Rotary-wing aircraft

Details Rotary-wing aircraft Rotary-wing aircraft

B - Operations, Transporting

64

C

B64C 27/08 (2006.01) B64D 47/08 (2006.01)

Patent

CA 2717810

The invention relates to a rotary-wing aircraft (100), comprising at least four rotors (110), which are disposed on girder elements (120a, 120b), wherein said rotors (110) and girder elements (120a, 120b) are disposed such that a free field of vision (S) is defined along a longitudinal axis (L) of said rotary-wing aircraft (100) at least between two terminal rotors.

L'invention concerne un aéronef à voilure tournante (100) comprenant au moins quatre rotors (110) disposés sur des éléments supports (120a, 120b), les rotors (110) et les éléments supports (120a, 120b) étant placés, de manière à ce qu'un champ visuel (S) libre soit défini au moins entre deux rotors situés aux extrémités, le long d'un axe longitudinal (L) de l'aéronef à voilure tournante (100).

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