MULTI-ELEMENT LIFTING SYSTEM WITH INTEGRATED PROPULSION AND AIRCRAFT USING SAME

A vertical take-off and landing aircraft with a multi-element lifting system with integrated propulsion. The multi-element lifting system may have an upper wing element, a lower wing element, and a control wing element which is located below the upper wing element and above, and rearward of, the low...

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Bibliographische Detailangaben
Hauptverfasser: BEVIRT, Joeben, MIKIC, Gregor
Format: Patent
Sprache:eng ; fre
Schlagworte:
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