PORTALE DELLA DIDATTICA

Ricerca CERCA
  KEYWORD

Innovative layout for a bladed-disk to be used in a Low Pressure turbine for aeronautical application, trade-off study and feasibility assessment

azienda 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