Method of fabricating a base plate for piezo actuation
10367135 ยท 2019-07-30
Assignee
Inventors
- David Django Dexter (Goleta, CA, US)
- Damon Douglas Brink (Ventura, CA, US)
- Ryan J. Schmidt (Santa Barbara, CA, US)
Cpc classification
B21D28/10
PERFORMING OPERATIONS; TRANSPORTING
Y10T83/0448
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
G11B5/4873
PHYSICS
G11B21/10
PHYSICS
International classification
B21D28/10
PERFORMING OPERATIONS; TRANSPORTING
G11B21/10
PHYSICS
Abstract
A method of fabricating a base plate for piezoelectric actuation, comprises providing a plate having a major surface, striking a first removable portion of the plate in a first direction substantially normal to the major surface to shear the first removable portion relative to the plate by a shear distance that is less than the plate thickness. Striking the first removable portion in a second direction substantially opposite the first direction to reduce the shear distance by a reduction in shear that is less than the plate thickness. Leaving it the first removable portion in place rather than removing. Alternately, the removable portion may be created by lancing one or more portions spanning at least one opening through a base plate adjacent a first side of at least one opening and adjacent a second side of the at least one opening.
Claims
1. A method of fabricating a base plate for a head suspension assembly that prevents interlocking of multiple base plates when packaged together and adds structural integrity during shipping, the method comprising: providing a plate; creating at least one opening through the plate, the plate including a first spanning portion that extends from a first side of the at least one opening to a second side of the at least one opening; lancing the first spanning portion adjacent the first side and adjacent the second side, so that the first spanning portion becomes removable by a reduced shear force where lanced; leaving the first spanning portion in place; packaging base plates with the first spanning portion in place for shipping to a destination; and removing the first spanning portion from each base plate upon receipt at the destination.
2. The method of claim 1, wherein lancing comprises striking a first surface of the first spanning portion with a lancing punch along a first cleavage boundary that is adjacent the first side and along a second cleavage boundary that is adjacent the second side.
3. The method of claim 2, wherein lancing comprises striking a second surface of the first spanning portion with a lancing punch along the first cleavage boundary and along the second cleavage boundary, the second surface of the first spanning portion being opposite the first surface of the first spanning portion.
4. The method of claim 1, wherein the plate further comprises a second spanning portion that extends from the first side to the second side, and further comprising: lancing the second spanning portion adjacent the first side and adjacent the second side, so that the second spanning portion becomes removable by a reduced shear force where lanced; and leaving the second spanning portion in place rather than removing the second spanning portion.
5. The method of claim 1, wherein the first spanning portion comprises at least a portion of a first edge of the plate such that the at least one opening is not completely enclosed by the plate without the first spanning portion.
6. The method of claim 1, further comprising: creating a second opening separate from the at least one opening.
7. The method of claim 6, wherein the first spanning portion is disposed between the at least one opening and the second opening.
8. The method of claim 4, wherein the first spanning portion comprises at least a portion of a first edge of the plate such that the at least one opening is not completely enclosed by the plate without the first spanning portion and the second spanning portion comprises at least a portion of a second edge of the plate such that a second opening through the plate is not completely enclosed by the plate without the second spanning portion.
9. The method of claim 4, wherein the first spanning portion comprises at least a portion of a first edge of the plate such that the at least one opening is not completely enclosed by the plate without the first spanning portion and the second spanning portion comprises at least a portion of a second edge of the plate such that the at least one opening through the plate is not completely enclosed by the plate without the second spanning portion.
10. The method of claim 1, further comprising: removing a portion of the base plate to form a swage opening for connecting the baseplate to an actuator arm via a swaging operation.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The exact nature of this invention, as well as the objects and advantages thereof, will become readily apparent from consideration of the following specification in conjunction with the accompanying drawings in which like reference numerals designate like parts throughout the figures thereof and wherein:
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DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
(16) Certain embodiments of the invention relate to methods of manufacturing piezo-capable base plate assemblies.
