A magnetic head suspension assembly is fabricated with an integral piece which includes a load beam section, a flexure section, a rear mount section and a leaf spring section between the load beam and rear mount. A tongue extends from the load beam to the flexure and has a down-facing load dimple which contacts the non-air bearing surface of an attached air bearing slider. The flexure includes narrow thin legs adjacent to a cutout that delineates the load beam tongue. The head suspension is characterized by a high first bending mode frequency and low pitch and roll stiffness.
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1. A magnetic head suspension assembly including comprising:
an air bearing slider and having at least one transducer disposed on said slider mounted thereon for transducing data that is recorded and read out from a surface of a rotating magnetic disk drive comprising: disc;
a single integral planar piece of a specified thickness of material comprising, :
a load beam section formed with a narrowed end;
a flexure section formed with having a shaped opening which defines two spaced narrow legs defining a cutout portion therebetween, said legs extending flexure beams that extend in a longitudinal direction from said narrowed end of said load beam section, and a lateral ear spaced said flexure section further including a transverse section spaced in said longitudinal direction from said load beam section, said transverse section connecting said legs flexure beams;
a load point tongue extending from said narrowed end of said narrowed load beam section into said shaped opening such that said flexure beams and load point tongue lie substantially in the same plane, said load point tongue being disposed substantially between said legs of said flexure section, said tongue beams and having a free end within said flexure section, shaped opening, said load point tongue being formed with having a load dimple supporting protrusion;
said air bearing slider being bended to said lateral ear transverse section and in contact with said load dimple; whereby load transfer is effectively separated from the gimballing action of said slider so that pitch and roll stiffness is effectively reduced supporting protrusion.
2. An assembly as in
0. 3. An assembly as in
0. 4. An assembly as in
0. 5. An assembly as in
6. An assembly as in
7. An assembly as in
8. An assembly as in
9. An assembly as in claim 2, including a load dimple formed in said tongue 1, wherein said beam section and said transverse section have a first thickness.
10. An assembly as in
11. An assembly as in claim 1, wherein said single integral planar piece including said tongue is about 0.0012 to 0.0015 inch thick and said narrow legs are about 0.0010 inch thick 9, wherein said flexure beams have a second thickness which is thinner than said first thickness.
12. An assembly as in
13. An assembly as in
a leaf spring section attached at a first end to said rear end of said load beam section, said leaf spring section providing a load force to said air bearing slider through said load supporting protrusion; and
including a mount section at the rear end of said load beam attached to a second end of said leaf spring section for enabling mounting said suspension attachment to an actuator arm.; and
a leaf spring section between said rear mount section and said load beam section for providing flexibility to said suspension.
14. An assembly as in claim 13 1, wherein said load beam section has a rear end opposite said narrowed end and further including:
a leaf spring section attached at a first end to said rear end of said load beam section, said leaf spring section providing a load force to said air bearing slider through said load supporting protrusion;
a mount section attached to a second end of said leaf spring section for attachment to an actuator arm; and
a swage plate joined to said mount section for providing rigidity to said rear end of said suspension assembly attachment to said actuator arm.
15. An assembly as in claim 13, including front flanges formed along the edges of said load beam section and rear flanges formed along the edges of said rear mount section with a hiatus between said front and rear flanges 1, wherein said load beam section has first and second sides, at least one of said sides having a flange integral therewith.
16. An assembly as in
17. An assembly as in claim 13, including a cutout in 1, wherein said load beam section has a rear end opposite said narrowed end and further including:
a leaf spring section attached at a first end to said rear end of said load beam section, said leaf spring section providing a load force to said air bearing slider through said load supporting protrusion, wherein said leaf spring section for providing flexibility to said suspension includes a trapezoidal-like opening; and
a mount section attached to a second end of said leaf spring section for attachment to an actuator arm.
18. An assembly as in
19. An assembly as in
20. An assembly as in claim 1 15, further including at least one load/unload tab formed at the sides of said on at least one of said sides of said load beam section.
22. An assembly as in
0. 23. An assembly as in
0. 24. An assembly as in
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This application is a continuation-in-part of application Ser. No. 07/958,516, filed Oct. 7, 1992, now abandoned.
its relatively narrow end into the flexure section 12. The tongue 14 is delineated by a U-shaped cutout 16 in the flexure section the relatively narrow end of the load beam section into a shaped opening 16 of flexure section 12. The tongue 14 delineates the U-shape of the opening 16. The load beam tongue 14 provides low deflections in the direction orthogonal to the plane of the load beam section and flexure section by virtue of its short length and low gram load force.
A constrained layer damping element 19 made of elastomer 10A about 0.002 inch thick and an overlay 10B of about 0.002 inch thick stainless steel is laid down on the top surface of the major section of the load beam to minimize undesirable resonances of the suspension, as shown in FIG. 1. Alternatively, a similar damping element 21 may be deposited on the bottom surface of the load beam without interfering with the flexure 12, as shown in FIG. 3.
The flexure section 12 includes narrow legs 32 that are located adjacent to the sides of the U-shaped cutout 16. The flexure legs 32 flexure beams 32 defined by shaped opening 16. The flexure beams 32 are chemically etched to a thickness of about 0.0010 inch for increased flexibility. The narrow legs 32 are flexure beams 32 are narrow, thin and relatively weak to allow the desired gimbaling action about the load dimple 18 and also to allow the suspension to have low roll and pitch stiffness. A lateral connecting part or ear transverse section 38 is formed with the integral flat load beam and flexure to connect ends of the narrow legs flexure beams 32.
In this implementation of the invention, a slider 22 is bonded to the lateral connecting part 38. A hemispherical load dimple 18 is formed on the load beam tongue 14 and is in contact with the top non-air bearing surface of an air bearing slider 22 that is bonded to the lateral part or ear transverse section 38. The load dimple 18 is formed so that the hemisphere of the dimple faces down to the slider. The dimple 18 may be offset, 0-0.006 inch for example, from the centerline of the slider in order to control flying height characteristics.
U-shaped flanges 24 extend along the sides of the load beam section and are truncated before reaching the flexure section 12. The flanges 24 contribute to the stiffness of the load beam section and localizes the bending action to the spring section 56, thereby minimizing the pitch attitude changes due to arm/disk vertical tolerances. Head circuitry wiring 92 without the conventional tubing is located within the channels of the flanges 24. The absence of tubing allows the U-shaped channels of the flanges 24 to be relatively shallow thereby contributing to the reduction of the Z-height of the head suspension assembly. Adhesive material 90 is used to maintain the wiring 92 fixed in place. Adhesive fillets 91 are provided adjacent to the ear transverse section 38 and the slider 22. The fillets 91 are exposed and thus can be cured easily by application of ultraviolet radiation.
In a disk drive using this head suspension and slider assembly, flexing occurs between the load beam tongue 14 and the flexure legs 32. With this design, the load force is transferred through the tongue 14 to the truncated conical section of the load beam. This integral load beam/flexure configuration allows the separation of the applied load transfer force from the gimbal action so that the structure may be made stiff at the load beam for proper bending and relatively weak about the load dimple to allow proper pitch and roll of the slider.
A feature of the head suspension and slider assembly disclosed herein is that the slider 22 is configured with a step 28, which is formed by cutting a recessed portion or platform 30 on the non-air bearing top surface of the slider 22. The Z-height of the step 28 is substantially the same as the Z-height of the hemisphere load dimple 18. Sufficient spacing is provided between the load beam tongue 14 and the top slider surface to allow free gimbaling action of the slider 22 with no interference from the load beam. The slider step 28 is sufficiently high so that the slider end at the trailing edge can accommodate a thin film magnetic transducer including its coil turns.
The leaf spring 56 between the load beam section 10 and the rear mount section 42 is formed with a trapezoidal-like cutout opening 60 to provide flexibility. The flexible section 56 is formed to provide a desired load force that counteracts the aerodynamic lift force generated by the rotating disk during operation of the disk drive. The load force arises from bending the suspension from the phantom position, shown in
The rear mount section 42 of the load beam 10 has a hole 48 to allow connection of a swage plate 46 to the suspension by means of a boss 48 and by laser welding. The swage plate 46 provides stiffness to the rear mount section 42. Rear flanges 54 provide wire routing channels to protect the wires during handling.
The head suspension and slider assembly described herein incorporates a stiff load beam and a relatively long and narrow flexure which includes thin weak flexure legs and connecting lateral part. With this design, low bending stiffness and high lateral and longitudinal stiffness with low roll and pitch stiffness are realized. The load beam tongue has a high vertical or perpendicular stiffness so that there is minimal bending of the load beam tongue up or down relative to the plane of the suspension. The first bending mode resonant frequency or vibration is substantially higher than known prior art suspension designs of comparable size.
In an actual implementation of this invention, the overall height of the slider is about 0.0110 inch, its length about 0.0400 inch, and its width about 0.020 inch. The height of the step 28 is about 0.0015 inch above the recessed portion 30 which is 0.0336 inch long. The surface area of the top of the step 28 is preferably minimized in size to reduce the effects of bending or warping at the surface of the slider step which may occur due to the difference in the thermal coefficients of expansion of the ceramic slider 22 and the stainless steel ear transverse section 38. Such bending would affect the flying characteristics of the head adversely.
In an alternative embodiment of the head suspension, illustrated in part in
With reference to
By virtue of this invention, a single integral piece is formed with a load beam and flexure, thereby realizing a significant savings in material and labor. Alignment of the load beam and flexure and welding of the separate parts are eliminated. Certain critical tolerances that were required in former load beam/flexure assemblies are no longer needed thereby enhancing the assembly process. The design allows the separation of the load transfer function from the gimbaling action which eliminates the weak bending characteristic found with prior art suspensions. It should be understood that the parameters, dimensions and materials, among other things, may be modified within the scope of the invention. For example, the slider design with the step and platform configuration disclosed herein can be used with a “50” nanoslider suspension or other size suspensions.
Leung, Chak M., Hatch, Michael R.
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