Modular drone with multi-configuration and multi-power systems

Abstract

A modular drone with multi-configuration and multi-propulsion systems has a main fuselage, a front fuselage, and a wing set. The main fuselage selectively has an electric stabilizer power module, or an internal combustion engine power module. The front fuselage is detachably mounted on the main fuselage via a connecting module. The wing set is detachably mounted on the main fuselage via the connecting module. Each one of the connecting modules has a protrusion, a recess, and a fixing member. When the protrusion protrudes in the recess, the fixing member is mounted through and fixes the protrusion and the recess. With the main fuselage, the front fuselage, the wing set, and the stabilizer set being connected via the connecting modules, the users may freely disassemble and reassemble the modular drone and select suitable components for rapid assembly.

Dependencies are inferred from the claim text.