B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 29/00 (2006.01) B64C 27/28 (2006.01)
Patent
CA 2255602
The invention discloses an aerodyne featuring vertical take-off and landing, comprising a fuselage (11) with a front end (12) and a rear end (16); a wing (19) mounted on the rear end and supported above the same; a horizontal stabilizer (40) mounted on the front end; two opposite arms (27, 29) which extend laterally relative to the fuselage between the wing and the horizontal tail unit; each arm comprising a distal end with respect to the fuselage, on which is pivotedly mounted a propeller pod (33) bearing a propeller (37) having a rotation axis; and driving means (17) to drive the propellers (37); each propeller being capable of pivoting between a first position in which its rotation axis is approximately horizontal, and a second position in which its rotation axis is approximately vertical.
L'invention concerne un aérodyne à décollage et atterrissage verticaux, comprenant un fuselage (11) comportant une extrémité avant (12) et une extrémité arrière (16); une aile (19) montée sur l'extrémité arrière et supportée au-dessus de celle-ci; un empennage horizontal (40) monté sur l'extrémité avant; deux bras opposés (27, 29) qui s'étendent latéralement par rapport au fuselage entre l'aile et l'empennage horizontal; chaque bras comportant une extrémité distale par rapport au fuselage, sur laquelle est montée de manière pivotante une nacelle d'hélice (33) portant une hélice (37) qui possède un axe de rotation; et des moyens moteurs (17) destinés à entraîner les hélices (37); chaque hélice étant apte à pivoter entre une première position dans laquelle son axe de rotation est appproximativement horizontal, et une seconde position dans laquelle son axe de rotation est appproximativement vertical.
Robic
Soulez-Lariviere Jean
LandOfFree
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