Integrated windage blocker for reduction of flex cable vibration in a disk drive

1. A base for a hard disk drive comprising:

a cavity portion comprising a planar surface defining an inner bottom surface of said cavity, said cavity portion for receiving an actuator assembly, said actuator assembly comprising a flex cable; and

at least one windage blocker integrated with said planar surface of said cavity of said base, said at least one windage blocker for reducing detrimental local excitation of an airflow encountering said flex cable wherein said windage blocker reduces vibrations of said flex cable in a frequency range of 400 Hz to 500 Hz.

2. The base for a hard disk drive of claim 1 wherein said airflow is generated by a rotating of a disk and said at least one windage blocker comprises an aerodynamically shaped leading edge with respect to a direction of rotation of said disk.

3. The base for a hard disk drive of claim 1 wherein said windage blocker comprises a planar surface that is perpendicular to said inner bottom surface of said cavity.

4. The base for a hard disk drive of claim 1 wherein a leading edge of said at least one windage blocker is formed in the shape of an arc generated by a motion of said actuator assembly.

5. The base for a hard disk drive of claim 1 wherein said windage blocker is disposed on said bottom surface of said cavity between a predetermined mounting location of said actuator assembly and a predetermined location of said flex cable.

6. The base for a hard disk drive of claim 1 wherein said windage blocker is cast within said cavity.

7. A hard disk drive comprising:

a housing comprising a cavity portion having a planar surface defining an inner bottom surface of said cavity,

a disk pack mounted to the cavity and having a plurality of disks that are rotatable relative to the housing, the disk pack defining an axis of rotation and a radial direction relative to the axis, wherein the rotating of said plurality of disks generates an airflow;

an actuator assembly mounted to the housing and being movable relative to the disk pack, the actuator assembly having a plurality of sliders thereon and a flex cable coupled thereto; and

at least one windage blocker integrated with said housing, said at least one windage blocker for reducing detrimental local excitation of said airflow encountering said flex cable.

8. The hard disk drive of claim 7 wherein said at least one windage blocker comprises an aerodynamically shaped leading edge with respect to said radial direction of said rotating of said disks.

9. The hard disk drive of claim 7 wherein said windage blocker comprises a planar surface that is perpendicular to said inner bottom surface of said cavity.

10. The hard disk drive of claim 7 wherein a leading edge of said at least one windage blocker is formed in the shape of an arc generated by a motion of said actuator assembly.

11. The hard disk drive of claim 7 wherein said windage blocker is formed as part of said bottom surface of said cavity at a location that is between said actuator assembly and said flex cable.

12. The hard disk drive of claim 7 wherein said windage blocker is cast within said cavity.

13. The hard disk drive of claim 7 wherein said windage blocker reduces vibrations of said flex cable in a frequency range of 400 Hz to 500 Hz.

14. A method for reducing flow induced vibration related to airflow encounters with a flex cable of a hard disk drive, said method comprising:

receiving a flex cable at an actuator assembly coupled to a base;

providing at least one windage blocker integrated within said base proximate said actuator assembly to reduce unsteady airflow related to airflow encounters with said flex cable, thereby reducing flow induced vibration of at least a portion of said actuator assembly; and

reducing vibrations of said flex cable in a frequency range of 400 Hz to 500 Hz by utilizing said windage blocker to reduce detrimental local excitation of an airflow encountering said flex cable.

15. The method as described in claim 14 further comprising:

casting said windage blocker as an integrated part of said base.

16. The method of claim 14 further comprising:

forming an aerodynamically shaped leading edge of said windage blocker with respect to a direction of rotation of a disk.

17. The method of claim 14 further comprising:

forming a planar surface of said windage blocker that is perpendicular to an inner bottom surface of said base.

18. The method of claim 14 further comprising:

forming said windage blocker in the shape of an arc generated by a motion of said actuator assembly.