Unmanned aerial vehicle for low-pressure hydrogen transport
View Patent ↗An unmanned aerial vehicle (UAV) for gas transport is disclosed. The UAV includes a fuselage enclosing a volume, and a gas reservoir enclosed within the fuselage, filling at least a majority of the volume. The gas reservoir is configured to receive and store a gas at a pressure no greater than 100 bar. The UAV also includes a propulsion system having at least one engine, each of the at least one engine coupled to a prop that is driven by the at least one engine using energy derived from the gas stored in the gas reservoir. The UAV also includes a control system communicatively coupled to the propulsion system and configured to operate the unmanned aerial vehicle to autonomously transport the gas. The UAV may have a footprint while on the ground, and the footprint of the UAV may be no larger than three standard parking spaces.
1. An unmanned aerial vehicle (UAV) for gas transport, comprising:
an airframe comprising a fuselage and a box wing, the fuselage being an airfoil enclosing a volume, wider than long, pointed upward while the UAV is on the ground, and pointed forward when the UAV is flying;
a gas reservoir comprising a plurality of tanks in fluid communication and enclosed within the fuselage, filling at least a majority of the volume, the gas reservoir configured to receive and store a gas at a pressure no greater than 30 bar, wherein the gas is hydrogen gas;
a propulsion system comprising a power generator and at least one engine, each of the at least one engine coupled to a prop that is driven by the at least one engine using electricity generated by the power generator from the gas stored in the gas reservoir, the power generator in fluid communication with the gas reservoir and communicatively coupled to the at least one engine, each prop having a rotational axis; and
a control system communicatively coupled to the propulsion system and configured to operate the unmanned aerial vehicle to autonomously transport the hydrogen gas;
wherein the UAV is a vertical take-off and landing (VTOL) aircraft;
wherein the box wing serves as the undercarriage of the UAV when the UAV is on the ground; and
wherein all prop rotational axes are parallel and fixed with respect to the fuselage.
2. The UAV of claim 1 , further comprising a gas interface for placing the gas reservoir in fluid communication with at least one of a user-end equipment and an on-site storage while the UAV is on the ground.
3. The UAV of claim 1 , wherein the power generator is communicatively coupled to an external electrical interface configured to provide electricity generated from the gas within the gas reservoir while the UAV is on the ground.
4. The UAV of claim 1 , wherein the power generator is a hydrogen-powered fuel cell.
5. The UAV of claim 1 , wherein the gas reservoir fills at least 85% of the volume of the fuselage.