초록 ▼

An exemplary anisotropic member (625, 1200, 1600, 1700, 1800, 1950) supports a bearing in a bore and can reduce non-synchronous vibration (NSV) of the bearing in the bore. An exemplary anisotropic member includes an annular body configured to receive a bearing and to space the bearing a distance fro

An exemplary anisotropic member (625, 1200, 1600, 1700, 1800, 1950) supports a bearing in a bore and can reduce non-synchronous vibration (NSV) of the bearing in the bore. An exemplary anisotropic member includes an annular body configured to receive a bearing and to space the bearing a distance from a bore surface and is configured to impart anisotropic stiffness and damping terms to the bearing when positioned in the bore. Such a member is suitable for use in a rotating assembly for a turbocharger where the bearing may be a floating bearing, a semi-floating bearing or a ball bearing. Various exemplary members, bearings, housings, assemblies, etc., are disclosed.

대표청구항 ▼

1. A rotating assembly for a turbocharger comprising: a center housing that comprises a through bore having a central axis;a fully-floating bearing positioned in the through bore;an anisotropic member that comprises a ring and a series of lobes arranged about the ring, the anisotropic member positio

1. A rotating assembly for a turbocharger comprising: a center housing that comprises a through bore having a central axis;a fully-floating bearing positioned in the through bore;an anisotropic member that comprises a ring and a series of lobes arranged about the ring, the anisotropic member positioned in the through bore between the fully-floating bearing and a surface of the center housing wherein the surface of the center housing defines at least part of the through bore; anda shaft, rotatably supported in the center housing by the fully-floating bearing, the shaft connected at one end to a compressor wheel and at another end to a turbine wheel. 2. The rotating assembly of claim 1 wherein the bearing comprises a compressor side ring that provides a compressor side journal and a turbine side ring that provides a turbine side journal, and wherein the rotating assembly comprises two of the anisotropic members, one configured as an anisotropic compressor side member for the compressor side ring of the bearing and the other configured as an anisotropic turbine side member for the turbine side ring of the bearing. 3. The rotating assembly of claim 1 wherein the through bore comprises an anisotropic through bore. 4. The rotating assembly of claim 1 wherein the anisotropic member comprises an anisotropic support positioned between an outer journal of the fully-floating bearing and the through bore. 5. The rotating assembly of claim 1 wherein the series of lobes of the anisotropic member define stiffness terms. 6. The rotating assembly of claim 1 wherein the ring of the anisotropic member comprises a split ring. 7. The rotating assembly of claim 1 having an axis perpendicular to the central axis of the through bore of the center housing and wherein the lobes of the anisotropic member comprise an alignment with respect to the axis perpendicular to the central axis. 8. The rotating assembly of claim 7 wherein the axis perpendicular to the central axis is aligned with gravity. 9. The rotating assembly of claim 1 wherein the series of lobes comprises lobes positioned at multiple angles about the central axis to generate one or more planes of reflection asymmetry.