| 摘要 |
The Flying Vehicle of Inverse Sustentation (FVIS) is an air transport unit for passengers and cargo. The vehicle has vertical takeoff due to a main flow-generating unit which generates combustion gases that are directed toward a circled firm wing, to obtain the necessary sustentation to elevate the vehicle. The flow directed toward the wing is protected with a cover with the surrounding means. The horizontal displacement is obtained using secondary propulsion units.
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