Patent ID: 7324302

Claim:
A system for reducing track misregistration in a disk drive, comprising: an enclosure; a disk mounted to the enclosure for rotation relative thereto, the disk having a surface with tracks; an actuator having a head and mounted to the enclosure for moving the head relative to the disk such that the head reads information from and writes information to the tracks on the disk; a flow-conditioning device mounted to the enclosure adjacent to the disk, the flow-conditioning device having a pair of fingers extending radially with respect to the disk and parallel to the surface of the disk, the pair of fingers forming an elongated slot in which the disk is located; a plurality of passages formed in each of the fingers, the passages being axially and radially transverse with respect to the disk, and the fingers is positioned in an air flow stream generated by the disk so that, as the disk rotates, the passages align with the air flow stream and reduce an air flow turbulence intensity and track misregistration between the head and the tracks on the disk; wherein the flow-conditioning device comprises a plurality of the flow-conditioning devices, and the plurality of flow-conditioning devices are mounted to the enclosure in a symmetrical array about the disk; the passages comprise a pair of parallel rows of the cylindrical tubes that are configured in an alternating pattern along a radial length of each of the fingers, such that a centerline of each of the cylindrical tubes is radially spaced apart from centerlines of other ones of the cylindrical tubes in respective ones of the fingers; a boundary layer device mounted directly to a side wall of the enclosure to form a lining along the side wall, the boundary layer device also extending radially from a side wall of the enclosure but radially spaced apart from the disk, and the boundary layer device being separate and spaced apart from the flow-conditioning device to further manipulate the air flow inside the disk drive to provide aerodynamic and acoustic damping that promote viscous dissipation of turbulent fluctuations to further reduce the air flow turbulence intensity and track misregistration between the head and the tracks on the disk; and the lining comprises cavities on the inner wall of enclosure forming a honeycomb of hexagonal walls, each of which is perforated by a small orifice, to form a close-packed array of Helmholtz resonators.