The proposal approach innovative solutions for the design and manufacturing of the tooling needed for the assembly of two different kinds ofconfiguration for the outer wings within a Smart Fixed Wing Aircraft.

 

The PROUD proposal, understand that the main requirement for this wingstructural part is based on their high dimensional stability and tight geometrical tolerances to compliance with surface quality for a natural laminar flow condition, and therefore stability control and manufacturing precision over the integration tools to be designed and manufactured shall bestrict.

 

The proposal combines a skilled and qualified aeronautical tooling designers and manufacturers, within technology providers, for the specificsolutions in manufacturing and metrology for stress or deformation measurements.