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11 - LAQ AerMec per componenti di turbine e compressori

Development of a methodology for Gearbox preliminary design and sizing considering dynamic 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 develop a methodology to optimize the gear geometries during preliminary design phase in order to achieve the desired dynamic behavior of the components (avoid resonances and minimize response amplitudes) leveraging on the available design space. The tool will then be applied on several different test- to assess the possible improvements and design feasibility on actual hardware.

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


Scadenza validita proposta 09/01/2020      PROPONI LA TUA CANDIDATURA




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