A gasoline-electric hybrid vertical take-off and landing forward-swept fixed-wing unmanned aerial vehicle
An oil-electric hybrid, vertical take-off and landing technology, applied to vertical take-off and landing aircraft, unmanned aircraft, wings, etc., can solve problems such as ineffectiveness and disadvantages, and limit the total weight capacity of aircraft
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[0055] Aiming at the requirement of the unmanned aerial vehicle carrying capacity of "250 km round-trip, 700 km one-way 15 kg load", using the technical solution of "a kind of oil-electric hybrid vertical take-off and landing forward-swept fixed-wing unmanned aerial vehicle" provided by the present invention, specifically Design a technical scheme of a new type of cargo UAV as an example, the three views of its appearance are as attached Figure 1-Figure 3 shown
[0056] The fuselage assembly 1 is characterized by: including three parts, the front cabin 11 of the nose, the front fuselage 12 and the rear fuselage 13, and is used to connect other parts such as the wing assembly 2, the empennage assembly 3 and the vertical lift device assembly 4 of the drone. , and load all the systems, loads, fuel and batteries of the UAV.
[0057] Wherein the feature of nose front compartment 11 is: in the middle part of nose front compartment 11, two longitudinal trim electric ducted fan engi...
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