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Nonlinear analysis of rotor-bearing systems using component mode synthesisThe method of component mode synthesis is developed to determine the forced response of nonlinear, multishaft, rotor-bearing systems. The formulation allows for simulation of system response due to blade loss, distributed unbalance, base shock, maneuver loads, and specified fixed frame forces. The motion of each rotating component of the system is described by superposing constraint modes associated with boundary coordinates and constrained precessional modes associated with internal coordinates. The precessional modes are truncated for each component and the reduced component equations are assembled with the nonlinear supports and interconnections to form a set of nonlinear system equations of reduced order. These equations are then numerically integrated to obtain the system response. A computer program, which is presently restricted to single shaft systems, has been written and results are presented for transient system response associated with blade loss dynamics with squeeze film dampers, and with interference rubs.
Document ID
19820051933
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nelson, H. D.
(Arizona State Univ. Tempe, AZ, United States)
Meacham, W. L.
(Arizona State University Tempe, AZ, United States)
Fleming, D. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Kascak, A. F.
(U.S. Army, Propulsion Laboratory, Cleveland OH, United States)
Date Acquired
August 10, 2013
Publication Date
April 1, 1982
Subject Category
Mechanical Engineering
Report/Patent Number
ASME PAPER 82-GT-303
Meeting Information
Meeting: International Gas Turbine Conference and Exhibit
Location: London
Start Date: April 18, 1982
End Date: April 22, 1982
Sponsors: American Society of Mechanical Engineers
Accession Number
82A35468
Funding Number(s)
CONTRACT_GRANT: NAG3-6
Distribution Limits
Public
Copyright
Other

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