Patent Document

This is a divisional of application Ser. No. 09/295,696, filed Apr. 21, 1999 now U.S. Pat. No. 6,174,218. 
    
    
     BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     The present invention relates to an apparatus and method for the manufacture of sliders used in magnetic storage devices. More particularly, the invention relates to an improved system for controlling the amount of non-linear deformation in wafer quadrants of slider rows during lapping in manufacturing. 
     2. Description of the Background Art 
     Digital magnetic disk drives are one very widely used type of storage device today. Such drives employ head-mounted magnetic transducers to read and write data on rotating disk media. The operable portion of such a transducer head is called a “slider,” and the key operational portion of a slider is a transducing gap between pole elements. It is the characteristics of this gap, which to a large degree, determine the performance of the slider, and ultimately its suitability for use in a disk drive. 
     Most dimensions of a slider&#39;s gap are dictated by the semiconductor-type fabrication processes used, and are therefore generally not a problem, since such processes can be very precise. A critical exception, however, is the depth of the gap, termed “stripe-height” for magneto-resistive heads (the present discussion also may apply to inductive heads, where the usual term used is “throat height”). The stripe height is achieved by abrasively removing material in a lapping step during manufacturing. 
     Problems arise with regard to the stripe height because sliders are typically manufactured together in batches. A number of such rows of sliders are deposited together onto a single semiconductor-type wafer, which is then cut into pieces commonly termed “wafer quadrants” (or just “quadrants”). A wafer quadrant is bonded onto an extender tool (also sometimes known as a row tool, transfer tool, or support bar) and the foremost slider row is lapped as a unit on an abrasive surface, such as a plate coated with an appropriate slurry mix. The slider row is then cut from the wafer quadrant, so that lapping of a new foremost slider row may commence. The sliced off row of sliders is ready for additional manufacturing steps, dicing into individual sliders, and then the final steps which ultimately produce working disk drive heads. 
     Unfortunately, lapping of a slider row as a unit can produce variation in the various slider&#39;s stripe heights. For example, even if a slider row is perfectly linear, it needs to be lapped in true parallel against the lapping surface, or sliders at one end of the row will be lapped differently than those at the opposite end. This is commonly referred to as “balance,” and it is a problem which the industry has long appreciated and has generally developed adequate methods to correct. 
     Of present interest is where the foremost slider row in a wafer quadrant is not linear. The stresses inherent in wafer material and in the operations of lapping and slicing can all produce varying degrees of concave, convex, and higher order curvatures. This non-linear deformation is commonly termed “row bow” (although the term “bow” is often an understatement of the actual non-linearity which may be present). If such nonlinearity is not corrected before lapping, and preferably also dynamically during lapping, the individual sliders within a row will have different amounts of material lapped away, i.e. end with different stripe heights. 
     Various systems for the correction of such bow have been tried. U.S. Pat. No. 4,457,114 discloses a carrier having a support bar to which a slider row workpiece is bonded. The support bar is connected to a base portion of the carrier by a central stem portion and thermal expansion is used between opposite ends of the support bar and the base to control the shape of the support bar. To get a range in shape from convex to flat to concave, the support bar may be made to be convex when cool. 
     U.S. Pat No. 5,117,589 discloses a transfer tool having a longitudinal slot or chamber in which a piezoelectric actuator or screw is present to control the shape of the transfer tool. To get a range in shapes, this transfer tool may also be convex when the actuator is off. 
     U.S. Pat No. 5,203,119 discloses a transfer tool secured in a bow yoke holder. The transfer tool has a single central slot in which the end of a piston is captured. Upward movement of the piston causes the transfer tool to assume a convex shape, and downward action of the piston produces a concave shape. 
     U.S. Pat. No. 4,914,868 discloses a holder having an elongated longitudinal slot which defines a beam portion of the holder. An actuator applies pressure in the middle of the beam to deflect it in a manner producing a quadratic curvature. Separate actuators at either end of the holder are used to control balance. 
