A seal assembly component includes an annular body having a centerline, first and second axial ends spaced along the centerline, an inner circumferential surface, and an opposing outer circumferential surface. The inner surface defines a bore for receiving a shaft and is sized such that the body inner surface frictionally engages the shaft outer surface to couple the component with the shaft. At least three cavities extend axially from the body first axial end and are spaced circumferentially about the centerline. Each cavity is located adjacent to the bore so as to define a separate centering body portion between a radially innermost surface section of the cavity and an axially-extending centering surface section of the body inner circumferential surface located inwardly of the cavity. Any radial growth of each centering body portion is lesser than concurrent radial growth of remaining portions of the body during rotation of the shaft.

A magnetic seal assembly comprises a metallic annular wear seal. A magnetic seal has a magnetic annular body adjacent to and attracting the wear seal into contact against a contact face thereof. A retainer ring is connected to a surface to the magnetic seal, the retainer ring having a coefficient of thermal expansion different than a coefficient of thermal expansion of the annular body, the coefficient of thermal expansion of the retainer ring selected to constrain a thermal expansion of the annular body. A method for controlling a thermal expansion of a magnetic seal assembly is also provided.

A seal assembly (1) for use with a rotating machine that includes a rotating shaft (2) includes a mating ring (16) having a mating ring seal face (17) and a seal ring (14) defining an interior member having an axially extending annular surface and a radially extending seal ring seal face (15). The assembly also includes a first bellows (18) that urges the seal ring toward the mating ring. At least one of the mating and seal ring seal faces includes one or more grooves (202, 206, 210) or surface features formed thereon that cause a gas to be drawn between the mating ring and the seal ring due to relative rotation between the seal ring and the mating ring and form a gas layer between the mating ring and the seal ring that urges the seal ring away from the mating ring. The assembly also includes an annular seal ring shell (22, 24, 62) that keeps the faces flat during operation.

A mechanical seal includes a pair of seal rings that rotate relative to each other; and a retainer that holds the seal ring. The retainer includes an annular base portion, an annular holding portion that is externally fitted to an outer periphery of the seal ring, and an annular connection portion that connects the base portion and the annular holding portion in an axial direction, and an annular space partially surrounded by the base portion, the annular connection portion, and the annular holding portion is formed between the outer periphery of the seal ring and an inner periphery of the retainer. The retainer has a plurality of beams which are disposed in the annular space to connect the annular base portion and the annular holding portion.

A mechanical seal includes a pair of seal rings that rotate relative to each other; and a retainer that holds the seal ring. The retainer includes an annular base portion, an annular holding portion that is externally fitted to an outer periphery of the seal ring, and an annular connection portion that connects the base portion and the annular holding portion in an axial direction, and an annular space partially surrounded by the base portion, the annular connection portion, and the annular holding portion is formed between the outer periphery of the seal ring and an inner periphery of the retainer. The retainer has a plurality of beams which are disposed in the annular space to connect the annular base portion and the annular holding portion.

A seal assembly component includes an annular body having a centerline, first and second axial ends spaced along the centerline, an inner circumferential surface, and an opposing outer circumferential surface. The inner surface defines a bore for receiving a shaft and is sized such that the body inner surface frictionally engages the shaft outer surface to couple the component with the shaft. At least three cavities extend axially from the body first axial end and are spaced circumferentially about the centerline. Each cavity is located adjacent to the bore so as to define a separate centering body portion between a radially innermost surface section of the cavity and an axially-extending centering surface section of the body inner circumferential surface located inwardly of the cavity. Any radial growth of each centering body portion is lesser than concurrent radial growth of remaining portions of the body during rotation of the shaft.

A gas turbine engine component includes a static component, a seal body associated with the static component, the seal body having an end surface configured to face a rotating seal seat, and a damper positioned radially outward of the seal body. The damper includes a contact that engages the seal body to dampen radial movement of the seal body while accommodating axial movement of the seal body.

A gas turbine engine component includes a static component, a seal body associated with the static component, the seal body having an end surface configured to face a rotating seal seat, and a damper positioned radially outward of the seal body. The damper includes a contact that engages the seal body to dampen radial movement of the seal body while accommodating axial movement of the seal body.

A magnetic seal assembly comprises a metallic annular wear seal. A magnetic seal has a magnetic annular body adjacent to and attracting the wear seal into contact against a contact face thereof. A retainer ring is connected to a surface to the magnetic seal, the retainer ring having a coefficient of thermal expansion different than a coefficient of thermal expansion of the annular body, the coefficient of thermal expansion of the retainer ring selected to constrain a thermal expansion of the annular body. A method for controlling a thermal expansion of a magnetic seal assembly is also provided.

A seal assembly includes a fixed seal ring, and a rotary part having a rotary seal ring with a friction edge intended to slide against a counter-track of the fixed seal ring, a receptacle connected to a rotary shaft and provided with teeth intended to be housed inside cavities obtained in a collar of the rotary seal ring in order to drive the rotary seal ring into rotation, and a protection ring disposed around the collar and provided with recessed housings intended to be disposed inside the cavities of the collar and to house the teeth of the receptacle.