To provide a sliding member including an overlay capable of realizing good fatigue resistance while preventing interlayer peeling. A sliding member including an overlay formed of an alloy plating film of Bi and Sb, and the overlay is bonded to a lining formed of a copper alloy via an intermediate layer containing Ag as a main component.

The invention relates to a sliding bearing element (1) comprising a supporting layer (2) and a sliding layer (3), the sliding layer (3) being made of silver or silver having a maximum content of other metals of 5% by weight, selected from a group consisting of Cu, Sb, Mo, Co, and the sliding layer (3) has a microstructure with grains (6, 7) and has a sliding layer thickness (12). The microstructure changes on the sliding layer thickness (12) from a globular habitus of the grains (7) in the region of a second surface (9) of the sliding layer (3) closer to the supporting layer (2) to a habitus in an at least approximately columnar form, a longitudinal extension (10) of the grains (7) being arranged in the region of a first surface (8) of the sliding layer (3) farther away from the supporting layer (2).

A bearing element for at least one adjustable guide vane of a turbomachine, in particular an aircraft engine, is provided. The bearing element comprising a porous matrix made of carbon and/or graphite and at least one metallic phase or a metal salt that is at least partially arranged inside the pores of the matrix, so that what results is a metal-infiltrated or a metal-salt-infiltrated material.

A rolling bearing of the present invention includes an inner ring, an outer ring and a rolling element which are all made of a steel material, and (A) a surface of the rolling element is formed with an Ag coating film, and a raceway of at least one of the inner ring and the outer ring is formed with a Cr coating film or (B) a surface of the rolling element is formed with a Cr coating film, and a raceway of at least one of the inner ring and the outer ring is formed with a Cr coating film.

A turbomachine according to an embodiment of the present disclosure may include a rotary shaft, a magnetic bearing including a core body configured to surround the rotary shaft, a plurality of poles radially extending from an inner surface of the core body toward the rotary shaft, and coils wound around the plurality of poles to levitate the rotary shaft by using a magnetic force generated by a magnetic field formed by applied electric current, a sleeve journal bearing disposed between the rotary shaft and the magnetic bearing so as to surround the rotary shaft and configured to levitate the rotary shaft by generating a dynamic pressure when the rotary shaft rotates, and a permanent magnet disposed between the plurality of poles and configured to support the rotary shaft by using a magnetic force.

Embodiments of the invention are directed to bearing assemblies configured to effectively provide heat dissipation for bearing elements, bearing apparatuses including such bearing assemblies, and methods of operating such bearing assemblies and apparatuses. In an embodiment, a bearing assembly includes a plurality of superhard bearing elements distributed about an axis. Each superhard bearing element of the plurality of superhard bearing elements has a superhard table including a superhard surface. The bearing assembly includes a support ring structure coupled to the plurality of superhard bearing elements. One or more of the superhard bearing elements includes a superhard table, which may improve heat transfer from such superhard bearing elements.

A technique capable of reducing the possibility of generation of a CuSb compound in an overlay and the possibility of delamination between layers. A sliding member includes: an overlay including an alloy plating film of Bi and Sb; a lining including an Al alloy; a first intermediate layer including Cu as a main component, and laminated on the lining; and a second intermediate layer including Ag as a main component, and connecting the first intermediate layer and the overlay.

Embodiments of the invention are directed to bearing assemblies having features that provide heat dissipation for bearing elements, bearing apparatuses including such bearing assemblies, and methods of operating such bearing assemblies and apparatuses. In an embodiment, a bearing assembly includes a plurality of superhard bearing elements distributed about an axis. Each superhard bearing element of the plurality of superhard bearing elements has a superhard table including a superhard surface. The bearing assembly includes a support ring structure coupled to the plurality of superhard bearing elements. One or more of the superhard bearing elements includes a superhard table, which may have a thickness at a peripheral that is greater than an average thickness of the superhard table improve heat transfer from such superhard bearing elements.

A thrust sliding bearing may include a thrust receiving surface comprising radial oil grooves, and a resin portion, the resin portion comprising a plurality of resin sheets in an area defined by the oil grooves of the thrust receiving surface, the plurality of resin sheets being laminated. Circumferential widths of the plurality of resin sheets may increase upwardly from a bottom resin sheet. A circumferential width of the resin portion may decrease upwardly.

The invention relates to a sliding bearing element (1) comprising a supporting layer (2) and a sliding layer (3), the sliding layer (3) being made of silver or silver having a maximum content of other metals of 5% by weight, selected from a group consisting of Cu, Sb, Mo, Co, and the sliding layer (3) has a microstructure with grains (6, 7) and has a sliding layer thickness (12). The microstructure changes on the sliding layer thickness (12) from a globular habitus of the grains (7) in the region of a second surface (9) of the sliding layer (3) closer to the supporting layer (2) to a habitus in an at least approximately columnar form, a longitudinal extension (10) of the grains (7) being arranged in the region of a first surface (8) of the sliding layer (3) farther away from the supporting layer (2).