     U.S. Pat. No. 5,525,091 discloses a transfer tool which has an elongated longitudinal slot defining a beam. Actuators (of undefined nature, but implicitly electrically operated) are used to controllably press three pins against the beam such that the shape of a slider row bonded to the transfer tool is changed. 
     U.S. Pat. No. 5,607,340 discloses a row tool having a series of bend openings and stress relief openings. The openings are all disclosed as being generally quite proximate to the edge of the row tool to which a slider row is bonded. Related U.S. Pat. No. 5,620,356 by the same inventors discloses the system for operating this row tool. A pair of electromagnetic actuators are used to apply balance pressure and a set of three other electromagnetic actuators are used to apply rotational twist to the bend openings in the row tool. The noted structure and location of the openings dictates that the application of rotational twist is also proximate to the edge of the row tool where a slider row is bonded. 
     The last example presented above represents the most sophisticated prior art known to the inventors, but even it has severe limitations. Such limitations particularly include the intricate complexity of the row tool&#39;s shape, due to the number and placement of the openings, and the high difficulty of controlling all of the forces which must be applied together in concert to effect bow correction. Viewed as a vector sum, the use of rotational twist is effectively a simultaneous application of force in a direction normal to the lapping surface, along with lateral force. The normal forces applied from the three twist actuators can thus combine with the desired normal forces applied by the two balance actuators such that controlling the net forces throughout is quite difficult. 
     It is, therefore, an object of the present invention to provide an improved method, and apparatus for use of that method, for lapping sliders. Other objects and advantages will become apparent from the following disclosure. 
     SUMMARY OF THE INVENTION 
     The present invention relates to an apparatus and method for controlling the amount of row bow during lapping in the manufacture of sliders, and thus particularly controlling the stripe heights of individual sliders as material is lapped away. The method comprises: (i) bonding the wafer quadrant of slider rows onto an extender tool; (ii) mounting the extender tool in a carrier assembly; (iii) positioning the carrier assembly to bring the foremost slider row into contact with the lapping surface; and then compensating for non-linearity during lapping by: (iv) adjustably applying pressure to the carrier assembly; and (v) distorting the extender tool artificially with at least one force laterally applied to the extender tool such that it changes the profile of the foremost slider row in the wafer quadrant. 
     The apparatus is used to effectuate the method and includes: (i) an extender tool, to which the wafer quadrant of slider rows is bonded; (ii) a carrier assembly including a base and cover which are suitable for mounting and holding the extender tool bolted between them, wherein the carrier assembly is mountable in a generally conventional lapping system; and (iii) an actuator mechanism suitable for applying at least one lateral force to the extender tool as lapping operations commence and proceed. 
     A more thorough disclosure of the present invention is presented in the detailed description which follows and in the accompanying figures. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     The objects, advantages and features of the present invention will be more clearly understood by reference to the following detailed disclosure and the accompanying drawings in which: 
     FIG. 1 is a partially exploded view depicting the major elements of the invention; 
     FIG. 2 is a plan view of the extender tool portion of the invention with a wafer quadrant workpiece bonded to it; 
     FIG. 3 is a graphical depiction of four particular forms of row bow distortion which the invention can be used to correct; 
     FIG. 4 is a partially exploded view of the carrier cover of the invention removed from a carrier base and actuator with a mounted extender tool; 
     FIG. 5 is a rotated version of the view presented in FIG. 4, better showing other features of the invention; 
     FIG. 6 is a perspective view of the carrier cover portion of the invention without the probe assembly installed; and 
     FIG. 7 is a cross section view of the actuator portion of the invention, taken along axis  1 - 1  of FIG.  1 . 
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     The present invention relates to an improved apparatus and method for bow compensation during the manufacture of sliders. As illustrated in the various drawings herein, and particularly in the view of FIG. 1, a preferred embodiment of the inventive apparatus is depicted by the general reference character  10 . 
