- Description: Working on this rotor system design; following initial design
outlined in my patent; presented to DARPA who said it had merit but
felt pay off was not high enough for DOD. A few others were looking
it over. No word as of yet. Go figurer. A bit in left field. Its a
morphing (mechanical) airframe to control the rotor disc for
directional flight control. Effort to eliminate the angular
differences between retreating and advancing blades due to the
mechanical nature of swash plates when a helicopter with a
semi-rigid rotor system transitions from a hover into lateral
flight, requiring additional flight control manipulation to prevent
loss of lift in the direction of lateral flight.
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