Airbus Operations (s.a.s.)

Airbus France

Philippe Jimenez

Thierry Fol

Arnaud Namer

Stephanie Dantin

Ludovic Gerard

An aircraft including: a fuselage and two wings to which engine nacelles are attached and that are each connected laterally to the fuselage, one on each side thereof, by a central fairing. The central fairing includes, facing each wing, two opposed surfaces connected one to a suction face side and the other to a pressure face side of the wing and that extend longitudinally along the fuselage. At least one of the two surfaces includes at least one local geometric deformation configured to generate lateral aerodynamic disturbances on the central fairing toward the wing to control the flow of air over the wing.

Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations

An aircraft wing arrangement including a wing and at least one strut for attaching the aircraft engine suspended under the wing and including a front zone situated projecting towards the front with respect to a leading edge of the wing. The front zone includes a lateral projection delimiting a lateral air flow channel while being projected towards a proximal end of the wing.

Growing community of inventors

Toulouse, France

Philippe Jimenez