The present invention is related to servo systems used to control a position of a head relative to a disc. In particular, the present invention provides compensation for large repeatable runout caused by eccentricity between pre-written servo tracks and an axis of rotation of the disc.
Magnetic discs are used in disc drive storage systems for storing digital data and in spin-stands as components on which transducing heads are tested. Disc drives are commonly used in work stations, personal computers, laptops and other computer systems to store large amounts of data on one or more magnetic discs in a form that can be made readily available to a user. The discs are mounted to a spindle motor which rotates the discs at a high speed about an axis. An actuator assembly supports and positions an array of transducing heads over surfaces of the discs to write information to or read information from the discs.
Spin-stands are devices that are used to test transducing heads before they are placed in a disc drive. As in a disc drive, a spin-stand includes a disc that is mounted to a spindle motor which rotates the disc at a high rate of speed about an axis. Also, the spin-stand includes an actuator assembly that supports the head over the disc surface and moves the head to a desired location. The spin-stand allows a series of tests to be performed on the transducing head including, for example, error-rate testing, pulse width-fifty testing, track average amplitude testing, and track scan testing.
The discs used in disc drives and spin-stands generally include circular data tracks which extend circumferentially around each disc. These data tracks are defined by radially extending servo tracks that contain servo information. The servo information defines the boundaries and centerlines of each of the tracks.
Disc drives, and more recently spin-stands, utilize servo systems to control the position of a head relative to the data tracks using the servo information. As a head moves over a surface of a disc, the head reads the servo information and produces an output signal that indicates its position relative to the servo tracks. The output signal is demodulated and compared with a reference position signal relating to a desired head position to produce a position error signal (PES). The PES is provided to a servo controller that produces a control signal which is used to control an actuator mechanisms of the disc drive or spin-stand to move the head toward the desired position or data track. Once the head is positioned over the desired data track, the servo system allows the head to follow the track using the servo information.
The servo tracks are typically written after the discs have been installed in a disc drive or spin-stand with a servo track writer. These “post-written” tracks are substantially concentric with the axis of rotation of the disc on which they are written, since the axis of rotation remains constant from when the servo information is written to when the servo information is used to perform track following. However, uncontrolled factors such as bearing tolerances, spindle resonances, and the like, tend to introduce errors in the location of the servo information. As a result, each track is typically not perfectly concentric with the axis of rotation of the disc, but rather exhibits certain random, repeatable variations which are sometimes referred to as repeatable runout (RRO). This slight misalignment is exhibited in a periodic PES.
There is a continuing trend in the disc drive industry to provide successive generations of disc drive products with ever increasing data storage capacities and data transfer rates. Because the amount of disc surface available for the recording of data remains substantially constant (or even decreases as disc drive form factors become smaller), substantial advancements in areal recording densities, both in terms of the number of bits that can be recorded on each track as well as the number of tracks on each disc (measured as tracks per inch or TPI), are continually being made in order to facilitate such increases in data capacity. One way to improve storage capacities is to improve the writing of the servo patterns on the discs. To this end, servo information is written on the discs prior to their installation in a disc drive or on a spin-stand using highly precise servo writers.
Although these “pre-written” tracks can result in an increase in the TPI of the disc, large RRO will result due to large eccentricity between the data tracks and the axis of rotation of the disc. This eccentricity primarily stems from the re-mounting of the disc to the spindle motor of the disc drive or spin-stand. In addition, the RRO that affects disc drives and spin-stands using post-written discs will also be present when these pre-written discs are used. However, the RRO correction methods mentioned above are not suitable for compensating a PES corresponding to the large RRO resulting from the use of discs having pre-written servo tracks. This is due, in part, to the large sinusoidal current that would have to be injected into the PES to compensate the large adjustments to the position of the head that would be necessary to follow a particular data track as defined by the pre-written servo tracks.
The present invention addresses these and other problems, and offers other advantages over the prior art.
The present invention relates to repeatable runout (RRO) compensation of servo control systems used in disc drives and spin-stands. One embodiment of the invention is directed toward a servo control loop that includes compensation circuitry having a compensation signal that is generated based upon a compensation equation. The compensation signal represents RRO caused by eccentricity between pre-written servo tracks and an axis of rotation of a disc on which they are written. The compensation signal is injected into the servo control loop to compensate the RRO.
