| CPC B64U 10/16 (2023.01) [B64C 1/08 (2013.01); B64U 20/70 (2023.01); B64U 50/11 (2023.01); B64U 2101/60 (2023.01)] | 20 Claims |

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1. An unmanned aerial vehicle (UAV), comprising: a plurality of combustion engine modules, each combustion engine module including a respective helicopter blade propulsion system; a truss connecting and separating adjacent pairs of the combustion engine modules of the plurality of combustion engine modules, wherein each truss includes a plurality of truss chords, wherein at least one of the truss chords comprises a hollow interior portion therein configured to hold a fuel for at least one of the plurality of combustion engine modules; and a control system configured to allow a user to control the plurality of combustion engine modules and corresponding helicopter blade propulsion systems.
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