearing means positioned between said spindle shaft means and said rotor means at said first end of said spindle shaft means, said first bearing means for rotatably supporting said rotor means for rotation about said stator means and said spindle shaft means;
    second bearing means positioned between said spindle shaft means and said rotor means at a second end of said spindle shaft means, said second bearing means for rotatably supporting said rotor means for rotation about said stator means and said spindle shaft means, said second bearing means having a floating race;
    loading means disposed between said spindle shaft means and said floating race of said second bearing means; and a plurality of disc mounted in spaced apart relationship on said rotor means.
  11. CLAIM 11. The disc drive assembly of claim 10 wherein:
    said loading means comprises at least one canted spring disposed about said spindle shaft means.
  12. CLAIM 12. The disc drive assembly of claim 11 wherein said at least one canted spring comprises two canted springs, one of said canted springs longitudinally disposed above the other on said spindle shaft means.
  13. CLAIM 13. The disk drive assembly of claim 11 wherein:
    said spindle shaft means includes a recess wherein said at least one canted spring is disposed.
  14. CLAIM 14. The disk drive assembly of claim 10 further includes:
    preload means for imposing a preload on said first and second bearing means.
  15. CLAIM 15. The disk drive assembly of claim 14 wherein said preload means comprises:
    a spring washer about said spindle shaft means; and retainer means at one end of said spindle shaft means for imposing a preloading force on said spring washer.
  16. CLAIM 16. The disk drive assembly of claim 10 wherein said mounting means comprises at least one sleeve attached to said stator means and secured about said spindle shaft means.
CA 2109249 1992-12-23 1993-10-26 Magnetic disk drive unit Abandoned CA2109249A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US99517892A 1992-12-23 1992-12-23
US995,178 1992-12-23

Publications (1)

Publication Number Publication Date
CA2109249A1 true CA2109249A1 (en) 1994-06-24

Family

ID=25541481

Family Applications (1)

Application Number Title Priority Date Filing Date
CA 2109249 Abandoned CA2109249A1 (en) 1992-12-23 1993-10-26 Magnetic disk drive unit

Country Status (4)

Country Link
JP (1) JPH0778449A (en)
CA (1) CA2109249A1 (en)
FR (1) FR2699719A1 (en)
GB (1) GB2273809A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7542225B1 (en) 2006-11-17 2009-06-02 Western Digital Technologies, Inc. Disk drive idle mode responsive to flex circuit cable bias changes

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3419814C1 (en) * 1984-05-26 1985-11-28 GMN Georg Müller Nürnberg GmbH, 8500 Nürnberg Motor spindle for magnetic disk storage
US4676672A (en) * 1985-02-19 1987-06-30 International Business Machines Corporation Precision spindle
JPS62154272A (en) * 1985-12-25 1987-07-09 Nec Corp Positioning mechanism for magnetic disk device
US4814652A (en) * 1987-02-27 1989-03-21 Maxtor Corporation Disk drive motor with thermally matched parts
US4835637A (en) * 1987-09-08 1989-05-30 International Business Machines Corporation Disk file with in-hub motor
US4797762A (en) * 1987-09-22 1989-01-10 Micropolis Corporation Stress free winchester drive shaft mounting
JP2771006B2 (en) * 1990-02-05 1998-07-02 富士通株式会社 Rotary body support device for disk storage device
US5212607A (en) * 1990-07-31 1993-05-18 Seagate Technology, Inc. Disk drive including unitary deck for aligning and supporting axially retractable spindle assembly

Also Published As

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GB2273809A (en) 1994-06-29
FR2699719A1 (en) 1994-06-24
GB9326317D0 (en) 1994-02-23
JPH0778449A (en) 1995-03-20

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