Abstract: A compliant foil seal comprising at least one smooth resilient foil for facing a rotor and at least one bump foil for providing film riding stiffness and controlled deformation of the smooth resilient foil for providing an effective seal which is capable of operating reliably in the presence of large rotor excursions.

Abstract: A pressure balanced floating seal system positioned within a structure about a rotating shaft. The floating seal system has a cylindrical outer seal housing having a cylindrical internal recessed region formed in the outer seal housing with a retaining flange extending into said internal recessed region. A cylindrical inner seal housing is positioned within the internal recessed region. The inner seal housing has an annular internal surface for accommodating the rotating shaft. Two sealing member retaining grooves are formed in the inner seal housing annular internal surface and a lubricant recess is formed between the two grooves. An intermediate seal is retained on the forward side of the inner seal housing forward face between the inner seal housing and the outer seal housing at the retaining flange. Sealing members are positioned in the sealing member retaining grooves at substantially the same radius as the intermediate seal.

Abstract: A seal which is arranged between a shaft and a casing opening and separates, from one another, two spaces at different pressures, with the exception of a residual annular gap which permits a slight leakage caused by a gap flow. The seal can replace prior seal types and only permits a very small leakage volume flow while being relatively uncomplicated in terms of components, assembly and maintenance. The seal includes a bush (13) tightly surrounding the shaft (2), having at least one grooves (14) in each of which is arranged, with slight axial clearance, an elastic annular element (15, 18, 20, 21, 23) split by a longitudinally extending gap (16, 17, 19). The pressure difference between axial end surfaces of the annular element(s) (15, 18, 20, 21, 23) urges the annular element(s) (15, 18, 20, 21, 23) into sealing contact with the casing opening (3) in such a way that the gap flow is guided via the annular gap between the groove(s) (14) and the annular element(s) (15, 18, 20, 21, 23).

Abstract: A lip type seal is provided with an outer ring part (31) which is tightly fitted to a seal installation part (12) of a housing (1); a seal main body (32) which is fixed to the outer ring part (31) and whose inner circumferential part extending in a bent state to the side of a sealed space (A) is sealably brought into slidable contact with an outer circumferential surface of a rotary shaft (2) inserted in the housing (1); a rear surface support plate (33) which is arranged on the rear side of the seal main body and whose outer circumferential part together with the seal main body (32) is fixed to the outer ring part (31); and a movable support plate (34) which is engaged movably in a radial direction between the seal main body (32) and the rear surface support plate (33) and whose inner diameter is clearance fitted to the outer circumferential surface of the rotary shaft (2).

Abstract: An improved rotary shaft seal assembly is disclosed herein. The seal assembly is disclosed in combination with an example of transmission components with which it may be used. The assembly provides a rotary seal for fluid flow between a stationary cylinder and a shaft which rotates within the cylinder. The shaft includes a porting groove and seal grooves on each side of the porting groove. The seal grooves each include a cast iron and a polymeric (such as Teflon®) seal which form seals between the shaft and cylinder on both sides of the porting groove.

Abstract: A seal is provided for an offshore fluid swivel to seal a gap passage (34) leading from a transfer chamber (20) to the environment, which uses pressured fluid to apply a variable pressure that pushes the seal tightly against a sealed surface (52) on one side of the gap passage. In one arrangement, a ring-shaped seal device includes a seal body (82) of largely U-shaped cross-section, with a base (84) and a pair of legs (86, 88) extending from opposite sides of the base, with the base and at least one leg sealing against walls of the cavity that holds the seal. A hose (90) lies between the two legs and against the base of the seal body, and pressured fluid of greater than chamber fluid pressure is applied to the hose to expand it and thereby push apart the legs of the seal body.

Abstract: A system for delivering a pressurized lubricant fluid from a stationary source to an interior of a drive shaft of a gas turbine engine which rotates at high speed and operates at high temperatures, includes a pair of axially spaced-apart seals that surround the shaft. The pressurized lubricant fluid is delivered to a radial passage defined between the seals. To ensure reliable operation under the high speed and high temperature conditions, the seals are constructed so that a film of the lubricant fluid is formed between the rotating shaft and the seals. The seals float on the film and wear is reduced. In order to minimize variations in the space between the seals and the shaft caused by changes in operating temperatures, each seal is surrounded by a control ring of material having a coefficient of expansion similar to the material of the shaft. The advantage is reliable delivery of lubricant to a shaft rotating at high speed in a high temperature environment.

Abstract: A configuration seals a leadthrough gap between a wall and a shaft which is passed through the wall and can be set in rotation relative to the wall. The configuration has a sealing ring through which the shaft can be passed as well as a holder that can be firmly connected to the wall and has a cylindrical recess and a groove opening into the recess. The groove has a first groove surface and a second groove surface, between which the sealing ring is held while leaving respective radial gaps as well as a chamber that surrounds the sealing ring and can be filled with oil. The radial gap at the first groove surface is blocked to prevent a throughflow of oil from the chamber. The configuration can be used in a sealing system for an electrical machine filled with hydrogen, in particular for a turbogenerator.

Abstract: A sealed bushing assembly adapted to permit a push rod to pass through an adapter isolating a pressurized chamber, formed by attaching a sleeve to said adapter, inserting a bushing, and crimping the end of said sleeve opposite said adapter to restrain said bushing.