DELTA FUSELAGE FOR VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT

A vertical take-off and landing (VTOL) aircraft is provided. The aircraft includes a wing, nacelles supportively disposed at opposite ends of the wing, proprotors respectively attached to each of the nacelles with each of the proprotors being rotatable to generate lift in vertical flight and thrust...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Alber Mark R, Gayagoy Charles
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A vertical take-off and landing (VTOL) aircraft is provided. The aircraft includes a wing, nacelles supportively disposed at opposite ends of the wing, proprotors respectively attached to each of the nacelles with each of the proprotors being rotatable to generate lift in vertical flight and thrust in horizontal flight and a delta-wing shaped fuselage disposed along the wing between the nacelles.