4. Fluid reaction surfaces (i.e., impellers)
  5. Sustained ancillary movement of rotary working member
  6. Lead-lag type rotor blade movement

Dewey H. Hodges

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Hingeless helicopter rotor with improved stability

Fluid reaction surfaces (i.e. – impellers) – Sustained ancillary movement of rotary working member – Lead-lag type rotor blade movement
Patent

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Real time missile guidance system

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
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Profile ID: LFUS-PAI-P-287072

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