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SSME seal test program: Test results for smooth, hole-pattern and helically-grooved statorsAll of the listed seals were tested in a liquid Halon test facility at high Reynolds numbers. In addition, a helically-grooved-stator seal was tested in an air seal facility. An analysis of the test results with comparisons to theoretical predictions supports the following conclusions: (1) For small seals, the Hirs' friction-factor model is more restricted than had been thought; (2) For smooth seals, predictions of stiffness and damping improve markedly as the radical clearance is reduced; (3) Friction-factor data for hole-pattern-seal stators frequently deviates from the Hirs model; (4) Predictions of stiffness and damping coefficients for hole-pattern-stator seals is generally reasonable; (5) Tests for the hole-pattern stators at reduced clearances show no clear optimum for hole-pattern seals with respect to either hole-area ratio or hole depth to minimum clearance ratios; (6) Tests of these hole-pattern stators show no significant advantage in net damping over smooth seals; (7) Tests of helically-grooved seal stators in Halon show reasonable agreement between theory and prediction for leakage and direct stiffness but poor agreement for the net damping coefficient.
Document ID
19870016920
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Childs, Dara W.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Subject Category
Mechanical Engineering
Report/Patent Number
TRC-SEAL-7-87
NASA-CR-179126
NAS 1.26:179126
Report Number: TRC-SEAL-7-87
Report Number: NASA-CR-179126
Report Number: NAS 1.26:179126
Accession Number
87N26353
Funding Number(s)
CONTRACT_GRANT: NAS8-35824
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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