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  • MECHANICAL ENGINEERING  (2)
  • MACHINE ELEMENTS AND PROCESSES
  • 1990-1994  (2)
  • 1970-1974
  • 1991  (2)
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Keywords
  • MECHANICAL ENGINEERING  (2)
  • MACHINE ELEMENTS AND PROCESSES
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  • 1990-1994  (2)
  • 1970-1974
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  • 1
    Publication Date: 2011-08-19
    Description: The dynamic behavior of multistage gear transmission system, with the effects of gear-box-induced vibrations and rotor mass-imbalances is analyzed. The model method, using undamped frequencies and planar mode shapes, is used to reduce the degree-of-freedom of the system. The various rotor-bearing stages as well as lateral and torsional vibrations of each individual stage are coupled through localized gear-mesh-tooth interactions. Gear-box vibrations are coupled to the gear stage dynamics through bearing support forces. Transient and steady state dynamics of lateral and torsional vibrations of the geared system are examined in both time and frequency domain. A typical three-staged geared system is used as an example. Effects of mass-imbalance and gear box vibrations on the system dynamic behavior are presented in terms of modal excitation functions for both lateral and torsional vibrations. Operational characteristics and conclusions are drawn from the results presented.
    Keywords: MECHANICAL ENGINEERING
    Type: ASME, Transactions, Journal of Vibration and Acoustics (ISSN 0739-3717); 113; 333-344
    Format: text
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  • 2
    Publication Date: 2019-07-13
    Description: An analytical procedure to simulate vibrations in gear transmission systems is presented. This procedure couples the dynamics of the rotor-bearing gear system with the vibration in the gear box structure. The model synthesis method is used in solving the overall dynamics of the system, and a variable time-stepping integration scheme is used in evaluating the global transient vibration of the system. Locally each gear stage is modeled as a multimass rotor-bearing system using a discrete model. The modal characteristics are calculated using the matrix-transfer technique. The gearbox structure is represented by a finite element models, and modal parameters are solved by using NASTRAN. The rotor-gear stages are coupled through nonlinear compliance in the gear mesh while the gearbox structure is coupled through the bearing supports of the rotor system. Transient and steady state vibrations of the coupled system are examined in both time and frequency domains. A typical three-geared system is used as an example for demonstration of the developed procedure.
    Keywords: MECHANICAL ENGINEERING
    Type: NASA-TM-103797 , E-6085 , NAS 1.15:103797 , AVSCOM-TR-90-C-033 , International Conference on Motion and Power Transmissions; Nov 24, 1991 - Nov 26, 1991; Hiroshima; Japan
    Format: application/pdf
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