VF150P/Oil powered vertical takeoff and landing fixed-wing UAV

The VF150P unmanned aerial vehicle platform is a self-developed oil powered long endurance composite wing vertical takeoff and landing unmanned aerial vehicle by our company. It adopts a fixed wing combined with quadcopter composite wing overall layout, which solves the problem of vertical takeoff and landing of fixed wing unmanned aerial vehicles in a simple and reliable way. It combines the characteristics of long endurance, high speed, and long distance of fixed wing unmanned aerial vehicles with the vertical takeoff and landing function of rotary wing unmanned aerial vehicles. The vertical takeoff and landing mode greatly enhances the environmental adaptability of the modified unmanned aerial vehicle platform. This unmanned aerial vehicle platform can operate smoothly in complex terrain and densely populated areas such as mountains, hills, and jungles, greatly expanding the application range of unmanned aerial vehicles. It is an ideal choice for industrial grade unmanned aerial vehicles. The VF150P unmanned aerial vehicle platform is equipped with an industrial grade vertical takeoff and landing fixed wing flight control and navigation system, as well as professional aerial survey and inspection ground station software, which can ensure the autonomous flight of the unmanned aerial vehicle throughout the entire process, without the need for operator intervention to complete autonomous takeoff, flight state transition, autonomous cruising, autonomous landing and other flight stages. It also supports automatic route planning for 1000 waypoints and emergency alternate landing plans for 100 waypoints. This drone platform has the following characteristics and advantages: a) Practical and efficient: It has the characteristics of long endurance, fast speed, long distance, and large payload of fixed wing unmanned aerial vehicles; b) Vertical takeoff and landing: With the takeoff and landing mode of rotary wing unmanned aerial vehicles, it significantly reduces the requirements for takeoff and landing sites and airspace; c) Low cost of use: No need for complex and bulky launch and recovery equipment, no need to add additional recovery sensors; d) Easy to operate: Integrated with specialized flight control and navigation systems, fully autonomous flight throughout the entire process, operators only need to send flight plans, without the need for professional training or operational experience; e) Compact system: No need for complex auxiliary equipment, simple transportation, deployment, maintenance, and dismantling. Technical Parameter Performance/Indicator Parameters Body length 3270mm Wingspan 6935mm Body height 1307mm Maximum takeoff weight 150kg Maximum payload of 40kg Range time of 7h~10h (fuel consumption varies with different mounting and additional auxiliary fuel tank) Full load fuel consumption cruise stage: 4L/h, high power stage: 6L/h Flight radius 300km (depending on fuel capacity) Maximum speed 45m/s Cruise speed 35m/s Stall speed 27m/s Maximum fuel capacity 30L Limit up to 4500m Maximum wind resistance of 12m/s (level 6 wind) Operating environment -10 ℃+45 ℃; Prevent light rain Engine B2G290 (electronic fuel injection inspired integrated), 32 * 16 tail propeller blades Hanging/lowering power battery 12S-22000mAh * 4 lithium battery, series connected Vertical takeoff and landing method GPS positioning system RTK dual antenna