Flight device with a lift-generating fuselage

Details Flight device with a lift-generating fuselage Flight device with a lift-generating fuselage

B - Operations, Transporting

64

C

B64C 1/00 (2006.01) B64C 3/10 (2006.01) B64C 39/00 (2006.01) B64C 39/10 (2006.01)

Patent

CA 2505013

The invention relates to an aircraft comprising a lift-producing fuselage (1) whose largest span (11) lies in the middle third (14) of the total length and whose horizontal projection progressively diminishes in the front third (13) and in the rear third (15). The aircraft also comprises two wings (2), whereby the surface of the projection of both wings represents, in a horizontal plane, less than thirty percent of the total lift surface, and the wings are located in the middle third (14) of the total length of the fuselage. The aircraft additionally comprises a horizontal tail unit (4) situated in the rear third of the fuselage. The aircraft has a shape similar to that of a fish.

L'invention concerne un aérodyne comprenant un fuselage porteur (1) dont la plus grande envergure (11) se situe dans le tiers central (14) de la longueur totale et dont le tracé s'effile progressivement dans le tiers avant (13) et dans le tiers arrière (15). L'aérodyne selon l'invention comprend également deux ailes (2), dont la projection dans un plan horizontal a une surface représentant moins de 30 % de la surface de portance totale et qui se trouvent au niveau du tiers central (14) de la longueur totale du fuselage, ainsi qu'un empennage horizontal (4) situé sur le tiers arrière du fuselage. L'aérodyne selon l'invention présente une analogie avec la forme d'un poisson.

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