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Self-acting geometry for noncontact sealsTwo hydrodynamic self-acting seal designs for a LOX turbopump were analyzed in order to predict performance. A radial face seal-to-seal LOX at 310 N/sq cm and 32,000 rpm (130 m/s) was analyzed for pressure differentials of 172 to 448 N/sq cm and speeds from 98 to 147 m/s. A segmented circumferential seal-to-seal helium at 34.5 or 69 N/sq cm and 157 m/s was analyzed for pressures of 35 to 86 N/sq cm (10 N/sq cm ambient) and speeds from 94 to 189 m/s. Test results confirmed noncontact operation near the design speed and pressure, and relatively good qualitative agreement between test and analysis. The face seal was found to operate with mostly liquid in the pads and mostly gas across the dam.
Document ID
19810049463
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Allen, G. P.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1981
Subject Category
Mechanical Engineering
Report/Patent Number
ASLE PREPRINT 81-AM-5B-2
Report Number: ASLE PREPRINT 81-AM-5B-2
Meeting Information
Meeting: Annual Meeting
Location: Pittsburgh, PA
Start Date: May 11, 1981
End Date: May 14, 1981
Sponsors: American Society of Lubrication Engineers
Accession Number
81A33867
Distribution Limits
Public
Copyright
Other

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