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Self-acting geometry for noncontact sealsPerformance ot two self acting seal designs for a liquid oxygen (LOX) turbopump was predicted over ranges of pressure differential and speed. Predictions were compared with test results. Performance of a radial face seal for LOX was predicted up to 448 N/cu cm and 147 m/sec. Performance of a segmented circumferential seal for helium was predicted up to 69 N/cu cm and 189 m/sec. Results confirmed predictions of noncontact operation. Qualitative agreement between test and analysis was found. The LOX face seal evidently operated with mostly liquid in the self acting geometry and mostly gas across the dam.
Document ID
19810007957
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Allen, G. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-81659
E-473
Report Number: NASA-TM-81659
Report Number: E-473
Meeting Information
Meeting: Ann. Meeting of ASLE
Location: Pittsburgh, PA
Country: Untied States
Start Date: May 11, 1981
End Date: May 14, 1981
Accession Number
81N16474
Funding Number(s)
PROJECT: RTOP 505-32-42
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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