A rotor mounting assembly for a vertical take-off and landing aircraft includes a boom configured for mounting to a wing of the aircraft; a mount for mounting a rotor assembly, the mount connected to the boom at a joint and tiltable about the joint from a forward thrust orientation in which the rotor assembly can provide forward thrust for forward flight to a vertical thrust orientation in which the rotor assembly can provide vertical thrust for vertical take-off and landing and hover; a multi-link assembly extending from the boom to the mount; and a rotary actuator for actuating the multi-link assembly to control tilting of the mount.
SYSTEMS AND METHODS FOR CONTROLLING ROTOR TILT FOR A VERTICAL TAKE-OFF AND LANDING AIRCRAFT
SYSTEME UND VERFAHREN ZUR STEUERUNG DER ROTORNEIGUNG FÜR EIN SENKRECHT STARTENDES UND LANDENDES FLUGZEUG
SYSTÈMES ET PROCÉDÉS DE COMMANDE D'INCLINAISON DE ROTOR POUR AÉRONEF À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX
2024-04-17
Patent
Electronic Resource
English
SYSTEMS AND METHODS FOR CONTROLLING ROTOR TILT FOR A VERTICAL TAKE-OFF AND LANDING AIRCRAFT
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|SYSTEMS AND METHODS FOR CONTROLLING ROTOR TILT FOR A VERTICAL TAKE-OFF AND LANDING AIRCRAFT
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