A hydrostatic advanced low leakage seal configured to be disposed between relatively rotatable components. The seal includes a base. The seal also includes a shoe extending circumferentially. The seal further includes a radially outer beam operatively coupling the shoe to the base. The seal yet further includes a radially inner beam operatively coupling the shoe to the base, wherein one of the radially inner beam and the radially outer beam is oriented to be angled relative to the other of the radially inner and outer beam.

A seal segment has an arcuate body having: a first end; a second end circumferentially opposite the first end; a first face; a second face axially opposite the first face; an inner diameter (ID) face; and an outer diameter (OD) face. The seal segment is shaped to interfit with a plurality of identical seal segments first end to second end to form a seal surrounding a central longitudinal axis. The first face has: a circumferential channel closer to the ID face than the OD face; and a plurality of channels extending from the circumferential channel to the OD face. The ID face has: a circumferential channel closer to the first face than the second face; and a plurality of channels extending from the circumferential channel to the second face. The ID face circumferential channel has an open end.

A tangentially cut rod packing ring is provided. The tangentially cut rod packing ring comprises a first ring formed from a plurality of segments. Each of the segments has a portion of two interfaces where each interface slidably engages an interface of an adjacent segment. One interface terminates at a leading surface. One interface has a stop surface. The leading surface is originally separated from the stop surface by a gap. As the interfaces slidably move, the gap lessens until the leading surface abuts the stop surface. The tangentially cut rod packing ring also comprises a second ring formed from a plurality of segments. The second ring has a first portion and a second portion. The first portion forms as shelf on which the first ring sits. The second portion surrounds the first ring. An elastic member in a groove on the outer surface of the second portion provides a compressive force on both the second ring and the first ring.

A clearance-control-type seal structure including a plurality of arc-shaped grooves (23) formed side by side in the axial direction with respect to an inner circumferential surface of a housing (22) of a turbine; and abradable seal rings (11, 12) having fitting parts (11a, 12a) that are fitted into the grooves so as to leave a prescribed gap, that have extended parts (11b, 12b) that are exposed from the housing in the radial direction toward the inside and expand in the axial direction, and that, during operation, due to back pressure inside the grooves, receive a force that moves in the radial direction toward the inside. One extended part has a protruding part extending even further in the axial direction toward the upstream side, and the other extended part has formed in an outer circumferential surface of a downstream-side end part thereof a recessed part that corresponds to the protruding part.

A circumferential seal assembly suitable for forming a thin film between a rotatable runner and a sealing ring is presented. The assembly includes an annular seal housing, a rotatable runner, an annular seal ring, and a plurality of groove structures. Each groove structure includes a groove and an optional feed groove. The groove includes at least two adjoining steps defined by base walls arranged to decrease depthwise. Two adjoining base walls are disposed about a base shoulder. Each base shoulder locally redirects a longitudinal flow to form an outward radial flow in the direction of the annular seal ring. The base walls are bounded by and intersect a pair of side walls. A side wall includes side shoulders which narrows the groove widthwise and locally redirects the longitudinal flow to form a lateral flow in the direction of the other side wall. Outward and lateral flows separately or in combination enhance stiffness of a thin-film layer between the annular seal ring and the rotatable runner.

An intershaft seal assembly for use between an inner shaft and an outer shaft rotatable within a turbine engine is presented. The seal assembly includes a sealing ring, an inner ring, and a pair of end rings. The sealing ring further includes a plurality of asymmetric ring segments whereby each asymmetric ring segment further includes a vertical flange and a pair of horizontal flanges extending from the vertical flange in a non-symmetric arrangement. The non-symmetric seal geometry provides an axial force balance thereby reducing wear and increasing seal life. The sealing ring is disposed about the inner ring. The inner ring includes a plurality of ridges that engage the asymmetric ring segments so as to prevent rotation of the asymmetric ring segments with respect to the inner shaft. The end rings are disposed about the sealing ring and the inner ring. The horizontal flanges separately contact the end rings so that the vertical flange extends from and between the end rings in the direction of the outer shaft. A non-contact seal is formed between an outer sealing surface along the vertical flange and an inner sealing surface along the outer shaft.

A seal assembly for a bearing housing is provided. The seal assembly may include a rotor seal member configured to be in sealing engagement with a rotary shaft. The seal assembly may also include a stator seal member formed from a plurality of stator seal member segments and configured to be in sealing engagement with the bearing housing. The stator seal member may also include an annular stator outer surface configured to be disposed on an inner surface of the bearing housing in sealing engagement therewith, and an annular stator inner surface radially opposing the annular stator outer surface and forming a first stator inner annular groove configured to receive the rotor seal member therein and form a sealing engagement therewith.

Aspects of the disclosure are directed to a seal comprising: a support ring, at least one beam coupled to the support ring, and a shoe coupled to the at least one beam, the shoe having an axial shoe face that includes a rounded edge that is configured to contact a support structure face of a support structure when the seal is subjected to a load that is equal to or greater than a first threshold.

A circumferential seal assembly for sealing about a rotatable shaft includes two or more generally arcuate bodies coupleable together to form a generally annular seal disposeable about a shaft outer surface. Each arcuate body has opposing female and male circumferential ends. Each female end includes a recess defined between a radially-inner arm and a radially-outer arm each extending generally circumferentially from a remainder of the arcuate body. Each male end includes a projection extending circumferentially from the remainder of the arcuate body and is sized to be disposeable within the recess of an adjacent arcuate body to couple the arcuate body with the adjacent arcuate body. Further, the female end inner arm of each arcuate body is disposed radially between the shaft outer surface and at least a portion of the male end projection of the adjacent arcuate body when the arcuate body is coupled with the adjacent arcuate body.

A seal assembly includes first and second generally annular seals disposable about the shaft so as to be spaced apart axially along the shaft central axis. Each seal has an inner circumferential sealing surface and inner and outer axial sides, each inner axial side facing the other seal inner axial side. The first seal has at one or more coupling pockets extending inwardly from the first seal inner axial side and the second seal has one or more retaining pockets extending inwardly from the second seal inner axial side, each retaining pocket being aligned with one coupling pocket. One or more biasing members each have a first end disposed within one coupling pocket and an opposing, second end disposed within one retaining pocket, the biasing member being configured to exert an axial biasing force on each one of the first and second seals.