A system includes a hydraulic transfer system configured to exchange pressures between a first fluid and a second fluid, where the first fluid has a pressure higher than the second fluid, includes a sleeve comprising an elliptical shape, a cylindrical rotor disposed within the sleeve in a concentric arrangement, where the cylindrical rotor is configured to rotate circumferentially about a rotational axis and has a first end face and a second end face disposed opposite each other. The system includes a first and second end cover having a first and second surface which interface with a first and second end face of the rotor. The system includes a first and a second radial clearance disposed between the sleeve and the cylindrical rotor, where the radial clearances are configured to increase or decrease based at least in part on a pressure differential.

Embodiments disclosed herein are directed to tilting pad bearing assemblies, bearing apparatuses including the tilting pad bearing assemblies, and methods of using the bearing apparatuses. The tilting pad bearing assemblies disclosed herein include a plurality of tilting pads. At least some of the superhard tables exhibit a thickness that is at least about 0.120 inch and/or at least two layers having different wear and/or thermal characteristics.

A hydrodynamic sliding bearing, including: a housing shell including an inner surface which forms a bearing surface configured for a rotating shaft having a radius, the housing shell including a center point, the bearing surface including at least two surface sections which are arranged one behind the other in a circumferential direction of the bearing shell, the at least two surface sections including at least one first surface section and at least one second surface section, the at least one second surface section forming a load segment, the at least one first surface section forming a non-load segment, the at least two surface sections each configured for being inscribed thereinto in an axial section with a respective circle, the respective circle of each of the at least two surface sections each having a radius that is larger than the radius of the rotating shaft and each having a center point each of which exhibits a respective eccentricity relative to the center point of the housing shell, the eccentricity of the load segment being greater than the eccentricity of the non-load segment.

A turbocharger includes a compressor wheel, a shaft, a bearing housing, and a floating ring. The shaft is coupled to the compressor wheel and extends through the bearing housing. The bearing housing includes an inner housing surface extending circumferentially around the shaft. The floating ring rotatably supports the shaft in the bearing housing and rotates relative to the bearing housing and the shaft. The floating ring includes an outer bearing surface that extends circumferentially around the shaft and that faces the inner peripheral housing surface. The inner housing surface is formed of a rigid material and has an inner housing cross-sectional shape that in a first axially outer region of the inner housing surface is non-circular perpendicular to the axis, decreases in area moving axially toward a first axial end, and forms a first outer fluid film interface with the outer bearing surface of the floating ring.

A gas bearing system has at least one gas bearing (30, 32, 34) with a moving part and a static part and which can be operated in both aero-dynamic and aero-static modes. The system has a source (36) of pressurized gas fluidly connected with the bearing and a control system (134) for regulating the supply of pressurized gas to the bearing in dependence on the rotational speed of the moving part. The system has particular application in a turbocharger (1) where a flow of pressurized gas from the source is introduced into the bearing at the start-up and slow down phases of operation of the turbocharger, the flow being stopped, or reduced, when the turbocharger has reached normal operating speeds.

A countershaft as disclosed herein may include one or more bearing zones along its axial length. Each bearing zone may include one or more radial holes in fluid communication with one or more grooves, respectively, and one or more axial channels formed along the longitudinal length of the countershaft. Each groove may be positioned adjacent an interface between a rotating member and a non-rotating member and include one or more features therein, such as a profile and/or taper.

In an exhaust gas turbocharger, comprising a first radial bearing and a second radial bearing configured for the radial support of a shaft of the exhaust gas turbocharger, wherein the first radial bearing comprises a bearing axis extending in alignment with the bearing axis of the second radial bearing which is arranged spaced from the first radial bearing, a third radial bearing with a third bearing axis, which is extends parallel to, but at a distance (E) from, the first bearing axis and the second bearing axis is arranged between the first and second radial bearings.

A turbocharger assembly includes a center housing which defines a bore, a journal bearing, and a rotating assembly. The bore further defines primary and secondary annular grooves. The journal bearing may be disposed within the bore such that the annular groove encircles the journal bearing and feeds the fluid thereto. The rotating assembly includes a shaft, a turbine wheel and a compressor wheel. The turbine wheel is configured to be driven by the post-combustion gasses while the compressor wheel pressurizes the airflow for delivery to a combustion chamber. The shaft may be supported by one or more journal bearings for rotation within the bore about a longitudinal axis. The shaft includes a shaft surface which defines a standard region and a feature in a feature region. The feature is configured to generate a plurality of fictitious forces which stabilizes the turbocharger shaft.

A multi-arc bearing includes: a bearing surface a cross-sectional shape of which perpendicular to an axial direction of a shaft includes a plurality of arcs; and an oil supply groove provided on the bearing surface and extending in the axial direction of the shaft, the oil supply groove having a bearing clearance at a front side end portion in a rotation direction of the shaft smaller than a bearing clearance at a rear side end portion in the rotation direction.

A hydrodynamic plain bearing having a stator and a rotor rotatable with respect to the stator, a rotor bearing surface being located opposite a counter-surface of the stator in order to generate hydrodynamic pressure. The rotor bearing surface and/or the counter-surface constitutes in a section view, in the context of a section along and through the rotation axis, a continuous bearing contour that is constituted from at least two contour segments. The contour segments are suitable for generating hydrodynamic load capacity in a radial and axial direction. The contour segments are led into one another, by at least one transition segment, in such a way that hydrodynamic load capacity is generatable via the contour segments and the transition segment. The plain bearing is embodied as a multiple-surface plain bearing having two or more lubrication wedges in the region of the contour segments and of the transition segment.