AIRCRAFT ROTOR WITH DISCRETE FLAP HINGE

An aircraft rotor assembly has upper and lower hub plates adapted to be mounted to a central rotor mast for rotation therewith. A plurality of radial arms is connected to at least two flap bearings mounted between the hub plates and forming a discrete flap hinge, each flap hinge defining a flap axis...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: STAMPS, FRANK B, POPELKA, DAVID A, RAUBER, RICHARD E, TISDALE, PATRICK R, DONOVAN, TOM
Format: Patent
Sprache:eng ; fre
Schlagworte:
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