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Takao Yoshitsugu

Researcher at Panasonic

Publications -  27
Citations -  195

Takao Yoshitsugu is an academic researcher from Panasonic. The author has contributed to research in topics: Bearing (mechanical) & Flange. The author has an hindex of 8, co-authored 27 publications receiving 195 citations. Previous affiliations of Takao Yoshitsugu include Takata Corporation.

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Patent

Hydrodynamic bearing and motor having the same

TL;DR: In this paper, the relation between width-A and width-B in the first herringbone pattern is expressed by 0 <(A−B)<0.2x(A+B), where A denotes the dimension from a turning point of the first pattern to the end of the second pattern, and B denotes the dimensions from the turning point to end thereof in the second side.
Patent

Hydrodynamic bearing device and disk rotating apparatus

TL;DR: In this paper, a hydrodynamic bearing device with a radial bearing face having a dynamic pressure generating groove on a shaft or an inner periphery of a sleeve is provided and an annular depression is provided on one end face of the sleeve adjacent to a rotor hub.
Patent

Hydrodynamic bearing device, motor, and disk driving apparatus

TL;DR: In this paper, a hydrodynamic bearing device consisting of a shaft, a thrust flange, a sleeve, a seal plate, and a retaining plate is presented, where a communicating hole is formed for communicating between the gap between the sleeve and the seal plate.
Patent

Spindle motor and method for assembling the same

TL;DR: In this article, a downsized spindle motor having a longer bearing service life and enhanced shock resistance includes a flange 11, which bears an axial load of a shaft 8, and which is fixed to an end of shaft 8.
Patent

Hydrodynamic bearing device

TL;DR: In this paper, a hydrodynamic bearing which prevents a lubricating fluid from scattering out of the dynamic pressure generating portion is proposed, which includes radial spacing d of a gap at an open end of the thrust-side dynamic pressure generation portion, whose value is greater than a spacing relative to the thrust direction.