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  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 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 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.

Required skills MS engineering students (energy, aerospace, mechanical or equivalent).
Bonus: Finite Element Analysis and vibration mechanics.

Notes Duration: 8 months
Location of the internship: GE-AVIO


Deadline 09/03/2020      PROPONI LA TUA CANDIDATURA