CN CN121608552A
The invention discloses a three-in-one type electric vertical take-off and landing fixed-wing hovercar layout method, and belongs to the technical field of land-air dual-purpose vehicles. According to the method, the hovercar is decoupled into three independent modules, namely a special flight module, a general cabin module and an automatic driving ground module, which can be quickly separated and combined. The flight module adopts a high-aspect-ratio upper single-wing normal T-shaped tail fixed wing layout, integrates six sets of distributed electrically-driven tilting rotor units which are symmetrically arranged front and back in the wingspan direction, and has the vertical take-off and landing capability and the high-speed high-voyage cruise performance; the cabin module serves as a general manned unit and is provided with a standardized butt joint interface. The ground module is a wheel type automatic driving chassis. Through the modular design, the performance contradiction between flight and ground driving is solved, the flight speed exceeding 350 km/h and the voyage of 300 km or above are achieved, and high-order safety redundancy is provided through the distributed power unit. The invention provides an innovative solution for urban three-dimensional traffic in the future.
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