Spindle-mounted mandrel panels reduce tool breakage and eliminate post-curing cutting by damping AFP vibrations.
Segmented pressing means resolve autoclave size limits by applying localized pressure to large thermoplastic blanks, avoiding global alignment complexity.
A pre-patterned layup kit uses a flexible carrier to index composite laminae for automated application.
Overlapping caul plates feature compliant edges that deform under pressure to form a continuous face across gaps between adjacent plates.
An internal support structure extends into a lightening cavity of the UAV foot stand to boost rigidity, preventing resonance with propeller vibrations.
Segmenting fuselage skins into composite modules reduces capital investment and factory space while increasing production rates.