(17) Base plates for use with piezoelectric microactuators may have large openings where parts grouped together may undesirably interlock. Additionally, it is desirable to produce base plates that are sufficiently compliant to be deformed/deflected by piezoelectric microactuators. However, the more compliant the base plate is, the more likely it is to be damaged during handling. In accordance with certain embodiments of the invention, a variety of temporary structures may be used to prevent interlocking and to add structural rigidity until removal at an appropriate stage of the assembly process. For the purposes of this invention, lancing means modifying a surface to create a cleavage line along which a removable portion may be removed from a final part by a reduced shear force. Methods for modifying the surface include but are not limited to stamping, machining, etching, skiving, and other methods known to those of skill in the art for creating a cleavage line along which a removable portion may be removed from a final part by a reduced shear force.
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(20) A second spanning portion 470 may extend from a third side of the second opening 430 to a fourth side of the second opening 430. The second spanning portion may be lanced along a third cleavage boundary 480 adjacent the third side and along a fourth cleavage boundary 490 adjacent the fourth side, so that the second spanning portion 470 becomes removable by a reduced shear force where lanced. The first spanning portion 440 and/or the second spanning portion 470 may be left in place rather than removed from plate 410 to prevent interlocking of multiple base plates 400 and to add structural rigidity until removal of first spanning portion 440 and second spanning portion 470 at an appropriate stage of the assembly process. As shown in
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(25) In certain embodiments, base plate 900 may be lanced by striking a first surface of a first spanning portion 910 with a lancing punch along a first cleavage boundary 920 of base plate 900, as shown in
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(27) The first removable portion 1120 may be struck with a push back punch 1410 (shown in
(28) One of ordinary skill in the art will recognize that the shear distance 1340 may alternately be equal to or greater than plate thickness 1320, resulting in temporarily pressing first removable portion 1120 entirely out of plate 1110 and creating a first opening in plate 1110. In such embodiments, push back punch 1410 may push first removable portion 1120 in a second direction substantially opposite the first direction to reduce the shear distance 1340, thereby forcing first removable portion 1120 back into the first opening in plate 1110 to prevent interlocking of multiple base plates 1100 and to add structural rigidity until removal of first removable portion 1120 at an appropriate stage of the assembly process. In such embodiments, the reduction in shear may be substantially equal to the shear distance, such that major surface 1330 of the first removable portion 1120 lies substantially in a plane with a corresponding major surface of plate 1110.
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(30) One of ordinary skill in the art will recognize that a variety of combinations of openings, spanning portions, and cleavage boundaries may be utilized without deviating from the scope of the invention and that the foregoing embodiments are exemplary and non-limiting.
(31) One of ordinary skill in the art will recognize that any portion of the periphery of any 15 spanning portion described herein or encompassed in equivalent embodiments of the invention may be lanced so that the spanning portion becomes removable by a reduced shear force where lanced. For example and without limitation, rather than creating the at least one opening 720 in the embodiment of
(32) One of ordinary skill in the art further will recognize that in the embodiments of
(33) One of ordinary skill in the art further will recognize that removable spanning portions as described herein may be created by any method for making such spanning portions removable by a reduced shear force without limitation to lancing without departing from the scope of the present invention without departing from the scope of the present invention.
(34) One of ordinary skill in the art further will recognize that a portion of the base plate may be removed in any of the foregoing embodiments to form a swage opening 170 for connecting the base plate to an actuator arm via a swaging operation.
(35) While the invention has been described with reference to the specific embodiments thereof, it should be understood by those skilled in the art that various changes may be made and equivalents may be substituted without departing from the true spirit and scope of the invention as defined by the appended claims. In addition, many modifications may be made to adapt a particular situation, material, composition of matter, method, operation or operations, to the objective, spirit, and scope of the invention. All such modifications are intended to be within the scope of the claims appended hereto. In particular, while the methods disclosed herein have been described with reference to particular operations performed in a particular order, it will be understood that these operations may be combined, sub-divided, or re-ordered to form an equivalent method without departing from the teachings of the invention. Accordingly, unless specifically indicated herein, the order and grouping of the operations is not a limitation of the invention.