Invention Grant
US08167248B2 Aircraft comprising a device for reducing the induced drag 有权
飞行器包括用于减小诱发阻力的装置

Aircraft comprising a device for reducing the induced drag
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.
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