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Pressure Actuated Leaf Seals for Improved Turbine Shaft SealingThis presentation introduces a shaft seal in which leaf seal elements are constructed from slotted shim material formed and layered into a frusto-conical assembly. Limited elastic deflection of seal leaves with increasing system pressure close large startup clearance to a small, non-contacting, steady state running clearance. At shutdown seal elements resiliently retract as differential seal pressure diminishes. Large seal clearance during startup and shutdown provides a mechanism for rub avoidance. Minimum operating clearance improves performance and non-contacting operation promises long seal life. Design features of this seal, sample calculations at differential pressures up to 2400 psid and benefit comparison with brush and labyrinth seals is documented in paper, AIAA 2005 3985, presented at the Advanced Seal Technology session of the Joint Propulsion Conference in Tucson this past July. In this presentation use of bimetallic leaf material will be discussed. Frictional heating of bimetallic leaf seals during a seal rub can relieve the rub condition to some extent with a change in seal shape. Improved leaf seal rub tolerance is expected with bimetallic material.
Document ID
20070002981
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Grondahl, Clayton
(CMG Tech, LLC Rexford, NY, United States)
Date Acquired
August 24, 2013
Publication Date
October 1, 2006
Publication Information
Publication: 2005 NASA Seal/Secondary Air System Workshop, Volume 1
Subject Category
Space Transportation And Safety
Distribution Limits
Public
Copyright
Public Use Permitted.
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