Abstract: An exemplary system for a turbomachine includes a bore extending from an inner end to an outer end with an inner seat proximate to the inner end and an outer seat proximate to the outer end, a rotatable shaft with an inner slot and an outer slot, an outer seal ring capable of being received by the outer slot and capable of being seated in the outer seat and an inner seal ring capable of being received by the inner slot, capable of bridging the outer seat and capable of being seated in the inner seat where an axial width of the inner seal ring exceeds an axial width of the outer seal ring. Various other exemplary devices, systems, methods, etc., are also disclosed.

Abstract: An exemplary method includes positioning a plurality of seal rings on a shaft operably coupled to a turbine wheel and inserting the shaft into a bore via axial inward movement wherein during insertion, an outer seal ring contracts and then expands along a chamfer to reach an outer seal seat. Various other exemplary devices, systems, methods, etc., are also disclosed.

Abstract: An exemplary bore for a shaft of a turbomachine includes a longitudinal axis extending generally from an inner end to an outer end of the bore, an outer seat disposed proximate to the outer end of the bore at an outer seat radius for an outer seal ring wherein the outer seat comprises an inner end, an outer end, a step at the inner end extending radially inward to a step radius, and a chamfer at the outer end extending radially inward over an outward axial distance to a chamfer plateau radius and an inner seat disposed inward the outer seat at an inner seat radius for an inner seal ring wherein the outer seat radius exceeds the inner seat radius. Various other exemplary devices, systems, methods, etc., are also disclosed.

Abstract: A hydrodynamic thrust bearing of this invention comprises a body having a load-bearing surface comprising an oil supply channel and an oil return channel positioned along respective inside and outside body diameters. A number of thrust pads are positioned along the surface that each include an oil supply groove, positioned adjacent a leading edge/upstream portion of each thrust pad and extending radially a distance from the oil supply channel, and an oil return groove, positioned adjacent a trailing edge/downstream portion of each thrust pad and extending radially a distance from the oil return channel. The oil supply grooves are separate from the oil return grooves, and the thrust pads each comprise a series arrangement of three differently configured land or pad sections. Configured in this manner, oil is provided onto the series of land sections by the oil supply groove and is collected after passing over the series of land sections by the separate oil collection groove.

Abstract: A hydrodynamic thrust bearing of this invention comprises a body having a load-bearing surface comprising an oil supply channel and an oil return channel positioned along respective inside and outside body diameters. A number of thrust pads are positioned along the surface that each include an oil supply groove, positioned adjacent a leading edge/upstream portion of each thrust pad and extending radially a distance from the oil supply channel, and an oil return groove, positioned adjacent a trailing edge/downstream portion of each thrust pad and extending radially a distance from the oil return channel. The oil supply grooves are separate from the oil return grooves, and the thrust pads each comprise a series arrangement of three differently configured land or pad sections. Configured in this manner, oil is provided onto the series of land sections by the oil supply groove and is collected after passing over the series of land sections by the separate oil collection groove.

Abstract: A hydrodynamic thrust bearing having a series arrangement of three differently configured land sections across the bearing axial surface that are separated by an oil supply groove (on one side) and an oil return or collection grove (on an opposite side). Configured in this manner, oil is provided onto the series of land sections by the oil supply groove and is collected after passing over the series of land sections by the separate oil collection groove. The use of separate oil supply and collection grooves acts to minimize mixing, of input oil with the heated return oil, thereby reducing oil film temperature and increasing bearing thrust load capacity.

Abstract: An integrated bearing system with journal and thrust bearings is incorporated in a single unit centrally pinned to the bearing housing and having integral thrust surface and journal surface lubrication grooves in combination with turbine and compressor wheel thrust surfaces. The bearing employs a first aperture substantially equidistant from the ends to engage the locating pin to prevent rotation of the bearing within the bearing case bore, while allowing the bearing to be free to symmetrically wobble within the bearing case bore.