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High temperature seal test rigThe High Temperature Seals Test Rig Program at NASA's Lewis Research Center is a joint effort involving three separate federal government agencies. Testing has been underway at Lewis in this test rig since April, 1993. The rig was designed to run tests at temperatures to 800 F at pressures to 200 psia or at temperatures to 1300 to 1500 F at pressures to 65 psia. It was designed to run at speeds of up to 50,000 rpm which, for a 5.1 inch diameter disk, is a surface speed of about 1100 ft./sec. The rig was designed to allow easy replacement of the disks as well as the seals such that different disk materials and coatings may be tested.
Document ID
19950007180
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Addy, Harold E., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Publication Information
Publication: Seals Flow Code Development 1993
Subject Category
Research And Support Facilities (Air)
Accession Number
95N13593
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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