Another embodiment of the invention is directed toward a method of compensating RRO in a servo control loop that is related to eccentricity between pre-written servo tracks on a disc and a path followed by a head that is concentric with an axis of rotation of the disc. In the method a compensation equation is formed that represents the RRO. A compensation signal is generated based upon the compensation signal. The compensation signal is injected into the servo control loop to cancel the RRO and cause the head to follow a virtual track that is concentric with the axis of rotation of a disc.
The present invention relates to compensation of servo control systems used in disc drives and spin-stands for large repeatable runout (RRO). The large RRO results from pre-written servo tracks which define data tracks that are eccentric to an axis of rotation of the disc on which they are written. The present invention overcomes problems presented by the large RRO by compensating the servo control loop to control a transducing head to follow “virtual” tracks which coincide with the axis of rotation of the disc, but are eccentric to the “real” data tracks defined by the pre-written servo tracks. Consequently, the present invention allows a disc drive or a spin-stand to utilize discs having pre-written servo patterns, which can result in an increase in storage capacity and better testing of transducing heads and their supporting mechanisms.
Actuator assembly 110 is mounted to base plate 102 for rotation about a cartridge bearing assembly 112. Actuator assembly 110 is adapted to rotate in response to a control current supplied to coil 113 of voice coil motor 114. Actuator assembly 110 typically includes a plurality of rigid track accessing arms 116 which extend into the stack of discs 106, as shown in
Spin-stand 130 also includes a carriage 146 that moves between rails 148 and 150 in the “Y” direction as indicated by arrows 152. Similar to platform 134, carriage 146 can be supported by a cushion of air during movement and can be locked into position by applying a vacuum between carriage 146 and granite base 140. A position encoder 154 can be located, for example, along guide 150 to provide an indication of the position of carriage 146.
Carriage 146 and platform 134 both move using electromotive motors mounted between one of the guide rails and the respective platform or carriage. Other types of motors, such as a stepper motor, may be used in place of the electromotive motors. These motors generally perform coarse adjustment of a suspension assembly 118, which is connected to a suspension chuck 156 and supports a transducing head 120 proximate a surface of disc 106. In one embodiment, suspension chuck 156 is connected to piezo platform 158 through piezo elements that are able to move suspension chuck 156, generally in the “X” direction 142, to perform fine adjustment of transducing head 120 relative to disc 106.
During head loading operations, pivot motor 160 rotates eccentric cam 162 causing lever arm 164 and the back end of pivoting platform 166 to rotate upward about pivot pins 168 and 170. Carriage 146 can be moved forward so that transducing head 120, carried at the end of suspension assembly 118, moves under the spinning disc 106. Support platform 134 is also moved so that the head 120 is positioned at a desired radius along discs 106. When head 120 nears the desired location relative to discs 106, motor 160 rotates eccentric cam 162 back so that pivoting platform 166 returns to its level position and the head is brought into proximity with discs 106 so that head 120 can fly over the surface 110 of discs 106.
Head 120 on suspension assembly 118 is connected by electrical leads to printed circuit 172, which has further connections to control box 174. Control circuitry, which is either part of circuit 172 or contained in control box 174, is used to control the positioning of head 120 on suspension assembly 118. The control circuitry for spin-stand 130 can be adapted to move head 120 to a test track on disc 106 which data is to be read from or written to. Additionally, the position of head 120 can be adjusted by the control circuitry to move head 120 to a number of different locations within the test track during readback, so that a profile of head 120 can be determined. Additional circuitry can be used to control the tests that are performed by spin-stand 130, such as error-rate testing, pulse width-fifty testing, track average amplitude testing, and track scan testing, all of which are familiar to those skilled in the art.
One embodiment of suspension assembly 118, is shown in
Suspension assembly 118 generally includes load beam 176 and gimbal 178. Load beam 176 has a mounting portion 180 for connecting suspension assembly 118 to a track accessing arm 116 or suspension chuck 156. Flexible beam portion 182 applies a pre-load force to head 120 through rigid beam section 184 to limit the flying height of head 120. Flexible beam portion 182 can also include microactuators 186 and 188 to provide precise control to the position of head 120. In one embodiment, microactuators 186 and 188 are capable of contracting or expanding depending on a voltage applied by respective conducting lines 190, 192, 194, and 196 for fine control of the position of head 120. Microactuator 186 can contract while microactuator 188 expands to move head 120 in direction 198. Likewise, microactuator 188 can contract while microactuator 186 expands to move head 120 in direction 200. Alternative types and configurations of microactuators may be used along suspensions 118 and 194 as is understood by those skilled in the art. For example, multiple microactuators may be used within the same suspension assembly with their movement coordinated by the control circuitry for disc drive 100 and spin-stand 130.
