B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 23/08 (2006.01) B64C 39/00 (2006.01)
Patent
CA 2263581
An aircraft lifting member (wing) comprises a crossflow rotor (2) formed of a core (4) having rotor vanes (5) mounted around it, disposed in a trough (3) at the front upper part of a wing-like body (1). Rotation of the rotor induces a downwardly and rearwardly directed airflow over the upper surface (6) of the wing-like body (1) generating both lift and thrust. The upper part of the rotor vane path projects above the upper surface (6) and the lift-generating member is open at the leading edge to expose the cross-flow rotor (2) to the incident airflow.
L'invention concerne un élément de sustentation d'avion (aile). Cet élément comprend un rotor à courant transversal (2) composé d'un noyau d'induit (4) sur lequel sont fixées des pales de rotor (5). Ce rotor est logé dans un évidement (3) au niveau de la partie supérieure avant du corps (1) de type aile. La rotation du rotor induit un écoulement dirigé vers le bas et vers l'arrière, sur la surface supérieure (6) du corps (1) de type aile, ce qui génère tant une sustentation qu'une poussée. La partie supérieure de la trajectoire de la pale de rotor se projette au-dessus de la surface supérieure (6) et l'élément générant une sustentation est ouvert au niveau du bord de tête pour exposer le rotor (2), à l'écoulement d'air incident.
Fanwing Limited
Norton Rose Or S.e.n.c.r.l. S.r.l./llp
Peebles Patrick
LandOfFree
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