ROTOR SEQUENCING FOR DUAL-ROTOR AIRCRAFT

An aircraft has a fuselage, a first rotor module having a first rotor hub and first rotor blades pivotably coupled to the first rotor hub and a second rotor module having a second rotor hub and secondrotor blades pivotably coupled to the second rotor hub. The first and second rotor blades have deplo...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: FRANK BRADLEY STAMPS, ERIC RICARDO GONZALEZ
Format: Patent
Sprache:chi ; eng
Schlagworte:
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