Discs 106 used in disc drive 100 and spin-stand 130 include servo patterns which can be used to establish data tracks on disc 106 and control the position of head 120 relative to disc 106. The servo patterns are typically written to a surface of the disc 106 in a plurality of radially extending servo sectors 202, as shown in the portion of a disc 106 shown in
In addition, the servo information includes servo track identifying information in the form of an index sector 207 which can be used to determine a relative angular position of the servo track. Consequently, the servo information provides coarse position information in terms of a track number (radial position) and an index sector 207 (angular position). Additionally, the servo sectors 202 can provide fine position information using known patterns, such as a split-burst servo pattern or a null-type servo pattern to indicate the location of a head 120 relative to a center of a given data track 204.
A servo control loop provides control of the position of head 120 relative to servo tracks 204 using the servo information and can be configured to carry out two main types of servo operation: seeking and track following. During a typical seek, a head 120 is moved from an initial track to a destination track on the corresponding disc 106. A velocity profile is formulated indicative of a target velocity trajectory for the head 120, with current being applied to the coil 113 to first accelerate and then decelerate the head 120 toward the destination track in accordance with the velocity profile. To maintain the trajectory of the head 120, the current is successively adjusted in relation to the difference between the actual velocity and the target velocity of the head 120.
During a track following mode of operation, the head 120 is caused to follow a corresponding selected data track 204 on the disc 106. The servo information from the track being followed is periodically sampled and provided to a servo controller, which controls the actuator mechanisms used to control the position of head 120 in order to maintain head 120 in a desired relationship to the data track 204.
As disc 106 is rotated, head 120 of HDA 212 periodically samples servo information contained in the servo sectors 202 and produces an output signal in response thereto on path 218. The servo information (coarse and fine position information) contained in the output signal is demodulated by demodulator 214 and is presented as a head position signal on path 220. The head position signal is provided as an input to summing junction 216, which also receives a reference signal relating to a data track number from path 222 that is indicative of a desired position of head 120. Summing junction 216 compares the reference signal to the head position signal and produces a position error signal (PES) on path 224. The PES relates to a correction in the position of head 120 relative to data tracks 204 that is required to position the head 120 in accordance with location indicated by the reference signal. The PES is provided to servo controller 210, which responds by adjusting a control signal that is provided to HDA 212 along path 226. The control signal causes the actuator mechanisms of HDA 212 to adjust the position of head 120 toward the desired position.
Traditionally, servo sectors 202 (
Unlike the prior art, the present invention focuses on compensation of RRO in a disc drive or spin-stand that is caused by the use of discs 106 having servo patterns 202 which were written on the discs 106 prior to their installation in a disc drive 100 or spin-stand 130. These “pre-written” servo patterns or sectors 202 make track-following operations more difficult due to substantial eccentricity between the “real” data tracks defined by the servo patterns and a circular path that a head follows. The present invention does not attempt to compensate the RRO to allow the servo control loop to better perform track- following operations. Rather, the compensation (or cancellation) of this large RRO is made to allow a head to follow “virtual” tracks, which are eccentric to servo tracks 204 while being substantially concentric with the axis of rotation of the disc 106 on which they are written.
As mentioned above, the present invention solves the above-described misalignment problem by establishing “virtual” tracks 234 (only one shown), which are substantially concentrically aligned with the circular path 228 and axis of rotation 232 of disc 106, as illustrated in
To facilitate an understanding of the present invention,
In the embodiment depicted in
The compensation signal is a periodic signal that represents the RRO and has a period relating to integer multiples of the time for one revolution of disc 106. In its basic form, the compensation signal has a period equal to the time for one revolution of disc 106. However, higher frequency components of the compensation signal can be included as well. The amplitude of the compensation signal varies with the angular position and relates to the radial position difference Δr between circular path 228 of head 120 and a reference data track 204 as defined by the pre-written servo information, as shown in
In one embodiment of the invention, the compensation signal is based upon a compensation equation, designated as C, that comprises discrete compensation values set as the radial position difference Δr measured at each servo sector 202, as shown in Equation 1. The subscript k represents the sector index 207 and N represents the number of sectors 202. The reference data track 204 from which the radial position difference Δr is measured is preferably selected such that the compensation values represent only the RRO rather than the RRO plus a constant offset value. The resulting compensation equation can then be represented as a purely sinusoidal equation having only an periodic or AC component while lacking a constant or DC component. If desired, the values of the compensation equation between adjacent servo sectors can be obtained using known interpolation techniques.
