Landing and take-off assembly for vertical take-off and...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 29/02 (2006.01) B64C 27/22 (2006.01) B64F 1/12 (2006.01)

Patent

CA 2260960

An aircraft (12) adapted for flight in helicopter mode with its longitudinal axis oriented generally vertically and in airplane mode with its longitudinal axis oriented generally horizontally is provided with the capability of launching and landing with the tail end (202) directed skyward. The invention also includes improvements to the controllability and efficiency of aircraft (12) in helicopter mode provided by the stabilizer wings (24, 26, 28) and relative rotation of the fuselage section (14) about the aircract's longitudinal axis. The aircraft (12) may have an elongate boom (83) for engagement with a base structure (81). The base structure (81) may be attached to a building, a trailer transporter, a ship or some other structure.

Un aéronef (12) adapté pour le vol en mode hélicoptère avec son axe longitudinal orienté généralement verticalement et en mode avion avec son axe longitudinal orienté généralement horizontalement est doté de la fonction de décollage et d'atterrissage avec l'extrémité de queue (202) dirigée vers le ciel. L'invention concerne également des perfectionnements apportés à la manoeuvrabilité et au rendement de l'aéronef (12) en mode hélicoptère par l'intermédiaire d'ailes stabilisatrices (24, 26, 28) et par la rotation relative de la section (14) du fuselage autour de l'axe longitudinal de l'aéronef (12). Ce dernier peut posséder une flèche allongée (83) venant en prise avec une structure de base (81). Cette dernière peut être fixée à un immeuble, un véhicule transporteur à remorque, un navire ou une autre structure.

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