Claims
- 1. An apparatus for reducing windage-induced vibration in a disc drive having a rotating disc, the apparatus comprising:
a load beam; a trench arrangement on the load beam; and a circuit housed within the trench arrangement.
- 2. The apparatus of claim 1 further including a plate coupled to the load beam, wherein the circuit is between the load beam and the plate.
- 3. The apparatus of claim 1, wherein the load beam is made from a laminate material.
- 4. The apparatus of claim 3, wherein the laminate material includes a bottom steel layer, a core polyimide layer, and a top steel layer.
- 5. The apparatus of claim 4, wherein the bottom steel layer has a thickness in the range of about 20 to 75 μm, the core polyimide layer has a thickness in the range of about 10 to 125 μm, and the top steel layer has a thickness in the range of about 20 to 75 μm.
- 6. The apparatus of claim 4, wherein the bottom steel layer has a thickness of about 30 μm, the core polyimide layer has a thickness of about 75 μm, and the top steel layer has a thickness of about 30 μm.
- 7. A disc drive system comprising:
a rotating disc having an inner and an outer diameter; a suspension assembly for supporting a head over the disc, the suspension assembly having; a load beam comprising a laminate material; a trench arrangement formed in the load beam; and a circuit housed within the trench arrangement.
- 8. The system of claim 7 including a plate coupled to the load beam, wherein the circuit is between the load beam and the plate.
- 9. The system of claim 7 wherein the laminate material includes a bottom steel layer, a middle polyimide layer, and a top steel layer.
- 10. The system of claim 9 wherein the bottom steel layer has a thickness in the range of about 20 to 75 μm, the core polyimide layer has a thickness in the range of about 10 to 125 μm, and the top steel layer has a thickness in the range of about 20 to 75 μm.
- 11. The system of claim 8 wherein the load beam comprises a gimbal portion, a bend section, and a base portion, the gimbal portion supporting the head and the bend section being positioned between the base portion and the gimbal portion, and the trench arrangement includes a trench that extends from the bend section and through at least a part of the base portion.
- 12. A suspension assembly configured to reduce windage-induced vibration in a head supported by the suspension assembly, comprising:
a base plate; a load beam mounted to the base plate and having a length, the load beam comprising a laminate material, the laminate material having a bottom layer a top layer, and a core layer positioned between the top and bottom layers, the load beam further comprising a trench formed in the laminate material and extending along at least a portion of the length of the load beam; and an interconnect circuit mounted to the load beam in at least a portion of the trench.
- 13. The assembly of claim 12 wherein the load beam is secured to the base plate at the bottom layer of the laminate material.
- 14. The assembly of claim 12 wherein the trench is formed in the bottom and core layers of the laminate material.
- 15. The assembly of claim 12 wherein the interconnect circuit includes a first portion and a second portion, and the load beam further comprises an exposed primary surface and a leeward edge, the first portion being mounted in the trench, and the second portion extending along the leeward edge of the load beam.
- 16. The assembly of claim 12 wherein the top layer comprises steel, the core layer comprises a polymer material, and the top layer comprises steel.
- 17. The assembly of claim 12 wherein the load beam includes a first end supporting the head, a second end adjacent the base plate, and a bend section between the first and second ends, and the trench extends from the second end to the bend section.
- 18. The assembly of claim 12 wherein the interconnect circuit is a flex-on-suspension circuit.
- 19. The assembly of claim 12 wherein the load beam further comprises a boss aperture configured to mount the suspension assembly to a support arm having a boss, and the trench extends around the boss aperture.
- 20. A method of forming a suspension assembly that is resistant to windage-induced vibrations, the suspension assembly comprising a load beam constructed of a laminate material and having a length, an interconnect circuit, and a base plate, the method comprising the steps of:
etching layers of the laminate material; assembling the etched layers into a composite material, the assembled layers defining a trench that extends along a portion of the load beam length; securing a first portion of the interconnect circuit in the trench; and mounting the load beam to the base plate so that the first portion of the interconnect in the trench is positioned between the load beam and the base plate.
- 21. The method of claim 20 wherein the load beam further includes a leeward edge and a primary exposed surface, and the interconnect circuit further includes a second portion, the method further comprising the step of securing the second portion of the interconnect circuit to the leeward edge and the exposed primary surface of the load beam.
- 22. The method of claim 20 wherein the laminate material comprises top, bottom, and core layers, and the etching step includes etching trenches in the core and bottom layers.
- 23. The method of claim 20 wherein the etching step includes etching a bottom layer and a top layer from a sheet comprising steel, and etching a core layer from a sheet comprising a polymer material.
- 24. The method of claim 20 wherein the laminate material includes bottom, top, and core layers, and the mounting step includes mounting the bottom layer to the base plate.
- 25. The method of claim 20 wherein the load beam includes a first end configured to support a disc drive head, a second end positioned adjacent the base plate, and a bend section positioned between the first and second ends, and the trench extends from the second end to the bend section of the load beam.
RELATED APPLICATIONS
[0001] This application claims priority of U.S. provisional application Serial No. 60/409,889, filed Sep. 11, 2002, entitled “Interconnect Routing For A Head Gimbal Assembly”.
Provisional Applications (1)
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Number |
Date |
Country |
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60409889 |
Sep 2002 |
US |