Air Riding Seal
AssigneeStein Seal Company
InventorsGlenn M. Garrison, Alan D. McNickle, Diane McNickle
Life of this patent
Estimating the term…
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AssigneeStein Seal Company
InventorsGlenn M. Garrison, Alan D. McNickle, Diane McNickle
Estimating the term…
An improved air-riding seal system for turbine engines is presented. The seal system includes a movable primary seal assembly, a stationary secondary seal assembly, and at least one structure to increase the stiffness of a thin film between the primary seal and a rotating component. The primary seal assembly includes an annular seal ring and an arcuate support arm. The annular seal ring has a cross section that is substantially L-shaped and a surface with a step face and a circumferential dam. The arcuate support arm has a tooth at one end adjacent to an outermost circumferential surface along the seal runner, which could include an optional notch. The tooth and outermost circumferential surface are separated by a gap. A plurality of radial dams disposed along the surface in an outward radial arrangement from the circumferential darn is provided to improve the stiffness of the thin film.
An air-riding seal system comprising:
An air-riding seal system comprising:
An air-riding seal system comprising:
An air-riding seal system comprising:
Dependencies are inferred from the claim text.