Split type vertical take-off and landing fixed-wing unmanned aerial vehicle

Abstract

1. Name of the product in this design: Split-type vertical take-off and landing fixed-wing unmanned aerial vehicle. 2. Application of this design: for use in unmanned aerial vehicles (UAVs), specifically a detachable vertical take-off and landing fixed-wing UAV, which can be used in low- and medium-altitude operations such as reconnaissance, photography, monitoring, surveying, power line inspection, and logistics transportation. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design points: 3D diagram of the combined state 2. 5. Other situations requiring explanation: Component description: Component 1 is a multi-rotor UAV, and Component 2 is a fixed-wing UAV. The two are used in combination.

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