A slide bearing can include a metal support, a primer layer, an adhesive layer applied directly thereto, and a sliding layer applied to the adhesive layer. The primer layer can include an oligomeric condensate of at least one silanol selected from the group having the formula: ##STR00001## wherein x is 1 or 2, y is 0 or 1.
The moieties R.sup.1 and R.sup.2 can be the same or different. The moieties R.sup.1 and R.sup.2 can be selected from the group consisting of methyl, ethyl, n-propyl, i-propyl, and a functionalized alkyl group R(CH.sub.2).sub.z, wherein z is at least 1. Slide bearings comprising a primer system based on silanol oligomeric condensates show improved peel strength than their analogous slide bearings lacking the primer system.

The present application relates to a sliding bearing material comprising a steel substrate back and an aluminum alloy applied thereto, characterized in that the aluminum alloy contains an aluminum alloy matrix and hard particles, preferably 0.01 to 10 wt %, and/or fibers, preferably 0.01 to 50 vol %. The invention further relates to a method for producing a sliding bearing material, to the use of a sliding bearing material for a sliding bearing and to a sliding bearing.

A gear shaft allows a ceramic bearing to be used in environments where gear steel is desirable for driving a gear. The gear shaft includes a gear region and a bearing region. A bearing can be disposed about the bearing region of the gear shaft. A gear can be disposed about the gear region of the gear shaft. The bearing includes a ceramic material. The gear region of the gear shaft includes gear steel, whereas the bearing region of the gear shaft includes a bearing-region material that has a coefficient of thermal expansion (CTE) that is close to the CTE of the ceramic material.

A landing bearing assembly for a rotary machine having a stator assembly, a rotor assembly and a magnetic bearing. The landing bearing assembly having a stator landing portion integral with the stator assembly and a rotor landing portion integral with the rotor assembly. A first coating, which is an anti-wear and/or an anti-friction coating, is dispensed on at least one of the stator landing portion and the rotor landing portion. The invention also concerns such a rotary machine.

An aircraft includes an airframe and a rotary component rotatably connected to the airframe by way of a plain bearing. The rotary component is part of a rotorcraft control system. The plain bearing includes an inner member rotatably engaged in at least two axes of rotation to an outer member. The inner member has a coefficient of thermal expansion (CTE) substantially less than that of the outer member.

A static pressure gas bearing used in a vacuum environment includes a guide shaft and a tubular slider which is movable in an axial direction in a state where the guide shaft is accommodated therein. The slider is configured by fastening a plurality of plate-shaped members. A film formed of a soft material having a smaller elastic modulus than that of each of the plate-shaped members is interposed between joint surfaces of the plate-shaped members.

Bearings with grooves and methods of producing the same are disclosed. Examples disclosed herein include a bearing having a bearing surface with a groove, the bearing positioned adjacent to a shaft, the groove facing the shaft, and a negative thermal expansion (NTE) material positioned in the groove, the NTE material at least partially filling the groove.

In an embodiment, a bearing assembly may include a support ring to which one or more superhard bearing elements may be mounted. The support ring may include one or more relief features configured to reduce residual stresses in the superhard bearing elements that are induced by brazing the superhard bearing elements to the support ring, operational loads, other processes, or combinations of the foregoing. Reducing the residual stresses in the superhard bearing elements may help prevent damage to the superhard bearing elements. The bearing assembly may be used in subterranean drilling systems and/or other types of systems.

In an embodiment, a bearing assembly may include a support ring to which one or more superhard bearing elements may be mounted. The support ring may include one or more relief features configured to reduce residual stresses in the superhard bearing elements that are induced by brazing the superhard bearing elements to the support ring, operational loads, other processes, or combinations of the foregoing. Reducing the residual stresses in the superhard bearing elements may help prevent damage to the superhard bearing elements. The bearing assembly may be used in subterranean drilling systems and/or other types of systems.

A radial bearing assembly and method of manufacture that provides a radial bearing assembly having a plurality of spherical bearing inserts, such as ball-shaped carbide inserts, bonded to a bearing sleeve. The method of manufacture utilizes a mold for simultaneously brazing and bonding the spherical beating inserts to the surface of the bearing sleeve.