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Preliminary experimental results for a cryogenic brush seal configurationPreliminary fluid nitrogen flow data are reported for a five-brush, ceramic-coated-rub-runner brush seal system, where the brushes and the rub runner were placed at each end of a centrally pressurized multifunction tester ('back-to-back' set of brushes) and tested at rotor speeds of 0, 10, 18, and 22.5 krpm. After testing, both the brushes and the ceramic-coated rub runner appeared pristine. The coating withstood both the thermomechanical and dynamic loadings with minor wear track scarring. The bristle tips showed some indication of material shearing (smearing) wear. The Ergun porous flow equation was applied to the brush seal data. The Ergun relation, which required heuristic information to characterize the coefficients, fit the gaseous data but was in poor agreement with the fluid results. The brush seal exit conditions were two phase. Two-phase, choked-flow design charts were applied but required one data point at each rotor speed to define the (C(sub f)A x Constant) flow and area coefficients. Reasonable agreement between prediction and data was found, as expected, but such methods are not to be construed as two-phase-flow brush seal analyses.
Document ID
19930019438
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carlile, J. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Hendricks, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Hibbs, R. I.
(Rockwell International Corp. Canoga Park, CA., United States)
Mcvey, S. E.
(Rockwell International Corp. Canoga Park, CA., United States)
Scharrer, J. K.
(Rockwell International Corp. Canoga Park, CA., United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:106236
E-7952
AIAA PAPER 93-2535
NASA-TM-106236
Meeting Information
Meeting: AIAA Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: AIAA, ASEE, ASME, SAE
Accession Number
93N28627
Funding Number(s)
PROJECT: RTOP 584-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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