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US 2010/0059624 A1Published application
Aircraft comprising a device for reducing the induced drag
AssigneeAirbus France
InventorsThierry Fol, Majorie Defos
Life of this patent
Estimating the term…
Abstract
An aircraft including a longitudinal fuselage, at least two lateral wings connected symmetrically one on each side of the fuselage and at least one engine pod fixed to each lateral wing via an engine support pylon. At least one profiled bearing rod is positioned on each of the engine support pylons so as to generate a propulsive resultant force under action of an oblique air flow.
Claims10
1-9. (canceled)
An aircraft comprising:
- a longitudinal fuselage;
- at least two side wings connected symmetrically to opposite sides of the fuselage;
- at least one engine nacelle fixed to each side wing by an engine support pylon;
- and
- at least one profiled lifting member disposed on each of the engine support pylons, so as to generate a propulsive resultant force under action of an oblique air flow.
2 more elements
Dependencies are inferred from the claim text.