NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Effect of support flexibilty and damping on the dynamic response of a single mass flexible rotor in elastic bearingsA steady state analysis of the shaft and the bearing housing motion was made by assuming synchronous precession of the system. The conditions under which the support system would act as a dynamic vibration absorber at the rotor critical speed were studied; plots of the rotor and support amplitudes, phase angles, and forces transmitted were evaluated by the computer, and the performance curves were automatically plotted by a CalComp plotter unit. Curves are presented on the optimization of the support housing characteristics to attenuate the rotor unbalance response over the entire rotor speed range. The complete transient motion including rotor unbalance was examined by integrating the equations of motion numerically using a modified fourth order Runge-Kutta procedure, and the resulting whirl orbits were plotted by the CalComp plotter unit. The results of the transient analysis are discussed with regards to the design optimization procedure derived from the steady-state analysis.
Document ID
19720020849
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kirk, R. G.
(Virginia Univ. Charlottesville, VA, United States)
Gunter, E. J.
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1972
Publication Information
Publisher: NASA
Subject Category
Machine Elements And Processes
Report/Patent Number
ME-4040-105-71U
NASA-CR-2083
Report Number: ME-4040-105-71U
Report Number: NASA-CR-2083
Accession Number
72N28499
Funding Number(s)
CONTRACT_GRANT: NGR-47-005-050
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available