A skew detection arrangement uses movable targets and sensors to monitor transition states for reliable position sensing.
A wing assembly high-lift body moves via a four-bar guide mechanism nested within the main wing contour.
Catch mechanism replaces roller arm in deflection control rib, removing flap cutouts that increase aerodynamic drag.
Segmented supply ducts and nested transfer tubes reduce thermal shielding requirements while extending anti-icing coverage.
Deflecting aerodynamic control surfaces deploys UAV wings using airflow forces, eliminating heavy actuators and improving payload capacity.
Semi-spherical inserts in the coupler compensate for geometric deviations between superposed surfaces, eliminating wedge grips and reducing assembly time.
Segmented swashplate actuator channels maintain stability during failures, reducing pilot workload and transient responses.