The compensation equation is preferably stored in memory of disc drive 100 or spin-stand 130. The embodiment of the compensation equation represented in Equation 1 is preferably stored as a look-up table in memory where the compensation values Δr are indexed according to their corresponding servo track 202. For disc drive 100 the memory used to store the compensation equation is preferably flash memory, which can be accessed during power on 20 conditions. In spin-stand 130, the memory used to store the compensation equation can be part of the control circuitry.
The establishment of virtual tracks 234 on disc 106 also requires that a reference virtual track be established from which the other virtual tracks 234 are displaced. For example, the reference virtual track could be selected as a virtual track zero that is positioned adjacent inner diameter ID of disc 106 (
The general method for establishing the compensation values Δr used to form the compensation equation is illustrated in the flowchart of
As discussed above with reference to
Disc drive 100, shown in FIGS. 1 and 1.1, typically includes a stack of discs 106, all of which are mounted to spindle 104. Each of the discs 106 includes the above-described pre-written servo tracks 204 and one or two corresponding heads 120 that are adapted to perform reading and writing operations on their respective disc 106. Each of the heads 120 are mounted to actuator assembly 110, as shown in
It is desirable to configure disc drive 100 to operate in a “cylinder” mode where respective virtual tracks of each head are vertically aligned with each other to increase switching efficiency and performance. An example of disc drive 100 operating in a cylinder mode will be described with reference to
One embodiment of the present invention is directed to a method of correlating the virtual tracks associated with each head/disc combination of disc drive 100 to facilitate operating disc drive 100 in a cylinder mode. This can be accomplished using the method illustrated in
Since each disc 106 of a disc drive 100 is mounted to spindle 104 after the servo sectors 202 have been written, the angular position of the index sectors 207 of the discs 106 will be misaligned. This can be taken into account by establishing the relative angular positions of the index sectors 207 for each disc 106 of disc drive 100 with respect to a reference location or index sector. This can be desirable to establish the proper timing for writing to the surfaces of discs 106 to avoid writing data in the wrong location within a virtual data track when switching between heads 120.
In summary, the present invention relates to repeatable runout (RRO) compensation of servo control systems used in disc drives 100 and spin-stands 130. One embodiment of the invention is directed toward a servo control loop 236 that includes compensation circuitry 238 having a compensation signal that is generated based upon a compensation equation. The compensation signal represents RRO caused by eccentricity between pre-written servo tracks 220 and an axis of rotation 232 of a disc 106 on which they are written. The compensation signal is injected into the servo control loop 236 to compensate the RRO.
Another embodiment of the invention is directed toward a method of compensating RRO in a servo control loop 236 that is related to eccentricity between pre-written servo tracks 204 on a disc 106 and a path 228 followed by a head 120 that is concentric with an axis of rotation 232 of the disc 106. In the method, shown in
It is to be understood that even though numerous characteristics and advantages of various embodiments of the invention have been set forth in the foregoing description, together with details of the structure and function of various embodiments of the invention, this disclosure is illustrative only, and changes may be made in detail, especially in matters of structure and arrangement of parts within the principles of the present invention to the full extent indicated by the broad general meaning of the terms in which the appended claims are expressed. For example, the particular elements may vary depending on the particular application for the various embodiments of the invention while maintaining substantially the same functionality without departing from the scope and spirit of the present invention. Furthermore, additional features and benefits will be made apparent in view of the figures.
This application claims the benefit of U.S. Provisional Patent Application No. 60/170,240, entitled “VIRTUAL TRACKS FOR REPEATABLE RUNOUT (RRO) MANAGEMENT,” filed on Dec. 10, 1999, and U.S. Provisional Patent Application No. 60/198,166, entitled “ECCENTRIC SERVO TRACK REFERENCING,” filed on Apr. 17, 2000.
