A tensioned inner rod inside a tubular outer rod adds fail-safe load bearing, fatigue tolerance, and visible failure checks in blade pitch control.
Gradual rotor speed reduction with backup engine support cuts rotorcraft noise in flight while preserving lift margin and stability.
Adjustable propeller blades increase drag-generated torque to preserve UAV controllability and enable safer landing after propulsion faults.
An elastic snap-fit hub lock keeps the propeller attached during speed changes and vibration while allowing tool-free removal after crashes.
A dual-cover airfoil uses rib-engaging corrugated coupling elements to resist shear loading and improve rotor blade fatigue life.
A threaded adjustable link helps tiltrotor blades shift to non-rotary flight, reducing aeroelastic instability and enabling higher cruise speed.
Closed-loop propeller speed and torque correction keeps a turboprop at efficient operating points across changing flight conditions.
A spring-biased sliding lock ring secures a threaded engine spinner or nosecone, then releases it without deformable lock hardware.
Ranks thrust vectoring, rotor speed, and aerosurfaces by control authority to stabilize hover and smooth VTOL-to-biplane transition.
Micro airfoil sensors and a pre-trained neural network detect stalls and vortex ring states early, enabling automatic control correction and lower power use.
A gimbaled rapid-connect nacelle combines battery, motor, and controls to speed aircraft assembly while enabling stable hover and VTOL transition.
Aircraft batteries mounted on elastic devices absorb rotor-induced vibration, cutting resonance without adding dead weight or extra hardware.
Counter-rotating propellers in airframe quadrants rebalance thrust after unit failure, limiting yaw torque and airframe stress.
Linear actuators adjust gimbal angle and blade pitch in UAV propulsion units to direct thrust precisely while also shaping noise output.
Antifriction interfaces and failure sensing help an anti-torque rotor maintain blade control when bearing damage causes twisting moments.
Aligned reinforcement fibers tailor fixture expansion to match composite parts, reducing tooling cost, distortion, and cure cycle time.
An elastic locking ring uses axial shaft motion to hold a retractable driveshaft without actuators, improving fail-safe wing engagement.
A resilient seal assembly closes the gap between hub and fixed rotor fairings to cut drag while allowing fairing removal without disturbing the seal.