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Device for lifting and driving aerodyne during takeoff and vertical landing, has protection units provided on side of longitudinal airfoils and extending outside longitudinal airfoils with respect to carrying structure
Device for lifting and driving aerodyne during takeoff and vertical landing, has protection units provided on side of longitudinal airfoils and extending outside longitudinal airfoils with respect to carrying structure
The device has longitudinal airfoils (1) rectilinearly placed on two sides of a carrying structure (3) and extended approximately parallel to a rolling axis (X). The longitudinal airfoils are symmetrical to each other with respect to a plane that is defined by the rolling axis and a yaw axis. Multiple protection units (7) are provided on a side of the longitudinal airfoils and extended outside the longitudinal airfoils with respect to the carrying structure. Each protection unit comprises a cross section delimited by a plane that passes through the yaw axis.
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