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Electronically Controlled Mechanical Seal for Aerospace Applications -- Part 1: Design, Analysis, and Steady State TestsAn electronically-controlled mechanial seal, for use as the purge gas seal in a liquid oxygen turbopump, has been designed, analyzed, and built. The thickness of the lubricating film between the faces is controlled by adjusting the coning of the carbon face. This is done by applying a voltage across a piezoelectric element to which the carbon face is bound. Steady state tests have shown that the leakage rate (and film thickness) can be adjusted over a substantial range, utilizing the available range of voltage.
Document ID
19950056894
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Salant, Richard F.
(Georgia Inst. of Tech., Atlanta, GA] United States)
Wolff, Paul
(Georgia Inst. of Tech., Atlanta, GA] United States)
Navon, Samuel
(Georgia Inst. of Tech., Atlanta, GA] United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1994
Publication Information
Publication: STLE Tribology Transactions
Volume: 37
Issue: 1
ISSN: 0569-8197
Subject Category
Mechanical Engineering
Accession Number
95A88493
Funding Number(s)
CONTRACT_GRANT: NAG3-974
Distribution Limits
Public
Copyright
Other

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