Analytic Modeling of Floating Ring Annular Seals
Author:
Affiliation:
1. Institut Pprime, CNRS UPR3346, Université de Poitiers, 86962 Futuroscope Chasseneuil, France
2. SNECMA Space Engine Division, 27208 Vernon, France
3. Centre National d’Etudes Spatiales, 91023 Courcouronnes Evry, France
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.4004728/5894110/052507_1.pdf
Reference10 articles.
1. Leakage and Rotordynamic Analysis of a High Pressure Floating Ring Seal in the Turbo Pump Unit of a Liquid Rocket Engine;Ha;Tribol. Int.
2. Shapiro, W. , 2005, “Users’ Manual for Computer Code DYSEAL- Dynamic Response of Seals,” Report No. NASA/CR-2003-212368.
3. Transient Response of Floating Ring Liquid Seals;Kirk;J. Tribol.
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