     FIG. 1 depicts key elements of the inventive lapping tool  10  in a partially exploded view. Therein is shown a carrier assembly  12  having a carrier base  14 , a carrier cover  16 , and an extender tool  18 . In this view, the carrier base  14  has an actuator  20  already mounted onto it, the carrier cover  16  has a probe assembly  22  already mounted into it, and the extender tool  18  has a wafer quadrant  24  bonded to it. The wafer quadrant  24  is a “quad” of slider rows which constitute the workpiece upon which lapping is to occur, e.g., a block of thirty slider rows with forty-four MR type sliders in each. Other than the carrier assembly  12 , the lapping tool  10  may be generally conventional in nature and such portions are therefore not shown. 
     FIG. 2 depicts the extender tool  18  in plan view with a bonded wafer quadrant  24  (shown in ghost outline). With reference to the orientation used in FIG. 2 the edges may be termed: an actuated edge  26 , which in lapping may also be thought of as upward or backward most; a bonding edge  28 , which is bottom or forward during lapping; a left edge  30 ; and also a right edge  32 . At the lowest end of the wafer quadrant  24  is a working edge  34 , so termed because it constitutes the surface of the foremost slider row which is to be lapped. 
     A first L-slot  36  is provided toward the left edge  30  of the extender tool  18  and a second such L-slot  36  (reverse L-shaped) is provided toward the right edge  32 . The use of an L-shape is currently preferred by the inventors, but is not a limitation. The regions between the left edge  30  and right edge  32  and the respective L-slots  36  define extender arms  40 . Each such extender arm  40  includes an arm slot  44 , toward the actuated edge  26 . The region between the bonding edge  28  and the bottoms of both of the L-slots  36  forms a beam  48 . 
     FIG. 2 also portrays the primary forces which may be intentionally applied to the extender tool  18 . A left balance force  52  and a right balance force  54  are each depicted by single-arrowed vertical lines. A potentially bi-directional left side lateral force  56  and a similar bi-directional right side lateral force  58  are depicted by dual-arrowed horizontal lines. 
     The balance forces  52 ,  54  are typically provided by the apparatus holding the carrier assembly  12 , by pistons which bear down on it. This is largely the conventional manner used today with existing carrier assemblies and extender tools, although single and triple piston and balance force systems are also known. 
     In contrast, a novel departure from conventional technique here is the use of the lateral forces  56 ,  58 . A left or right lateral application of force to either of the arm slots  44  causes a bending moment to be transferred from the respective extender arm  40  into the beam  48 . The present invention makes controlled use of all of these forces  52 ,  54 ,  56 ,  58  in concert to correct for distortion at the working edge  34  of the wafer quadrant  24 , i.e., in the foremost slider row. 
     FIG. 3 is a graphical depiction of four particular forms of row distortion which the invention can be used to substantially reduce or eliminate. The working edge  34  of the wafer quadrant  24  is shown here merely as a graph line. Positive quadratic distortion, or convex row bow, is represented by line  60  and negative quadratic distortion, or concave row bow, is represented by line  62 . Represented by line  64  and line  66  are two opposite states of higher frequency waveform distortion commonly referred to as “S” shape row bow. In FIG. 3, line  60  is intentionally depicted as an asymmetrical convex distortion to emphasize that even such non-linearities (which are more than mere simple bow) may occur and be corrected using the inventive lapping tool  10 . 
     Correcting for these types of distortion is particularly difficult because of the need to integrate the compensation state, the magnitude of compensation, and the balance. The net mechanical actions are often in the same direction, downward, and thus in competition with each other. In the present invention, the balance forces  52 ,  54  and the lateral forces  56 ,  58  must still be dealt with simultaneously, but they are applied separately, in purely normal and purely lateral directions initially, and this simplifies control of their application. 
     FIG. 4 is a partially exploded view showing the extender tool  18  mounted on the carrier base  14  and engaged with the actuator  20  before the carrier cover  16  has been mounted and bolts (not shown) used to secure all together. An actuator arm  72  extending from each side of the actuator  20  engages each of the arm slots  44  in the extender tool  18 . When suitably engaged in this manner, the lateral forces  56 ,  58  are transferred into the arm slots  44  and onward to the beam  48  and any bonded wafer quadrant  24 . 
