The present paper deals with the analysis of a crack that developed in a gearbox panel mounted on a cold planer machine. The crack was discovered after approximately 950 work hours, after that an oil leakage was detected: at that stage of propagation it was about 40 mm long. A research was therefore tackled to experimentally reproduce the history of load that had led to cracking and to estimate the local amount of stress and strain. For this purpose, a not cracked identical panel was instrumented by three-grid strain gauge rosettes. Then, an experimental campaign was arranged to reproduce loads during assembly and in operating conditions. In particular, the most critical and frequent task, obstacle overcoming, was simulated 16 times in about two hours time. The most interesting result was that stress has always an increasing trend during stepping up and stepping down. This event can be regarded as a mechanical hysteresis: the primary cause, standing in the selfloosening of two bolts connecting the panel to the machine frame, due to engine induced vibrations, was found out. The mechanism leading to failure was therefore identified, as testified also by the maximum principal stress direction being perpendicular to that of crack propagation. The crack criticality at the current propagation stage was finally discussed, estimating its stress intensity factor.

An experimental investigation on a crack propagating from a geartrain housing in an asphalt milling machine

OLMI, GIORGIO
2014

Abstract

The present paper deals with the analysis of a crack that developed in a gearbox panel mounted on a cold planer machine. The crack was discovered after approximately 950 work hours, after that an oil leakage was detected: at that stage of propagation it was about 40 mm long. A research was therefore tackled to experimentally reproduce the history of load that had led to cracking and to estimate the local amount of stress and strain. For this purpose, a not cracked identical panel was instrumented by three-grid strain gauge rosettes. Then, an experimental campaign was arranged to reproduce loads during assembly and in operating conditions. In particular, the most critical and frequent task, obstacle overcoming, was simulated 16 times in about two hours time. The most interesting result was that stress has always an increasing trend during stepping up and stepping down. This event can be regarded as a mechanical hysteresis: the primary cause, standing in the selfloosening of two bolts connecting the panel to the machine frame, due to engine induced vibrations, was found out. The mechanism leading to failure was therefore identified, as testified also by the maximum principal stress direction being perpendicular to that of crack propagation. The crack criticality at the current propagation stage was finally discussed, estimating its stress intensity factor.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11585/290115
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