Number | Name | Date | Kind |
---|---|---|---|
3725764 | Oswald | Apr 1973 | A |
3863124 | Pierce et al. | Jan 1975 | A |
3914541 | Elliott | Oct 1975 | A |
4030132 | Iftikar et al. | Jun 1977 | A |
4103314 | Case | Jul 1978 | A |
4135217 | Jacques et al. | Jan 1979 | A |
4149199 | Chick et al. | Apr 1979 | A |
4217612 | Matla et al. | Aug 1980 | A |
4314295 | Frandsen | Feb 1982 | A |
4329712 | Lang | May 1982 | A |
4355266 | Pearson | Oct 1982 | A |
4371960 | Kroiss | Feb 1983 | A |
4396961 | Prasad et al. | Aug 1983 | A |
4414589 | Oliver et al. | Nov 1983 | A |
4456934 | Wedman et al. | Jun 1984 | A |
4485418 | Bremmer | Nov 1984 | A |
4497047 | Fujiie et al. | Jan 1985 | A |
4513333 | Young et al. | Apr 1985 | A |
4524397 | Chalmers et al. | Jun 1985 | A |
4562494 | Bond | Dec 1985 | A |
4575776 | Stephens et al. | Mar 1986 | A |
4605977 | Matthews | Aug 1986 | A |
4616276 | Workman | Oct 1986 | A |
4620244 | Krause | Oct 1986 | A |
4620252 | Bauck et al. | Oct 1986 | A |
4633345 | Keener | Dec 1986 | A |
4636885 | Yamada et al. | Jan 1987 | A |
4677602 | Okano et al. | Jun 1987 | A |
4679103 | Workman | Jul 1987 | A |
4697127 | Stich et al. | Sep 1987 | A |
4697213 | Kitamura | Sep 1987 | A |
4706250 | Patel | Nov 1987 | A |
4727533 | Erbert | Feb 1988 | A |
4764860 | Takao | Aug 1988 | A |
4786990 | Overton et al. | Nov 1988 | A |
4788608 | Tsujisawa | Nov 1988 | A |
4791599 | Hethuin et al. | Dec 1988 | A |
4803572 | Haruna et al. | Feb 1989 | A |
4816938 | Cowen et al. | Mar 1989 | A |
4822139 | Yoshizumi | Apr 1989 | A |
4878135 | Makino et al. | Oct 1989 | A |
4890172 | Watt et al. | Dec 1989 | A |
4897840 | Weiss et al. | Jan 1990 | A |
4924165 | Kohno | May 1990 | A |
4947272 | Yokozawa | Aug 1990 | A |
4956831 | Sarraf et al. | Sep 1990 | A |
4965782 | Mathews | Oct 1990 | A |
5046060 | Chow et al. | Sep 1991 | A |
5055731 | Nihei et al. | Oct 1991 | A |
5056074 | Tateishi et al. | Oct 1991 | A |
5062023 | Squire | Oct 1991 | A |
5073885 | Ito et al. | Dec 1991 | A |
5081552 | Glaser et al. | Jan 1992 | A |
5089757 | Wilson | Feb 1992 | A |
5122718 | Sawata | Jun 1992 | A |
5146372 | Cronch et al. | Sep 1992 | A |
5155422 | Sidman et al. | Oct 1992 | A |
5161077 | Jabbari | Nov 1992 | A |
5164863 | Janz | Nov 1992 | A |
5185681 | Volz et al. | Feb 1993 | A |
5187620 | Notake et al. | Feb 1993 | A |
5189578 | Mori et al. | Feb 1993 | A |
5197058 | Bell, Jr. et al. | Mar 1993 | A |
5198948 | Stover et al. | Mar 1993 | A |
5204793 | Plonczak | Apr 1993 | A |
5216559 | Springer | Jun 1993 | A |
5233487 | Christensen et al. | Aug 1993 | A |
5241433 | Anderson et al. | Aug 1993 | A |
5247501 | Hashimoto et al. | Sep 1993 | A |
5257149 | Meyer | Oct 1993 | A |
5270885 | Satoh et al. | Dec 1993 | A |
5274511 | Ikeda | Dec 1993 | A |
5287225 | Sukigara | Feb 1994 | A |
5287234 | Suzuki | Feb 1994 | A |
5299026 | Vincett et al. | Mar 1994 | A |
5303105 | Jorgenson | Apr 1994 | A |
5305160 | Funches et al. | Apr 1994 | A |
5311378 | Williams et al. | May 1994 | A |
5367513 | Bates et al. | Nov 1994 | A |
