| 摘要 |
An unmanned aerial vehicle 400 comprises a plurality of at least one type of fuel cell system component distributed about the vehicle. The fuel cell system component may be a fuel cell, a fuel cell generator, a coolant structure, a fuel reservoir or a reactant reservoir. The vehicle may be a rotor craft having a body 438 and a plurality of propulsion modules 440-443. The propulsion modules may be connected to the body by a plurality of struts 444-447. Each strut may include one or more of the fuel cell system components 452-455. |
