| KEYWORD |
Innovative layout for a bladed-disk to be used in a Low Pressure turbine for aeronautical application, trade-off study and feasibility assessment
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 This activity will analyze different Air Flow layout which will possibly increase the design space on a LPT row on an Engine. This A/F will be evaluated from both a mechanics and aeromechanics point of view in order to perform a complete trade-off for the different design alternatives available.
Conoscenze richieste MS engineering students (energy, aerospace, mechanical or equivalent).
Bonus: Finite Element Analysis and vibration mechanics.
Note Duration: 8 months
Location of the internship: GE-AVIO
Scadenza validita proposta 09/03/2020
PROPONI LA TUA CANDIDATURA