5379171 | Morehouse et al. | Jan 1995 | A |
5400201 | Pederson | Mar 1995 | A |
5404253 | Painter | Apr 1995 | A |
5416658 | Sega et al. | May 1995 | A |
5444582 | Suzuki | Aug 1995 | A |
5444583 | Ehrlich et al. | Aug 1995 | A |
5455724 | Suzuki et al. | Oct 1995 | A |
5465182 | Ishikawa | Nov 1995 | A |
5465183 | Hattori | Nov 1995 | A |
5521773 | Suzuki et al. | May 1996 | A |
5521778 | Boutaghou et al. | May 1996 | A |
5523902 | Pederson | Jun 1996 | A |
5535072 | Witt et al. | Jul 1996 | A |
5539714 | Andres, Jr. et al. | Jul 1996 | A |
5541784 | Cribbs et al. | Jul 1996 | A |
5550685 | Drouin | Aug 1996 | A |
5553086 | Sompel et al. | Sep 1996 | A |
5574354 | Kohchi | Nov 1996 | A |
5576909 | Dierkes et al. | Nov 1996 | A |
5585976 | Pham | Dec 1996 | A |
5602689 | Kadlec et al. | Feb 1997 | A |
5608586 | Sri-Jayantha et al. | Mar 1997 | A |
5610487 | Hutsell | Mar 1997 | A |
5610777 | Dang et al. | Mar 1997 | A |
5617388 | Ishioka et al. | Apr 1997 | A |
5638230 | Kadlec | Jun 1997 | A |
5646797 | Kadlec et al. | Jul 1997 | A |
5648738 | Welland et al. | Jul 1997 | A |
5675450 | Kadlec | Oct 1997 | A |
5677809 | Kadlec | Oct 1997 | A |
5680272 | Kadlec et al. | Oct 1997 | A |
5684650 | Kadlec et al. | Nov 1997 | A |
5706265 | Bang | Jan 1998 | A |
5708581 | Martinez | Jan 1998 | A |
5774294 | Fioravanti | Jun 1998 | A |
5774297 | Hampshire et al. | Jun 1998 | A |
5777816 | Hampshire et al. | Jul 1998 | A |
5793559 | Shepherd et al. | Aug 1998 | A |
5796535 | Tuttle et al. | Aug 1998 | A |
5796542 | Szeremeta | Aug 1998 | A |
5815332 | Suzuki et al. | Sep 1998 | A |
5822147 | Kisaka | Oct 1998 | A |
5825578 | Shrinkle et al. | Oct 1998 | A |
5826338 | Chilton et al. | Oct 1998 | A |
5828515 | Kim | Oct 1998 | A |
5835300 | Murphy et al. | Nov 1998 | A |
5835302 | Funches et al. | Nov 1998 | A |
5844743 | Funches | Dec 1998 | A |
5854722 | Cunningham et al. | Dec 1998 | A |
5883749 | Park | Mar 1999 | A |
5886846 | Pham et al. | Mar 1999 | A |
5898286 | Clare et al. | Apr 1999 | A |
5926338 | Jeon et al. | Jul 1999 | A |
5940239 | Lee et al. | Aug 1999 | A |
5940240 | Kupferman | Aug 1999 | A |
5949605 | Lee et al. | Sep 1999 | A |
5949608 | Hunter | Sep 1999 | A |
5956201 | Pham et al. | Sep 1999 | A |
5969494 | Kang | Oct 1999 | A |
5978169 | Woods | Nov 1999 | A |
6069764 | Morris et al. | May 2000 | A |
6097565 | Sri-Jayantha et al. | Aug 2000 | A |
6115203 | Ho et al. | Sep 2000 | A |
6128153 | Hasegawa et al. | Oct 2000 | A |
6130797 | Akagi et al. | Oct 2000 | A |
6141175 | Nazarian et al. | Oct 2000 | A |
6166875 | Ueno et al. | Dec 2000 | A |
6310742 | Nazarian et al. | Oct 2001 | B1 |
Number | Date | Country |
---|---|---|
3900683 | Jan 1989 | DE |
197 15 678 | Oct 1997 | DE |
0 130 248 | Jan 1985 | EP |
0 540 114 | May 1993 | EP |
0 549 814 | Jul 1993 | EP |
2 060 217 | Apr 1981 | GB |
1713268 | Mar 1991 | GB |
WO 9106096 | May 1991 | WO |
WO 9306595 | Apr 1993 | WO |
WO 9745833 | Dec 1997 | WO |
Number | Date | Country | |
---|---|---|---|
60170240 | Dec 1999 | US | |
60198166 | Apr 2000 | US |