A distribution station includes a mobile trailer and a delivery system. The delivery system includes a pump, a manifold fluidly connected with the pump, reels, hoses, valves situated between the manifold and a respective different one of the hoses, and fluid level sensors. There is also an additive injector fluidly connected with the delivery system and operable to introduce controlled amounts of an additive into the delivery system.

A distribution station includes a mobile trailer and a delivery system. The delivery system includes a pump, a manifold fluidly connected with the pump, reels, hoses, valves situated between the manifold and a respective different one of the hoses, and fluid level sensors. There is also an additive injector fluidly connected with the delivery system and operable to introduce controlled amounts of an additive into the delivery system.

The present invention provides a smart and automated system that is used for refueling of frac truck tanks during fracturing operations. The system is used to refuel the frac truck tanks which are constantly working in the high pressure and high-temperature zone for the fracturing of the wellbore to extract oil and gas. For safety, the system is equipped with explosion/fire free wiring system. The system incorporates inventive fuel valve to avoid the fuel clogging that increases the frac truck performance. The system employs artificial intelligence (AI) and cloud-based software for ease of operation and to maximize economic performance. The system is equipped with artificial intelligence and Programmable Logic Controller (PLC) software and incorporates charge pump and loop systems which maintain a predetermined pressure (in Pounds per Square Inch (PSI) unit) in each loop so as to maximize the performance and control function in the refueling system.

A distribution station includes a mobile trailer and first and second pumps on the trailer. At least one manifold on the mobile trailer is fluidly connected with the first pump. A plurality of first reels on the mobile trailer are fluidly connected with the at least one manifold. A plurality of first hoses are connected with different ones of the first reels. A plurality of first valves on the mobile trailer are situated between the manifold and respective different ones of the first reels. A plurality of fluid level sensors are associated with different ones of the first hoses. A second reel is not fluidly connected with the manifold, and is fluidly connected with the second pump. A second hose is connected with the second reel that has a manual pump handle, and a controller is configured to individually open and close the valves responsive to the fluid level sensors.

A distribution station includes a mobile trailer and first and second pumps on the trailer. At least one manifold on the mobile trailer is fluidly connected with the first pump. A plurality of first reels on the mobile trailer are fluidly connected with the at least one manifold. A plurality of first hoses are connected with different ones of the first reels. A plurality of first valves on the mobile trailer are situated between the manifold and respective different ones of the first reels. A plurality of fluid level sensors are associated with different ones of the first hoses. A second reel is not fluidly connected with the manifold, and is fluidly connected with the second pump. A second hose is connected with the second reel that has a manual pump handle, and a controller is configured to individually open and close the valves responsive to the fluid level sensors.

A satellite refueling system has a refueling satellite carrying fuel, a fuel hose connected to the fuel carried by the refueling satellite, with a maneuverable end effector at a deployed end of the fuel hose, the end effector comprising a fuel supply nozzle connected to the fuel hose, a plurality of thrusters on the end effector providing thrust in a plurality of directions, an imaging device on the end effector capturing images in an immediate environment of the end effector, and computerized circuitry operating individual ones of the plurality of thrusters in response to the images captured by the imaging device. The refueling satellite deploys the fuel hose, and the computerized circuitry operates the thrusters to maneuver the end effector, bringing the fuel supply nozzle to a location to deliver fuel.

A satellite refueling system has a refueling satellite carrying fuel, a fuel hose connected to the fuel carried by the refueling satellite, with a maneuverable end effector at a deployed end of the fuel hose, the end effector comprising a fuel supply nozzle connected to the fuel hose, a plurality of thrusters on the end effector providing thrust in a plurality of directions, an imaging device on the end effector capturing images in an immediate environment of the end effector, and computerized circuitry operating individual ones of the plurality of thrusters in response to the images captured by the imaging device. The refueling satellite deploys the fuel hose, and the computerized circuitry operates the thrusters to maneuver the end effector, bringing the fuel supply nozzle to a location to deliver fuel.

An example fuel cap assembly includes a fuel cap, a sensor element extending from the fuel cap, and a fuel tube extending from the fuel cap next to the sensor element. The fuel tube includes an outlet end having at least one side-diverting fuel outlet that extends through a sidewall of the fuel tube. A fuel cap assembly kit and method of filling a fuel tank are also disclosed.

An ordnance delivery system has a cable deployable by a winch from an aircraft, an end effector comprising controllable thrusters attached at a deployed end of the cable, first control circuitry in the end effector and second control circuitry in the aircraft, the first and second control circuitry in communication, an ordinance delivery region in the end effector carrying ordnance for delivery on a target, and a release mechanism by which the ordnance is released to fall on the target. The aircraft is piloted to a position over a target, the end effector is controlled to position more accurately over the target; and the release mechanism is activated, releasing the ordnance to fall on the target.

An ordnance delivery system has a cable deployable by a winch from an aircraft, an end effector comprising controllable thrusters attached at a deployed end of the cable, first control circuitry in the end effector and second control circuitry in the aircraft, the first and second control circuitry in communication, an ordinance delivery region in the end effector carrying ordnance for delivery on a target, and a release mechanism by which the ordnance is released to fall on the target. The aircraft is piloted to a position over a target, the end effector is controlled to position more accurately over the target; and the release mechanism is activated, releasing the ordnance to fall on the target.