Abstract
This paper presents an overall wind turbine model including a helical three stage gear system having twenty eight degree of freedom. First, the excitation of the model is induced by the periodic variation of the mesh stiffnesses and the aerodynamic forces are supposed constant. Then, the calculation of the dynamic response is performed by a step-by-step time integration method (Newmark method). Finally, the variation of the aerodynamic forces is introduced in the model. An analysis of the effects of these forces on the gear system dynamic behavior is then treated.
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Driss, Y., Abboudi, K., Bayaoui, M., Walha, L., Maatar, M., Haddar, M. (2012). Dynamic Behavior of an Aerodynamics Turbine Coupled to a Multiplier Helical Three-Stage Gear. In: Fakhfakh, T., Bartelmus, W., Chaari, F., Zimroz, R., Haddar, M. (eds) Condition Monitoring of Machinery in Non-Stationary Operations. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-28768-8_22
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DOI: https://doi.org/10.1007/978-3-642-28768-8_22
Publisher Name: Springer, Berlin, Heidelberg
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