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11 - LAQ AerMec per componenti di turbine e compressori

Reduced order model on bladed discs of gas turbine

azienda Thesis in external company    


keywords BLADED DISK DYNAMICS, TURBINE

Reference persons DANIELE BOTTO

Research Groups 11 - LAQ AerMec per componenti di turbine e compressori

Thesis type MASTER THESIS

Description The evaluation of the eigenfrequencies and modal shapes of a turbine blade is a fundamental step during the design phase. The possibility to have these preliminary results in the conceptual phase could be useful to select the best solution for the component, strongly reducing the development time of the project.
Reduced order model techniques will be applied to FE models of turbine blades in order to evaluate the modal response of the component, starting from preliminary geometries of the blade airfoils. In-house tools shall be used and implemented into the aero-loop of optimization to select the best solutions for the basic design phase of the component

Notes Duration: 8 months
Location of the internship: Ansaldo Energia, via N. Lorenzi 8, Genova, Italy.


Deadline 03/07/2021      PROPONI LA TUA CANDIDATURA




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