An auxiliary turbomachinery shaft-support system including a first assembly configured to axially support the shaft, the first assembly including a rotating disc having a part shaped to be torsionally coupled to the shaft, and a stator including at least one pad including at least one elastic component coupled with the pads and urging it in the direction of a disc sliding surface.

An auxiliary turbomachinery shaft-support system including a first assembly configured to axially support the shaft, the first assembly including a rotating disc having a part shaped to be torsionally coupled to the shaft, and a stator including at least one pad including at least one elastic component coupled with the pads and urging it in the direction of a disc sliding surface.

An eccentric compensating torsional drive system for reducing the rotational eccentric conflict as between multiple eccentric rotational movement limits on the eccentric offset within the drive system, the system includes a motor, a first offset distance coupling, an offset floating bearing, a dynamic element that is driven in a first offset distance rotation by the motor, coupling, and offset floating bearing. Wherein the dynamic element is pivotally connected to a static element via a pivotal offset bearing assembly having a substantially matching offset to the first offset distance. Operationally, the offset bearing can have relative rotational movement to the coupling and dynamic element to lessen the dynamic conflict as between the first offset distance and the pivotal offset bearing assembly as the offset bearing acts as a floating variance in rotational offset via changing a radial position to the coupling and dynamic element.

The element is formed from the winding of a fabric of small thickness ranging between 20 ?m and 150 ?m and mixed with a resin containing fillers. The fabric has the form of strips having a width ranging between 5 mm and 200 mm, with the strips being crossed in several layers.

An outer-ring-equivalent component having an annular raceway surface on which rolling elements roll is disposed on an outer circumference of a bearing. The bearing is, for example, a retainer-equipped roller. Between the bearing and a fixed member located apart from the bearing in an axial direction, a thrust washer is interposed so as to be movable in the axial direction. A gap forming device is provided which constantly forms a gap between the thrust washer and the outer-ring-equivalent component. For example, as the gap forming device, an axial width of the bearing is made larger than an axial width of the outer-ring-equivalent component.

An outer-ring-equivalent component having an annular raceway surface on which rolling elements roll is disposed on an outer circumference of a bearing. The bearing is, for example, a retainer-equipped roller. Between the bearing and a fixed member located apart from the bearing in an axial direction, a thrust washer is interposed so as to be movable in the axial direction. A gap forming device is provided which constantly forms a gap between the thrust washer and the outer-ring-equivalent component. For example, as the gap forming device, an axial width of the bearing is made larger than an axial width of the outer-ring-equivalent component.

A bearing assembly can be used in liquid service applications where the bearing assembly is intermittently or continuously exposed to liquid, such as below the liquid level of a solid-liquid extractor. In some examples, the bearing assembly includes an annular sleeve and an annular bearing. The annular sleeve is designed to be installed over the end of a rotatable shaft and positioned inside of a housing through which the rotatable shaft at least partially protrudes. The annular sleeve has an outer surface and length parallel to the rotational axis of the rotatable shaft. The outer surface of the annular sleeve may taper radially inwardly along at least a portion of the length of the sleeve. As a result, the bearing assembly and rotatable shaft positioned therein may pivot within housing about the taper of the annular sleeve.

An aircraft includes a rotor blade and a rotor hub system. The rotor hub system includes a lead-lag damper having a rod end and being operably associated with the rotor blade; a blade adapter having a first arm and an opposing second arm; a pin carried by the blade adapter and configured to secure in position via the first arm and the second arm; and an actuator secured to the pin and configured to adjust the position of the lead-lag rod end relative to the first arm and the second arm.

A tilting pad, preferably for a radial plain bearing which supports a shaft, with a spaced position in relation to a bearing axis and comprising a supporting surface and a bearing surface opposite the supporting surface, whereby the supporting surface is delimited in an axial direction by two lateral surfaces when viewed transversely, and in a circumferential direction by a run-in edge and a run-out edge when viewed in an installation position, and whereby structures aiding removal of lubricant and coolant are provided on the run-out edge; wherein the structures aiding removal of lubricant and coolant on the run-out edge comprise open-edged recesses arranged on the run-out edge spaced apart from one another in an axial direction.

The invention provides bearing systems characterized by single point contact with each jewel segment and a spring-loaded assembly with protection from radial and thrust forces. An important feature of jewel bearings of the invention is that they are self-lubricating, i.e., no oil or grease lubricants are needed. This can be a major advantage in medical and precision equipment. A secondary important feature is the reduced friction and effective heat-dissipation due to the unique design of the invention with significant reduction in contact surfaces and friction, which significantly prolong the lifespan of the bearings. Another advantage of the present invention is the substantial reduction in audible noise due to the unique design. Furthermore, the invention allows the use of relatively low cost synthetic jewel segments in bearings.