THIS THESIS DEALS WITH THE DESIGN AND FATIGUE ANALYSIS OF A CRANKSHAFT, DESCRIBING THE PROCEDURES FOLLOWED STEP BY STEP. THIS THESIS AIMS TO IMPLEMENT AND VALIDATE AN INTEGRATED FEM-MULTIBODY CALCULATION METHODOLOGY ORIENTED TO THE DYNAMIC ANALYSIS AND FATIGUE VERIFICATION OF THE CRANKSHAFT OF AN ENDOTHERMIC ENGINE. IN ORDER TO OVERCOME THE COMPUTATIONAL LIMITATIONS OF INTEGRATED STRUCTURAL MODELS, ANSYS WAS USED, WHICH ALLOWED A DRAMATIC LIGHTENING OF THE MASS AND STIFFNESS MATRICES OF THE NATIVE STRUCTURE. THE RESULTS OBTAINED DEMONSTRATE A CLEAR CORRESPONDENCE WITH THE AVAILABLE REFERENCE DATA AND METHODOLOGIES. IN THE STRESS RECOVERY PHASE AND THANKS TO THE CALCULATION OF THE SAFETY COEFFICIENTS, THE MOST STRESSED AREAS WERE MAPPED, CONFIRMING THE EFFECTIVENESS OF THE DEVELOPED MODEL.
SI TRATTA LA PROGETTAZIONE E ANALISI A FATICA DI UN ALBERO MOTORE, DESCRIVENDONE PASSO PASSO I PROCEDIMENTI SEGUITI. IL PRESENTE LAVORO DI TESI SI PROPONE DI IMPLEMENTARE E VALIDARE UNA METODOLOGIA DI CALCOLO INTEGRATA FEM-MULTIBODY ORIENTATA ALL’ANALISI DINAMICA E ALLA VERIFICA A FATICA DELL’ALBERO MOTORE DI UN MOTORE ENDOTERMICO.AL FINE DI SUPERARE I LIMITI COMPUTAZIONALI DEI MODELLI STRUTTURALI INTEGRATI, E’ STATO USATO ANSYS, CHE HA PERMESSO DI ALLEGGERIRE DRASTICAMENTE LE MATRICI DI MASSA E RIGIDEZZA DELLA STRUTTURA NATIVA.I RISULTATI OTTENUTI DIMOSTRANO UNA NETTA CORRISPONDENZA CON I DATI E LE METODOLOGIE DI RIFERIMENTO DISPONIBILI. NELLA FASE DI STRESS RECOVERY E GRAZIE AL CALCOLO DEI COEFFICIENTI DI SICUREZZA SI SONO MAPPATE LE ZONE PIU SOLLECITATE, CONFERMANDO L’EFFICACCIA DEL MODELLO SVILUPPATO.
PROGETTAZIONE E ANALISI A FATICA DI UN ALBERO MOTORE
MASCIOPINTO, VITO
2025/2026
Abstract
THIS THESIS DEALS WITH THE DESIGN AND FATIGUE ANALYSIS OF A CRANKSHAFT, DESCRIBING THE PROCEDURES FOLLOWED STEP BY STEP. THIS THESIS AIMS TO IMPLEMENT AND VALIDATE AN INTEGRATED FEM-MULTIBODY CALCULATION METHODOLOGY ORIENTED TO THE DYNAMIC ANALYSIS AND FATIGUE VERIFICATION OF THE CRANKSHAFT OF AN ENDOTHERMIC ENGINE. IN ORDER TO OVERCOME THE COMPUTATIONAL LIMITATIONS OF INTEGRATED STRUCTURAL MODELS, ANSYS WAS USED, WHICH ALLOWED A DRAMATIC LIGHTENING OF THE MASS AND STIFFNESS MATRICES OF THE NATIVE STRUCTURE. THE RESULTS OBTAINED DEMONSTRATE A CLEAR CORRESPONDENCE WITH THE AVAILABLE REFERENCE DATA AND METHODOLOGIES. IN THE STRESS RECOVERY PHASE AND THANKS TO THE CALCULATION OF THE SAFETY COEFFICIENTS, THE MOST STRESSED AREAS WERE MAPPED, CONFIRMING THE EFFECTIVENESS OF THE DEVELOPED MODEL.I documenti in UNITESI sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
https://hdl.handle.net/20.500.14253/109540