     In FIG. 4 the wafer quadrant  24  which is bonded to the extender tool  18  is shown as smaller than that in FIG. 1, depicting that a number of slider rows have already been lapped and removed from it. It should be appreciated that as individual slider rows are removed, the extender tool  18  is brought forward almost the entire length of the wafer quadrant  24  along a receiving surface  70  (FIG. 1) on the carrier base  14 . Since the extender tool  18  is bolted against the receiving surface  70 , in the preferred embodiment, it has been one of the inventors&#39; particular observations that the receiving surface  70  needs be particularly flat for this purpose, as well as for stabilizing the extender tool  18  and its bonded wafer quadrant  24  for consistent operation of the probe assembly  22  (discussed presently). 
     To mate the carrier base  14  to the carrier cover  16  in precise relationship a peg-in-hole system is used. The carrier base  14  includes holes  74  in side members  76  which are engaged by pegs  78  (see also FIG. 5) in the carrier cover  16 . 
     In the preferred embodiment the side members  76  each also have appropriate top surfaces  80  to receive downward pressure from balance pistons (not shown) and bottom surfaces  82  to receive upward pressure from retracting springs (not shown; also sometimes called ejecting springs in the industry). As has previously been noted, such pistons and springs are conventional parts of the overall lapping apparatus used. 
     FIG. 5 is a rotated view of FIG. 4, better showing other features of the invention. The probe assembly  22  is a film cable having at its bottom edge  86  a series of probe pads  84  which are each connected with electrical conductors  88  that go back to a lapping system control system. The probe pads  84  are conductive surfaces which respectively engage with conventional slider row electronic lapping guide (ELG) contacts. Such ELG contacts are typically provided in each slider row, including those in the foremost row, which will be present at the working edge  34  of the wafer quadrant  24 . 
     This view also illustrates how the actuator  20  is slidably mounted to the rest of the carrier assembly  12 . The carrier base  14  includes a dovetail rail  90  and the actuator  20  includes a suitable pinch mechanism  92  to engage the dovetail. The pinch mechanism  92  is operated by a lever  94  to compressably lock the actuator  20  onto place on the rail  90 . FIG. 6 depicts the carrier cover  16  without the probe assembly  22  installed. As can be particularly appreciated in this view, the carrier cover  16  includes a probe clamp spring  102  and a quad clamp spring  104 . The probe clamp spring  102  has a plurality of fingers  106  which are provided in sufficient number and which are suitably positioned to tend to force the probe pads  84  (FIG. 5) into electrical contact with all of the ELG contacts of the foremost slider row. The quad clamp spring  104  also has a plurality of fingers  108  (not necessarily the same in number as those of the probe clamp spring  102 ) which apply force through the flexible medium of the probe assembly  22  and against the wafer quadrant  24 . This force holds the bonded extender tool  18  and wafer quadrant  24  against the receiving surface  70  of the carrier base  14  (FIG.  1 ). 
     The inventors have particularly observed that the design and use of the probe clamp spring  102  and the quad clamp spring  104  are important. The pressure applied by the probe clamp spring  102  needs to be just sufficient that adequate electrical contact is made with the ELG contacts. Despite the seeming stiffness of the material of the wafer quadrant  24 , even very minor pressure on the wafer quadrant  24  may be manifested as deformation which can adversely affect lapping. The pressure applied by the quad clamp spring  104  also needs to be just sufficient that the wafer quadrant  24  is pressed against the receiving surface  70  of the carrier base  14  (through the flexible cable of the probe assembly  22 ). Excessive pressure by the quad clamp spring  104  can interfere with reliable operation of the probe clamp spring  102  and the ELG contacts, as well as contributing to undesirable deformation at the working edge  34  of the wafer quadrant  24 . Accordingly, any undue spring pressure is undesirable. 
