A mobile fuel monitoring system (MMU) is disclosed. The fuel monitoring system may be skid mounted and is configured to monitor fuel transfers between a fuel source and a vessel, such as a ship. The disclosed MMU is a stand-alone, self-contained unit that can be easily moved from place to place. The MMU is configured to monitor and remotely report custody transfers of fuel performed at any location. Parameters of the fuel transfer operation, such as the amount of fuel transferred, the flow rate, the fuel density, and fuel temperature can be monitored and alarms may be issued if any of the parameters are out of specification. The parameter values may be transmitted to a remote location, for example, via a satellite link.

A system for delivering a fluid to a fluid consuming asset having a fluid tank is disclosed. An inlet of a manifold is fluidically coupled to a storage tank that contains the fluid to be delivered. A first distal end of a fluid transporting mechanism is fluidically coupled to an outlet of the manifold. A second distal end of the fluid transporting mechanism is fluidically coupled to the fluid tank. A primary valve is fluidically coupled to the fluid transporting mechanism and restricts fluid flow to the fluid tank when fluid level in the fluid tank reaches a first fluid level threshold. A secondary valve is fluidically coupled to the fluid transporting mechanism and restricts fluid flow to the fluid tank when fluid level in the fluid tank reaches a second fluid level threshold. The first fluid level threshold is lower than the second fluid level threshold.

A system for delivering a fluid to a fluid consuming asset having a fluid tank is disclosed. An inlet of a manifold is fluidically coupled to a storage tank that contains the fluid to be delivered. A first distal end of a fluid transporting mechanism is fluidically coupled to an outlet of the manifold. A second distal end of the fluid transporting mechanism is fluidically coupled to the fluid tank. A primary valve is fluidically coupled to the fluid transporting mechanism and restricts fluid flow to the fluid tank when fluid level in the fluid tank reaches a first fluid level threshold. A secondary valve is fluidically coupled to the fluid transporting mechanism and restricts fluid flow to the fluid tank when fluid level in the fluid tank reaches a second fluid level threshold. The first fluid level threshold is lower than the second fluid level threshold.

Apparatus for delivering fluid to a fluid consuming asset having a fluid tank includes a tank operable to contain the fluid and a fluid delivery coupling fluidically coupling the tank to a manifold. A pressure relief valve is fluidically coupled to the manifold, disposed between the manifold and the tank, and coupled to the tank through a recirculation inlet. The pressure relief valve is set at a predetermined pressure threshold and opens when the back-pressure in the manifold exceeds that threshold. The fluid is directed to the tank through the recirculation inlet when the pressure relief valve opens. A fluid transporting mechanism is fluidically coupled to the manifold at a first distal end and a fill cap at a second distal end. The fill cap is coupled to an opening of the fluid tank and fluid can flow from the manifold to the fluid tank through the fluid transporting mechanism.

A device for refueling an aircraft, including a fuel flow duct, the downstream end of which is equipped with a wing coupler for connecting it to an inlet orifice of a fuel tank of the aircraft. The wing coupler includes a body, and a front valve that is movable with respect to the body. The wing coupler includes at least one detection member for detecting the position of the front valve, and an electrical or electronic transmission system for transmitting to a processing unit a signal representing the position of the front valve as detected by the at least one detection member.

A device for refueling an aircraft, including a fuel flow duct, the downstream end of which is equipped with a wing coupler for connecting it to an inlet orifice of a fuel tank of the aircraft. The wing coupler includes a body, and a front valve that is movable with respect to the body. The wing coupler includes at least one detection member for detecting the position of the front valve, and an electrical or electronic transmission system for transmitting to a processing unit a signal representing the position of the front valve as detected by the at least one detection member.

A fuel distribution system includes a fuel intake in communication with at least one fuel source that delivers a fuel through a fuel path. A filtering mechanism is positioned within the fuel path. A surge tank operates to maintain a minimum fluid pressure within the fuel path. A fuel manifold selectively delivers the fuel to a plurality of external fuel couplings. A flow meter monitors a flow of the fuel through the fuel manifold. The plurality of external fuel couplings are configured to contemporaneously deliver the fuel at a consistent flow rate.

A fuel distribution system includes a fuel intake in communication with at least one fuel source that delivers a fuel through a fuel path. A filtering mechanism is positioned within the fuel path. A surge tank operates to maintain a minimum fluid pressure within the fuel path. A fuel manifold selectively delivers the fuel to a plurality of external fuel couplings. A flow meter monitors a flow of the fuel through the fuel manifold. The plurality of external fuel couplings are configured to contemporaneously deliver the fuel at a consistent flow rate.

The invention relates to a fuel dispenser (1) comprising a hose storage space (2) adapted to accommodate at least one fuel hose (3), an electronic compartment (4) containing a main frame control unit (5), and a hydraulic compartment (6) containing fuel dispensing means (22) for dispensing fuel into a vehicle reservoir. According to the invention, the hydraulic control unit (7) is located inside the hydraulic compartment (6) and is electrically connected to the mainframe control unit (5) by a main electric cable means (17). The invention also relates to a method for handling a fuel dispenser (1).

The invention relates to a fuel dispenser (1) comprising a hose storage space (2) adapted to accommodate at least one fuel hose (3), an electronic compartment (4) containing a main frame control unit (5), and a hydraulic compartment (6) containing fuel dispensing means (22) for dispensing fuel into a vehicle reservoir. According to the invention, the hydraulic control unit (7) is located inside the hydraulic compartment (6) and is electrically connected to the mainframe control unit (5) by a main electric cable means (17). The invention also relates to a method for handling a fuel dispenser (1).