Disk drive having airflow suppressor comb for reduced disk rotation induced airflow
Granted 23 Sep 2003 · 1 office action
Current assignee: WESTERN DIGITAL TECHNOLOGIES · originally Western Digital
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Attorney: Attorney · Log in to unlock
Inventors: Chiao-Ping Ku, Gary C. Griffin, Sudha Narayanan, John R. Gustafson +4 · Examiner: George J. Letscher · AU 2652 · TC 2600
Life of the application
16 dated eventsAbstract
A disk drive including a disk drive base. The disk drive further includes at least one rotatable disk which includes a disk surface extending to an outer disk edge. The disk drive further includes a head stack assembly rotatably attached to the disk drive base in operable communication with the disk. The disk drive further includes an airflow suppressor comb coupled to the disk drive base and stationary relative to the disk drive base during operation of the disk drive. The comb includes a comb body disposed adjacent to the outer disk edge, and at least one tine extending from the comb body along the disk surface for mitigating disk rotation induced airflow upon the head stack assembly adjacent to the disk surface.
Description
6 parts›CROSS-REFERENCE TO RELATED APPLICATIONS
This application is related to U.S. application Ser. No. 09/872,236entitled DISK DRIVE HAVING AIRFLOW SUPPRESSOR COMB WITH CURVED EXTENSION FOR REDUCED DISK ROTATION INDUCED AIRFLOW, filed on May 31, 2001, incorporated herein by reference.
›BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates generally to disk drives, and more particularly to a disk drive having an airflow suppressor comb for reduced disk rotation induced airflow.
2. Description of the Prior Art
The typical hard disk drive includes a disk drive base, a head disk assembly (HDA), and a printed circuit board assembly (PCBA) attached to the disk drive base. The head disk assembly includes at least one magnetic disk, a spindle motor for rotating the disk, and a head stack assembly (HSA) having an actuator assembly having at least one transducer head, typically several, for reading and writing data from the disk. The printed circuit board assembly includes a servo control system in the form of a disk controller for generating servo control signals. The head stack assembly is controllably positioned in response to the generated servo control signals from the disk controller. In so doing, the attached heads are moved relative to tracks disposed upon the disk.
A topic of concern is the desire to reduce the effects of airflow generated within the disk drive due to rotation of the disks. Of particular concern is the occurrence of turbulent airflow which may tend to excite a resonance response of the actuator assembly. This results in an increase in the percent off-track values of the associated head. Further, such disk rotation induced airflow may result in a force applied to the actuator assembly, i.e., windage. In addition, such disk rotation induced airflow may result in vibration of the disk or disk flutter. Accordingly, there is a need in the art for an improved disk drive for mitigation of such disk rotation induced airflow in comparison to the prior art.
›SUMMARY OF THE INVENTION
An aspect of the invention can be regarded as a disk drive including a disk drive base. The disk drive further includes at least one rotatable disk which includes a disk surface extending to an outer disk edge. The disk drive further includes a head stack assembly rotatably attached to the disk drive base in operable communication with the disk. The disk drive further includes an airflow suppressor comb coupled to the disk drive base and stationary relative to the disk drive base during operation of the disk drive. The comb includes a comb body disposed adjacent to the outer disk edge, and at least one tine extending from the comb body along the disk surface for mitigating disk rotation induced airflow upon the head stack assembly adjacent to the disk surface.
The tine may include a base portion disposed adjacent to the comb body. The base portion may be sized and configured to contact the outer disk edge upon deflection of the disk. Further, the disk may include a non-data annular region and the tine has a distal portion sized and configured to contact the non-data annular region of the disk upon deflection of the tine.
›BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a perspective view of a disk drive (cover not shown) including an airflow suppressor comb as constructed in accordance with an aspect of the present invention;
FIG. 2 is a perspective view of the airflow suppressor comb of FIG. 1;
FIG. 3 is a cross-sectional view of a portion of the disk drive of FIG. 1 as seen along axis 3 — 3 ; and
FIG. 4 is a cross-sectional view of a portion of a disk drive similar to the view shown in FIG. 3, however, including an airflow suppressor comb according to another aspect of the present invention.
›DESCRIPTION OF THE PREFERRED EMBODIMENTS · 1 of 2
Referring now to the drawings wherein the showings are for purposes of illustrating preferred embodiments of the present invention only, and not for purposes of limiting the same, FIGS. 1-4 illustrate a disk drive and airflow suppressor combs in accordance with aspects of the present invention.
Referring now to FIGS. 1-3 there is depicted a disk drive 10 constructed in accordance with an aspect of the present invention. The disk drive 10 includes a disk drive base 12 . The disk drive 10 further includes rotatable disks 14 a-c . However, a single one of the disks 14 a-c may be utilized to practice the present invention. The disks 14 a-c each respectively include opposing disk surfaces 16 a-f . The disk surfaces 16 a-f respectively extend to outer disk edges 18 a-c . The disk drive 10 further includes a head stack assembly 20 rotatably attached to the disk drive base 12 . in operable communication with the disks 14 a-c . The disk drive 10 further includes an airflow suppressor comb 22 coupled to the disk drive base 12 and stationary relative to the disk drive base 12 during operation of the disk drive 10 . The comb 22 includes a comb body 24 disposed adjacent to the outer disk edges 18 a-c . The comb 22 further includes tines 26 a-c extending from the comb body 22 respectively along the disk surfaces 16 a-e for mitigating disk rotation induced airflow upon the head stack assembly 20 adjacent to the disk surfaces 16 a-e . However, a single one of the tines 26 a-c may be utilized to practice the present invention.
