A seal system has: a first member; a seal carried by the first member and having a seal face; and a second member rotatable relative to the first member about an axis. The second member has: a seat on a first piece of the second member, the seat having a seat face in sliding sealing engagement with the seal face; and a radially outwardly closed collection channel for collecting centrifuged oil; a second piece encircling and attached to the first piece and having a circumferential array of apertures; and cooperating with the first piece to define a plenum; and a flowpath from the collection channel passing radially outward axially spaced from the seat face to cool the seat face and passing axially away from the seat face in the plenum.

A brush seal system includes a component including a first mating surface. The brush seal system further includes a brush seal including a brush seal backing plate, a retaining ring, and a plurality of bristles retained between the brush seal backing plate and the retaining ring. The brush seal backing plate includes a second mating surface mounted to the first mating surface. The brush seal system further includes at least one cooling channel extending from an exterior side of the component to an interior side of the component so as to bypass the brush seal.

Systems and processes for forming seals. The seals have graphene embedded in the seal. The graphene-embedded seals exhibit improved wear resistance over seals without graphene.

A compressor includes an impeller configured so as to compress gas, an electric motor, a rotary shaft configured so as to join the impeller and the electric motor to each other, a housing configured so as to house the rotary shaft and the electric motor, a mechanical seal that includes a rotation-side seal member provided in the rotary shaft, and a stationary-side seal member fixed to the housing so as to be in contact with the rotation-side seal member on a side of the impeller, and a member that defines a lubricant reservoir provided under the mechanical seal in a gravity direction and disposed so as to store lubricant, the member being disposed so that the lubricant reservoir is arranged such that at least a part of the rotation-side seal member on an outer circumference side passes through when rotation-side seal member rotating due to rotation of the rotary shaft.

A fastener driving tool with a working cylinder and a piston, the piston outer surface having a lubricant-saturated foam material that stores and dispenses lubricant into the piston-cylinder wall interface, thereby increasing the performance and lifespan of the tool. Another embodiment discloses a two-part piston in which the bottom portion is made of metal and absorbs the main mechanical loading forces of the piston drive and return strokes, and the top portion is made of a non-metallic material that has surfaces that act as sliding bearings against the inner wall of the cylinder.

A rotating seal rotatable about a rotational axis is provided. The rotating seal includes a body having a first surface disposable to face the rotational axis and a second surface disposable to contact with a stationary element. The body defines a cooling channel including one or more entrance channels respectively extending from the first surface, one or more exit channels and a plenum. The plenum extends circumferentially through the body and has a hot side adjacent to the second surface. The plenum is fluidly interposed between the one or more entrance channels and the one or more exit channels whereby fluid exiting the one or more entrance channels and entering the plenum impinges against the hot side.

Described herein is a shaft seal system of a shaft supported in a bearing housing of a turbomachine. The shaft seal system includes a rotor-side seal arranged between the bearing housing and the shaft. Additionally, the shaft seal system includes an axial bearing supporting the shaft. Further, a gap is provided between a rotor-side thrust bearing surface of the axial bearing and an opposite surface of the shaft. A gap width of the gap is adjustable as a function of rotation speed of the shaft.

Aspects of the disclosure are directed to a sealing system for an engine having an axial centerline, comprising: a stationary carbon segment, and a seal plate that rotates when the engine is operated, where the seal plate includes an end face that is opposed to an interface between the carbon segment and the seal plate, and where the end face includes at least one groove that conveys a liquid cooling fluid.

Oil slinger systems include a seal runner comprising an annular radial member having a radius (R) and an outer axially extending member having an axial length (L), wherein a proximal surface of the outer axially extending member comprising a plurality of helical grooves. Methods of radial convective cooling include pumping a cooling liquid through the oil slinger system and convectively cooling the oil slinger.

The invention relates to a planetary gear box having at least one seal system, which has at least one rectangular-section sealing ring, which is arranged in a groove device, wherein the at least one rectangular-section sealing ring rests at least partially against a groove flank of the groove device, and the groove flank has profiling between the groove flank and the rectangular-section sealing ring for the purpose of distributing fluid, in particular oil, applied to the seal system, wherein the at least one seal system is part of an oil supply of a planet carrier and the seal system has at least two rectangular-section sealing rings, which are spaced apart axially from one another and are arranged radially between a drive shaft of the planetary gear box and the planet carrier. The invention also relates to a gas turbine engine.