Segmented rotor groups use asymmetrical balance to shape sound pressure levels and frequency spectrums, reducing component stress from vibration.
A separable helicopter rotor blade attachment uses a bolted junction and stiffened link to transfer centrifugal loads between the airfoil blade and flexbeam.
A rotorcraft generates an updraft by rotating blades at a negative pitch angle to supplement lift during vertical take-off.
Serially stacked swashplate assemblies enable independent pitch control of rotorcraft blades through concentric ring sections and sliding mechanisms.
A passive pitch adjustment apparatus uses levers and rods to rotate rotor blades via aerodynamic torsion moments.