The Electric Vertical Takeoff and Landing Fixed-wing UAV (eVTOL FWUAV) represents a revolutionary fusion of aerodynamic principles, merging the vertical lift capabilities of multicopters with the efficient forward flight of fixed-wing aircraft into a single, electrically-powered platform. This hybrid configuration utilizes distributed electric propulsion systems, typically employing multiple lift-generating rotors for vertical ascent and transition, coupled with a primary forward-facing propeller for cruise flight, all integrated with conventional fixed-wing surfaces that provide lift during horizontal operation. The operational profile is distinctly phased: achieving vertical takeoff like a helicopter, transitioning in mid-air through complex aerodynamic maneuvers where lift generation shifts progressively from rotors to wings, cruising with the high efficiency characteristic of fixed-wing design, and finally executing a vertical landing. This synthesis delivers the decisive advantage of operating without runways, enabling deployment from confined urban environments, ship decks, or rugged terrain, while simultaneously achieving significantly greater range, endurance, and speed compared to purely rotary-wing UAVs. The technological core resides in advanced flight control algorithms that autonomously manage the inherently unstable transition phase, alongside sophisticated airframe designs that minimize weight and drag. These capabilities make eVTOL FWUAVs uniquely suited for applications requiring both flexible deployment and long-distance operation, such as long-range logistics and delivery, large-scale infrastructure inspection across linear assets like pipelines and power lines, precision agriculture for field surveying, and broad-area military reconnaissance and surveillance. As advancements in battery energy density, composite materials, and autonomous systems continue, eVTOL FWUAVs are poised to become a dominant paradigm in unmanned aviation, effectively bridging the critical performance gap between the versatile launch-and-recovery of rotary aircraft and the efficient cruise performance of fixed-wing platforms, thereby unlocking a new era of operational flexibility for commercial, industrial, and defense missions.
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VF20E电动垂直起降固定翼无人机
VF20E 无人机核心特性分析特性参数与解读型号VF20E机身长度1.8m翼展3.2m最大有效载荷5kg续航时间160分钟 (@3kg负载) / 120分钟 (@5kg负载)巡航速度78-90 km/h
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VF25E电动垂直起降固定翼无人机
VF25E 无人机核心特性分析特性参数与解读型号VF25E机身长度1.75m翼展3.6m最大有效载荷10kg续航时间150分钟 (@5kg负载) / 90分钟 (@10kg负载)巡航速度80-95 km/h
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VF-180P Electric Vertical Takeoff And Landing Fixed-wing UAV
VF180P 无人机核心特性分析特性参数与解读型号VF180P机身长度3970mm (约4米)翼展7336mm (约7.3米)最大有效载荷60kg续航时间8小时 (@40kg负载) / 4小时 (@60kg负载)巡航速度38 m/s (约 136.8 公里/小时)
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