Advances in the case studies 2.2 and 2.3

INTEFIX unveils new developments in clamping of thin-walled curved workpieces and distortions in aeronautical structural parts corresponding to the cases studies 2.2 and 2.3 respectively.

Case study 2.2 deals with the reduction of deformation of the thin-walled aerospace part due to clamping forces whereas case study 2.3 focuses on the development of intelligent fixtures which can be applied to a wide range of aeronautical structural parts.