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Damping seals for turbomachineryRotor whirl stabilization of high performance turbomachinery which operates at supercritical speed is discussed. Basic whirl driving forces are reviewed. Stabilization and criteria are discussed. Damping seals are offered as a solution to whirl and high vibration problems. Concept, advantages, retrofitting, and limits of damping seals are explained. Dynamic and leakage properties are shown to require a rough stator surface for stability and efficiency. Typical seal characteristics are given for the case of the high pressure oxidizer turbopump of the Space Shuttle. Ways of implementation and bearing load effects are discussed.
Document ID
19850018583
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vonpragenau, G. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: Advan. High Pressure O2(H2 Technol.
Subject Category
Mechanical Engineering
Accession Number
85N26894
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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