| KEYWORD |
Reduced order model on bladed discs of gas turbine
Tesi esterna in azienda
Parole chiave BLADED DISK DYNAMICS, TURBINE
Riferimenti DANIELE BOTTO
Gruppi di ricerca 11 - LAQ AerMec per componenti di turbine e compressori
Tipo tesi MASTER THESIS
Descrizione 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
Conoscenze richieste MS engineering students (energy, aerospace, mechanical or equivalent).
Knowledge in mechanical integrity issues.
Bonus: Finite Element Analysis and vibration mechanics.
Note Duration: 8 months
Location of the internship: Ansaldo Energia, via N. Lorenzi 8, Genova, Italy.
Scadenza validita proposta 09/03/2020
PROPONI LA TUA CANDIDATURA