In further detail according to an embodiment of the present invention, the disk drive base 12 is contemplated to engage a disk drive cover (not shown in FIG. 1) for cooperatively housing the remainder of the components of the disk drive 10 . The disk drive 10 includes a spindle motor hub 28 (partially depicted in FIG. 3) rotatably attached to the disk drive base 12 . The disks 14 a-c are mounted upon the hub 28 . Spacers 30 a-b separate the disks 14 a-c . A disk clamp 32 is used to secure the stacked disks 14 a-c to the hub 28 . The head stack assembly 20 includes transducer heads (only a single head 34 is depicted in FIG. 1 ). In this regard, the head stack assembly 20 is configured to rotate relative to the disks 14 a-c for reading and writing data therewith.
The airflow suppressor comb 22 may be attached to the disk drive base 12 via a fastener 35 for maintaining the airflow suppressor comb 22 stationary relative to the disk drive base 12 . As shown FIG. 1, the disk drive 10 is configured to rotate the disks 14 a-c in a counter-clockwise direction. In this regard, the suppressor comb 22 is disposed up-stream of the head stack assembly 20 within a common quadrant relative to the disks 14 a-c . It is contemplated that the suppressor comb 22 may be angularly disposed about the disks 14 a-c at other locations relative to the head stack assembly 20 . Moreover, while the airflow suppressor comb 22 is oriented with the tines 26 a-c extending radially with respect to the disks 14 a-c , other angular orientations are contemplated.
Rotation of the disks 14 a-c results in disk rotation induced airflow about the disk surfaces 16 a-f . It is contemplated that the airflow suppressor comb 22 and in particular the tines 26 a-c thereof mitigate such disk rotation induced airflow in comparison to a disk drive configuration which does not include the airflow suppressor comb 22 . In addition to simply creating a physical barrier to such airflow, the tines 26 a-c tend to reduce the relative amount of turbulent airflow resulting in a relatively laminar airflow pattern. As such, this tends to mitigate airflow associated with excitation of the head stack assembly rigid body motion (i.e., arm turbulence), resonance response windage experienced by the head stack assembly 20 , and vibration of the disks 14 a-c (i.e., disk flutter) in comparison to a disk drive configuration without the airflow suppressor comb 22 . In this regard, the present inventors conducted a test utilizing a disk drive whereby off-track displacement was measured during a track follow operation. In a disk drive with a suppressor comb, similar to disk drive 10 constructed in accordance with the present invention, an off-track displacement of the head as a rigid body due to windage (arm turbulence) was determined to have a 1 sigma value of 0.1480 micro inches. In contrast, with the suppressor comb removed, an off-track displacement of the head as a rigid body due to windage (arm turbulence) was determined to have a 1 sigma value of 0.2066 micro inches (a 28% difference).
The disk surfaces 16 a-f may each include data annular regions 36 a-f and a non-data annular regions 38 a-f . Such non-data annular regions 38 a-f (typically referred to landing or parking zones) are typically disposed at the interior-most portion of the disk drive surfaces 16 a-f . The non-data annular regions 38 a-f do not include any recorded data. Thus, when the disk drive 10 is deactivated, the heads may be “parked” at a position where they will not damage the portion of the disk surface containing recorded data. As such, the head stack assembly 20 may be pivoted such that the transducer head 34 is disposed adjacent the non-data annular region 38 a , as shown in FIG. 1 .
The tines 26 a-c respectfully have distal ends 40 a-c . Preferably, such distal ends 40 a-c are disposed adjacent the non-data annular regions 38 a-e . Should the disk drive 10 be subjected to shock of significant magnitude, the tines 26 a-c may deflect in a cantilever manner. However, such particular disposition of the distal ends 40 a-c of the tines 26 a-c would tend to result in the distal ends 40 a-c engaging the non-data annular regions 38 a-e , rather than the data annular regions 36 a-e and possibly damaging the same.
Referring now to FIG. 4, there is depicted a cross-sectional view of a portion of a disk drive similar to the view shown in FIG. 3, however, including an airflow suppressor comb 42 according to another aspect of the present invention. In this regard, there are depicted disks 44 a-c similar to disks 14 a-c described above. As such, disks 44 a-c respectively include outer disk edges 46 a-c and opposing disk surfaces 48 a-f . The disk surfaces 48 a-f each include data annular regions 50 a-f and non data regions 52 a-f . The airflow suppressor comb 42 is attached to a disk drive base 54 . The airflow suppressor comb 42 includes a comb body 56 and tines 58 a-c extending from the comb body 56 .
›DESCRIPTION OF THE PREFERRED EMBODIMENTS · 2 of 2
The tines 58 a-c respectively include base portions 60 a-c disposed adjacent to the comb body 56 . The base portions 60 a-c are sized and configured to contact the outer disk edges 46 a-c upon deflection of the disks 44 a-c . In this regard, should the associated disk drive be subjected to shock of significant magnitude, the disks 44 a-c may tend to rotate in a plane other than their respective axes of rotation. However, the base portions 60 a-c are formed to engage the outer disk edges 46 a-c thereby mitigating contact between the tines 58 a-c and the data annular regions 50 a-e.
In addition, the tines 58 a-c may inc de distal pedestal portions 62 a-c are As sized and configured to contact the non-data annular regions 52 a-e of the disks 44 a-c upon deflection of the tines 58 a∝c . In this regard, the distal portions 62 a-c would tend to engage the non-data annular regions 52 a-e , rather than the data annular regions 50 a-e upon deflection which may possibly damage the same.
Claims as granted
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4 codes- G11B33/08
- G11B33/14
- G11B5/60
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