| abstract |
A hydrogen fuel cell drone according to the present invention comprises: a drone body in which a fuel cell stack for generating electricity by receiving hydrogen is disposed; a plurality of wing units receiving electricity from the fuel cell stack and generating lift for flight; and a plurality of frame combined hydrogen containers for storing hydrogen therein and supplying the hydrogen to the fuel cell stack, wherein the frame combined hydrogen containers are arranged to protrude radially at a predetermined distance along the outer periphery of the drone body, , characterized in that one end is connected to the drone body and the other end is connected to the wing unit. By using the present invention, the combined frame hydrogen container replaces the frame connecting the drone body and the wing, thereby eliminating the need for a separate frame and a separate hydrogen container, thereby remarkably reducing the total weight of the drone. |