Elastically deformable retention prongs absorb energy from a detached vane while the platform limits aerodynamic discontinuities.
Non-axial lift from a rolled tip portion helps looped blades redirect fluid flow into axial thrust for more efficient propulsion.
Distributed electric propulsion replaces mechanical power transmission in tiltrotor aircraft, reducing weight and supporting control after an OEI event.
Articulated rods and segmented attachments distribute thrust isostatically, reducing attachment size, weight, and aerodynamic drag.
Fuel flow and electric power are modulated around requested output to avoid undesired clutch behavior and reduce wear in a hybrid aircraft power plant.
A spring-biased tab maintains contact between a leading-edge metal band and the hub to route lightning through a composite propeller.
Height-based edge-sweep ranges balance aerodynamic efficiency and mechanical strength across turbomachine architectures.
Dual pinion gears apply opposing forces to a ring gear, minimizing backlash in rotor blade pitch control during rapidly reversing forces.