A portable fuel metering system (PMU) is described. The PMU has one or more flow meters capable of metering the flow of fluids, such as fuel, as the fluid is transferred from a source to a receiver. The PMU may include a telemetry unit configured to transmit parameters related to the fuel transfer to remote location. The PMU may be configured in a light, portable package that may be carried by one or two people. The PMU may include a power generator that is configured to use the flow of fluid to the PMU to generate power for the PMU's operation.

A portable fuel metering system (PMU) is described. The PMU has one or more flow meters capable of metering the flow of fluids, such as fuel, as the fluid is transferred from a source to a receiver. The PMU may include a telemetry unit configured to transmit parameters related to the fuel transfer to remote location. The PMU may be configured in a light, portable package that may be carried by one or two people. The PMU may include a power generator that is configured to use the flow of fluid to the PMU to generate power for the PMU's operation.

System and method relates to a fuel control and distribution system comprising a fuel source, a fuel line, wherein the fuel source is connected to the fuel line, a fuel pump, wherein the fuel line is connected to the fuel pump, a main fuel line, wherein the fuel pump is connected to the main fuel line, a first remote transport truck, wherein the first remote transport truck comprises a first remote transport truck fuel line, wherein the main fuel line is connected to the first remote transport truck and wherein the first remote transport truck fuel line is connected to the first remote transport truck, a first tap line, wherein the first remote transport truck is connected to the first tap line, and a first fuel cap, wherein the first fuel cap comprises a first fuel level sensor, wherein the first tap line is connected to the first fuel cap and wherein the first fuel cap is adapted to be removably attached to a first equipment fuel tank.

A fluid dispensing nozzle including a nozzle body having a fluid path therein and a valve positioned in the fluid path and configured to selectively prevent or allow a flow of fluid through the fluid path. The nozzle further includes a manually operable actuator operatively connectable to the valve, a spout shell coupled to the nozzle body, and a fluid tube at least partially positioned in the spout shell and in fluid communication with or at least partially defining the fluid path. The nozzle further has a spacer at least partially positioned in the spout shell, a spout tip at least partially positioned in the spout shell, and a seal positioned between the spout tip and the spacer.

A fluid dispensing nozzle including a nozzle body having a fluid path therein and a valve positioned in the fluid path and configured to selectively prevent or allow a flow of fluid through the fluid path. The nozzle further includes a manually operable actuator operatively connectable to the valve, a spout shell coupled to the nozzle body, and a fluid tube at least partially positioned in the spout shell and in fluid communication with or at least partially defining the fluid path. The nozzle further has a spacer at least partially positioned in the spout shell, a spout tip at least partially positioned in the spout shell, and a seal positioned between the spout tip and the spacer.

A system delivering fire retardant materials in fighting a surface fire is provided, having an aircraft carrying the fire-retardant material, a hose deployable from the aircraft, the delivery hose connected to the reservoir and having a controllable nozzle at a deployed end with a remotely operable valve, an end effector connected by a multi-axis gimbal at the deployed end of the delivery hose the end effector having fixed wings with ailerons and elevators, and a rudder, the ailerons, elevators and rudder moved by electrical actuators, and control apparatus and circuitry in the aircraft and the end effector enabling an operator in manipulating the ailerons, elevators and the rudder. An operative in the aircraft controls the end effector via the control apparatus to fly at a lower altitude and in a different path than the aircraft, and opens the remotely operable valve to deliver the fire-retardant material from the delivery hose.

A system delivering fire retardant materials in fighting a surface fire is provided, having an aircraft carrying the fire-retardant material, a hose deployable from the aircraft, the delivery hose connected to the reservoir and having a controllable nozzle at a deployed end with a remotely operable valve, an end effector connected by a multi-axis gimbal at the deployed end of the delivery hose the end effector having fixed wings with ailerons and elevators, and a rudder, the ailerons, elevators and rudder moved by electrical actuators, and control apparatus and circuitry in the aircraft and the end effector enabling an operator in manipulating the ailerons, elevators and the rudder. An operative in the aircraft controls the end effector via the control apparatus to fly at a lower altitude and in a different path than the aircraft, and opens the remotely operable valve to deliver the fire-retardant material from the delivery hose.

A refueling system has a first vehicle having a fuel tank connected to a deployable fuel hose with a nozzle on the deployable end, a second vehicle carrying a supply of fuel, having a refueling panel with a refueling port adapted to connect to the nozzle on the deployed end of the fuel hose, an end effector joined to the fuel hose proximate the nozzle, the end effector having a plurality of thrusters providing thrust in a plurality of directions; and control circuitry in the first vehicle and in the end effector enabling an operative to vary direction and thrust of the thrusters. The operative controls the thrusters through the control circuitry to direct the nozzle toward and to connect the nozzle to the refueling port on the refueling panel of the second vehicle.

A refueling system has a first vehicle having a fuel tank connected to a deployable fuel hose with a nozzle on the deployable end, a second vehicle carrying a supply of fuel, having a refueling panel with a refueling port adapted to connect to the nozzle on the deployed end of the fuel hose, an end effector joined to the fuel hose proximate the nozzle, the end effector having a plurality of thrusters providing thrust in a plurality of directions; and control circuitry in the first vehicle and in the end effector enabling an operative to vary direction and thrust of the thrusters. The operative controls the thrusters through the control circuitry to direct the nozzle toward and to connect the nozzle to the refueling port on the refueling panel of the second vehicle.

A dispensing unit having a circulation system for circulating a fluid in the dispensing unit is provided. The circulation system comprises, a circulation circuit, and a mechanism configured to circulate the fluid in the circulation circuit. By circulating the fluid, the fluid is counteracted from crystallizing. A method for circulating a fluid in a dispensing unit is also provided.