     FIG. 7 is a cut away view of the actuator  20 , as taken through section  1 — 1  of FIG.  1 . The actuator  20  has an actuator body  112  that includes two piston chambers  114 . These each house an actuator piston  116  which has a forward extending piston rod  118 . The piston rods  118  each pivotally connect to an arm body  120  that is itself pivotally mounted on pivot pins  122  which are fixed in the actuator body  112 . Each actuator arm  72  may then independently exhibit pivotal movement, depicted by arcs  124 , when an associated actuator piston  116  and piston rod  118  are moved forward or backward. 
     For pneumatic operation, access to each piston chamber  114  is provided by a positive pressure port  126  and a negative pressure port  128 . When a net pressure is applied which is greater at a positive pressure port  126  than it is at an associated negative pressure port  128 , the actuator piston  116  in the associated piston chamber  114  is moved forward and the associated actuator arm  72  is forced toward the outside. Conversely, when the net pressure is greatest at a negative pressure port  128 , the associated actuator arm  72  is forced inward. 
     Many other suitable means, beside pneumatic piston operation, may be used for moving the actuator arms  72 , and the method described above for this discussion should not be interpreted as restricting the true scope of the present invention. Some other examples, without limitation, include pneumatically operated bellows, hydraulically operated pistons or bellows, piezoelectric positioners, electromagnetic positioners, and thermal expansion positioners. 
     With particular reference now to FIG.  2  and FIG. 3, the preferred embodiment can be used to compensate for row bow as follows. First, a new wafer quadrant  24  is bonded to the extender tool  18  and this assembly is mounted in the carrier assembly  12 , creating the inventive lapping tool  10  for use in an otherwise generally common lapping system (not shown). For purposes of this example, assume that the uncompensated new wafer quadrant  24  has the quadratic curvature depicted by line  64  in FIG.  3 . As lapping commences at the working edge  34  of the wafer quadrant  24 , the controller in the lapping system monitors the ELGs for the foremost slider row as lapping away of some wafer material occurs, and is then able to determine that the quadratic curvature of line  64  is in fact present. 
     If compensation is not undertaken, many sliders in the left half of the slider row in this scenario are about to be under lapped, i.e., end up with excessive stripe height, and many sliders in the right half of the slider row are about to be over lapped, i.e., end up with less than optimal stripe height. Accordingly, the controller will attempt to direct compensation of the distortion present in a manner to achieve the highest yield and quality of sliders in the current foremost row. Up to this point, the method employed has been essentially a conventional one used in the industry. 
     However, using the inventive lapping tool  10 , the controller of the underlying lapping system is now able to more efficiently and effectively compensate for the non-linear distortion condition than would be the case using conventional lapping tools. In response to the condition in the left half of the working edge  34 , the controller directs appropriate pneumatic pressure to the pressure ports  126 ,  128  (FIG. 7) of the actuator  20 , causing the actuator piston  116  in that side to pivot the associated actuator arm  72  rightward. Due to the engagement of the actuator arm  72  in the arm slot  44  of the extender tool  18 , the left side extender arm  40  is forced rightward, and acts as a lever to bend the left half of the beam  48 . This produces a flattening in the left half of the working edge  34 . 
     In this example, based on line  64  in FIG. 3, the condition opposite that above must be compensated for in the right half of the working edge  34 . Therefore, the right side components of the actuator  20  and the extender tool  18  are simply used in an opposite manner, and the right half of the working edge  34  is flattened. 
     Addressing the other possible examples which FIG. 3 suggests should now be clear. Reversing all of the steps above will correct for quadratic curvature like that of line  66 . Forcing the extender arms  40  both outward will bend the beam  48  in a manner that corrects for the convex bow of line  60  and forcing both extender arms  40  inward corrects for the concave bow of line  62 . 
     Finally, the controller can actively continue monitoring the ELGs as lapping progresses, and dynamically apply appropriate pneumatic pressure to the pressure ports  126 ,  128  to compensate for slider row bow so that consistent and desired throat or stripe heights are obtained. 
     Although this invention has been described with respect to specific embodiments, the details thereof are not to be construed as limitations, for it will be apparent that various embodiments, changes and modifications may be resorted to without departing from the spirit and scope thereof; and it is understood that such equivalent embodiments are intended to be included within the scope of this invention.

Technology Category: 7