A vertical take-off and landing aircraft is shown. The VTOL aircraft has a main wing comprising a left wing and a right wing configured as folding wings, and one or more of a foreplane, comprising a left canard and a right canard configured as folding wings, and/or a tailplane, comprising a left stabiliser and a right stabiliser configured as folding wings. Each one of the folding wings has a fixed inboard section and a folding outboard section. The folding outboard section is downwardly foldable to a landing condition to support the aircraft on a surface.
VTOL AIRCRAFT
SENKRECHTSTART- UND -LANDEFLUGZEUG
AÉRONEF ADAV
2021-01-27
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |