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Preliminary results on passive eddy current damper technology for SSME turbomachinerySome preliminary results have been obtained for the dynamic response of a rotor operating over a speed range of 800 to 10,000 rpm. Amplitude frequency plots show the lateral vibratory response of an unbalanced rotor with and without external damping. The mode of damping is by means of eddy currents generated with 4 c shaped permanent magnets installed at the lower bearing of a vertically oriented rotor. The lower ball bearing and its damper assembly are totally immersed in liquid nitrogen at a temperature of -197 deg C (-320 deg F). These preliminary results for a referenced or base line passive eddy current damper assembly show that the amplitude of synchronous vibration is reduced at the resonant frequency. Measured damping coefficients were calculated to phi = .086; this compares with a theoretically calculated value of phi = .079.
Document ID
19850018579
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cunningham, R. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: NASA. Marshall Space Flight Center Advan. High Pressure O2(H2 Technol.
Subject Category
Mechanical Engineering
Accession Number
85N26890
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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