초록 ▼

A bearing supporting arrangement is provided for a turbocharger having a turbine shaft provided with turbine and compressor wheels. The bearing supporting arrangement includes first and second cylindrical oil film damper members, each of which is supported in a floating state through an oil film to

A bearing supporting arrangement is provided for a turbocharger having a turbine shaft provided with turbine and compressor wheels. The bearing supporting arrangement includes first and second cylindrical oil film damper members, each of which is supported in a floating state through an oil film to the inner peripheral surface of a bearing housing thereby constituting an oil film damper. First and second annular ball bearings are coaxially fixedly supported respectively to the first and second oil film damper members. A generally cylindrical thrust receiving member is interposed between the first and second oil film damper members to be contactable with the first and second oil film damper members. The thrust receiving member is fixed at an axially intermediate portion to the bearing housing by a pin fixed to the bearing housing so as to be movable to make contact with the bearing housing. A first clearance (C1) is defined between the bearing housing and the thrust receiving member, while a second clearance (C2) is defined between the bearing housing and each of the first and second oil film damper members. In the above arrangement, a first ratio (C1/L1), of the first clearance (C1) relative to the axial length (L1) of the thrust receiving member, is set smaller than a second ratio (C2L2) of the second clearance relative to the distance (L2) between the axially outside end face of the first oil film damper member and the axially outside end face of the second oil film damper member.

대표청구항 ▼

A bearing supporting arrangement for a turbocharger having a turbine shaft, comprising: a bearing housing defining a bore thereinside, first and second generally cylindrical oil film damper members located separate from each other with a distance (L2) separating their respective axially outside face

A bearing supporting arrangement for a turbocharger having a turbine shaft, comprising: a bearing housing defining a bore thereinside, first and second generally cylindrical oil film damper members located separate from each other with a distance (L2) separating their respective axially outside faces, each of said first and second oil film damper members being separated from a surface of said bearing housing bore to define therebetween a second clearance (C2) which is filled with a lubricating oil; first and second rolling bearings which are separate from each other and are coaxially fixedly secured respectively to said first and second oil film damper members; a compression coil spring disposed between axially inside end faces of said first and second oil film damper members; a generally cylidrical thrust receiving member of a length (L1) smaller than said distance separating said axially outside end faces (L2), interposed between the axially inside end faces of said first and second oil film damper members and extending generally in an axial direction of said bearing housing bore, the outer peripheral surface of said thrust receiving member being separated from the adjacent surface of said bearing housing bore to define therebetween a first clearance (C1); a fixing pin secured to said bearing housing and engaged with with an axially intermediate portion of a cylindrical wall of said thrust receiving member so that said thrust receiving member is slightly movable in a direction generally perpendicular to the axis of said bearing housing bore to be contactable with the surface of said bearing housing bore, a first ratio (C1/L1), of said first clearance (C1) realative to said axial length (L1) of said thrust receiving member being selected to be smaller than a ratio (C2/L2) of said second clearance relative to said distance (L2) separating said outside axial end faces.