Rotorcraft load factor enhancer

Details Rotorcraft load factor enhancer Rotorcraft load factor enhancer

B - Operations, Transporting

64

D

341/86, 341/88

B64D 31/06 (2006.01) G05D 1/08 (2006.01) H02P 23/00 (2006.01)

Patent

CA 1246717

- 12 - Rotorcraft Load Factor Enhancer Abstract Rotor speed is maintained at a reference speed by a closed-loop fuel control system. Load factor potential is enhanced by increasing the reference speed as a function of the helicopter pitch rate when undergoing positive pitch rate maneuvers.

458431

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