B - Operations – Transporting – 64 – B
Patent
B - Operations, Transporting
64
B
B64B 1/06 (2006.01) B63H 5/125 (2006.01) B64B 1/30 (2006.01) B64B 1/32 (2006.01) B64C 11/02 (2006.01) B64C 27/28 (2006.01) B64C 27/52 (2006.01) B64C 29/00 (2006.01)
Patent
CA 2276876
An aircraft has a fuselage substantially designed as an aerostatic lifting body and combined lifting and propelling devices joined to the fuselage, provided with propellers and forming driving units which can tilt between a lifting position, in which the plane of rotation of the respective propeller is substantially horizontal and the driven shaft of the associated drive that drives the propeller shaft is substantially vertical, and a propelling position in which the plane of rotation of the respective propeller is substantially vertical and the driven shaft of the associated drive that drives the propeller shaft is substantially horizontal. The plane of rotation of the propeller can swivel around the driven shaft of the associated drive that drives the propeller shaft.
L'aéronef décrit comprend un fuselage en forme de corps aérostatique de sustentation et des dispositifs d'ascension et de propulsion combinés reliés de manière articulée au fuselage qui forment des unités de propulsion pourvues d'hélices et qui peuvent basculer entre une position d'ascension, dans laquelle le plan de rotation des hélices est sensiblement horizontal et l'arbre mené du mécanisme d'entraînement de l'arbre de l'hélice respective est sensiblement vertical, et une position de propulsion dans laquelle le plan de rotation des hélices est sensiblement vertical et l'arbre mené du mécanisme d'entraînement de l'arbre de l'hélice respective est sensiblement horizontal. Le plan de rotation des hélices peut pivoter tout autour de l'arbre mené du mécanisme d'entraînement de l'arbre de l'hélice respective.
Gowling Lafleur Henderson Llp
Kunkler Hermann
LandOfFree
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