A radially offset mass on the actuator shaft raises wing tip inertia to lower flapping frequency, easing loads while improving flutter stability.
Redirecting high-pressure wingtip airflow rearward cuts trailing vortices and induced drag while struts preserve shield rigidity and low drag.
Asymmetrical hot air injection heats the nacelle air intake inner wall while limiting outer wall heat loss and frost buildup.
A single clutch arrests a foldable wing tip in both folded and extended positions, cutting wing weight, complexity, and maintenance.