NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Transient response of rotor-bearing systems.The equations of motion necessary to calculate the transient response of a multimass flexible rotor supported by nonlinear, damped bearings are derived from energy principles. Rotor excitation may be the result of imbalance, internal friction, rotor acceleration, nonlinear forces due to any number of bearing or seal stations, and gyroscopic couples developed from skewed disk effects. The method of solution for transient response simulation is discussed in detail and is based on extensive evaluation of numerical methods available for transient analysis. Examples of the application of transient response for the analysis of rotor bearing systems are presented and compared to actual machine performance. Recommendations for the use and extension of the present system simulation model are discussed.
Document ID
19730057277
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kirk, R. G.
(United Aircraft Corp. Pratt and Whitney Aircraft Div., East Hartford, Conn., United States)
Gunter, E. J.
(Virginia, University Charlottesville, Va., United States)
Date Acquired
August 7, 2013
Publication Date
September 1, 1973
Subject Category
Machine Elements And Processes
Report/Patent Number
ASME PAPER 73-DET-102
Report Number: ASME PAPER 73-DET-102
Accession Number
73A42079
Funding Number(s)
CONTRACT_GRANT: NGR-47-005-050
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available