Nested coaxial driveshafts let multiple electric motors share one gearbox axis, shrinking propeller propulsion diameter to cut drag and fuel use.
A single electrohydraulic servovalve combines overspeed, feathering, and reverse control to cut propeller system weight and preserve engine efficiency.
A 3D-woven hollow composite root cuts blade mass while resisting traction, bending, and circumferential compression in variable pitch turboprops.
Retractable side rotors and a steerable counter-rotating tail propeller enable VTOL flight in tight urban areas while cutting drag and noise.
Spaced flange members and a crosswise support stiffen cantilevered stator vanes to handle bending loads in unducted turbofan airflow.
Varying stator blade chords around aerodynamic obstacles improves airflow straightening, limits local overload, and supports thrust efficiency.
A plies core reinforced by a composite wrap helps turbine airfoils stay lightweight while improving heat-region strength and impact resistance.
A releasable annular shroud lets pitch change components be removed and reassembled quickly while preserving kinematic adjustment.
A gimbal-linked rotor hub enables cyclic pitch control without a swashplate, cutting AMV rotor vibration and noise during takeoff and edgewise flight.
A balancing insert counteracts center-of-mass shift in a variable pitch airfoil assembly, reducing vibration stress and mechanical load.
Motor waste heat and redirected oil flow prevent ice on eVTOL propellers and air inlets without adding dedicated anti-icing weight or power.
A 3D woven hollow root with an inserted spar enables a compact rotationally symmetric propeller blade root that resists traction, bending, and compression.
A coaxial gearbox and hydraulic actuators fit variable-pitch fan control inside the hub, handling high loads in limited turbofan space.
A forward-extending movable slat boosts low-speed lift through gap airflow acceleration while cutting cruise drag in the same wing arrangement.
Variable fibre alignment follows blade curvature to cut laminate waste and improve blade spar mechanical properties.
Snap-fit capture walls and an alignment boss secure VTOL propellers in the correct orientation, reducing installation errors and detachment risk.
Transverse fiber layup improves head clearance on complex composite parts while supporting varied reinforcement angles and crease-free multilayer deposition.
Variable chord, twist, and offset along the blade span reduce pitch control loads at high speed while preserving hover and low-speed lift.
Fibre paths that follow blade spar curvature reduce laminate waste and improve mechanical properties in rotor blade manufacturing.