B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 17/06 (2006.01) B64C 15/00 (2006.01) B64C 27/20 (2006.01) B64C 29/00 (2006.01) B64C 39/06 (2006.01)
Patent
CA 2638591
An aircraft has a generally circular main body including an upper surface portion supported for rotation about a central passenger compartment to produce a gyroscopic effect on the aircraft. The rotatable upper surface portion includes viewable panes therein arranged to provide visibility therethrough from the central passenger compartment to an exterior of the main body. An engine communicates between a central inlet opening in the upper surface portion and an exhaust opening in the bottom of the main body to provide upward thrust to the aircraft.
L'appareil est généralement composé d'une structure principale circulaire comprenant une partie de la face supérieure supportée pour la rotation autour d'un compartiment passager central afin de produire un effet gyroscopique sur l'aéronef. La partie de la face supérieure rotative comprend des carreaux de fenêtre disposés de façon à offrir une visibilité de l'intérieur du compartiment passagers central vers l'extérieur de la structure principale. Un moteur se trouve entre un orifice d'admission central, situé sur la partie de la face supérieure, et un orifice d'échappement, situé au bas de la structure principale, afin de fournir la propulsion verticale de l'appareil.
Battison Williams Dupuis
Davidson Robert M.
LandOfFree
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