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Electrical Wiring Interconnection System for a compound fast rotorcraft

The aim is to perform the detailed design of equipment installation, design the harnesses and their content, perform the detailed design of these harnesses installation and anemometry installation, perform the detailed design of ADU structure, manufacture harnesses and ADU structure, assemble ADU, test, deliver and ensure the FAL and Flight Line support.
To be noted innovation on use of 270 V DC voltage for power supply and presence of an ESN (Electrical Structural Network).