International audienceDistortions after machining of large aluminum forgings are a recurrent problem for the aeronautical industry. These deviations from design geometry are caused by the presence of residual stresses, which are developed along the manufacturing chain. To solve this problem, a series of post-machining operations called reshaping are required. Despite reshaping manages to restore the correct geometry, it is highly manual and time-consuming, therefore, there is a need at an industrial level to use numerical simulation to study reshaping. The present document describes the problem of distortion, the operations required to mitigate these geometrical defects and the challenges associated to simulate reshaping
International audienceLarge aeronautical parts present important distortions at the end of its manuf...
International audienceAluminium alloy structural aerospace parts are usually large monolithic parts ...
International audienceAeronautic parts have generally complex structure and need high mechanical pro...
International audienceDistortions after machining of large aluminum forgings are a recurrent problem...
International audienceDistortions after machining of large aluminum forgings are a recurrent problem...
Distortions after machining of large aluminum forgings are a recurrent problem for the aeronautical ...
Distortions after machining of large aluminum forgings are a recurrent problem for the aeronautical ...
The final publication is available at Springer via http://dx.doi.org/10.1007/s00170-020-05856-zLarge...
Distortions after machining of large aluminium forgings are a recurrent problem for the aeronautical...
Large aluminium monolithic parts used in the aeronautic industry frequently show significant geometr...
Large aeronautical structural parts present important distortions after machining. This problem is c...
Large aeronautical structural parts present important distortions after machining. This problem is c...
Large aeronautical structural parts present important distortions after machining. This problem is c...
International audienceLarge aeronautical structural parts present important distortions after machin...
International audienceAluminium alloy structural aerospace parts are usually large monolithic parts ...
International audienceLarge aeronautical parts present important distortions at the end of its manuf...
International audienceAluminium alloy structural aerospace parts are usually large monolithic parts ...
International audienceAeronautic parts have generally complex structure and need high mechanical pro...
International audienceDistortions after machining of large aluminum forgings are a recurrent problem...
International audienceDistortions after machining of large aluminum forgings are a recurrent problem...
Distortions after machining of large aluminum forgings are a recurrent problem for the aeronautical ...
Distortions after machining of large aluminum forgings are a recurrent problem for the aeronautical ...
The final publication is available at Springer via http://dx.doi.org/10.1007/s00170-020-05856-zLarge...
Distortions after machining of large aluminium forgings are a recurrent problem for the aeronautical...
Large aluminium monolithic parts used in the aeronautic industry frequently show significant geometr...
Large aeronautical structural parts present important distortions after machining. This problem is c...
Large aeronautical structural parts present important distortions after machining. This problem is c...
Large aeronautical structural parts present important distortions after machining. This problem is c...
International audienceLarge aeronautical structural parts present important distortions after machin...
International audienceAluminium alloy structural aerospace parts are usually large monolithic parts ...
International audienceLarge aeronautical parts present important distortions at the end of its manuf...
International audienceAluminium alloy structural aerospace parts are usually large monolithic parts ...
International audienceAeronautic parts have generally complex structure and need high mechanical pro...