Abstract: A fuel pump system for an aerial refueling system including: a variable displacement motor operable to be driven by a hydraulic fluid pressure; a fuel pump operable to be driven by the variable displacement motor; and a drive system controller (DSC) connected to the variable displacement motor, wherein the DSC is operable to direct an operation of the fuel pump in modes comprising: a flow control mode operable to maintain an output fuel flow rate from the fuel pump to a predetermined maximum inlet pressure at a reception coupling for a receiver aircraft; a fuel pressure control mode operable to regulate the output fuel flow rate to not exceed the predetermined maximum inlet pressure; and a priority mode operable to reduce the output fuel flow rate in response to a decrease in the hydraulic pressure. Also a method of refueling a receiver aircraft.

Abstract: A fuel pump system for an aerial refueling system including: a variable displacement motor operable to be driven by a hydraulic fluid pressure; a fuel pump operable to be driven by the variable displacement motor; and a drive system controller (DSC) connected to the variable displacement motor, wherein the DSC is operable to direct an operation of the fuel pump in modes comprising: a flow control mode operable to maintain an output fuel flow rate from the fuel pump to a predetermined maximum inlet pressure at a reception coupling for a receiver aircraft; a fuel pressure control mode operable to regulate the output fuel flow rate to not exceed the predetermined maximum inlet pressure; and a priority mode operable to reduce the output fuel flow rate in response to a decrease in the hydraulic pressure. Also a method of refueling a receiver aircraft.

Abstract: An apparatus comprising: a port cap operable to be coupled to a hydraulic motor/pump, the port cap comprising a first fluid port, a second fluid port and an access port; a first transducer coupled to the port cap through the first fluid port; a second transducer coupled to the port cap through the second fluid port; and a resolver coupled to the port cap through the access port, the resolver comprising a splined shaft to couple to an output shaft of the hydraulic motor/pump when the port cap is coupled to the hydraulic motor/pump. A system including a hydraulic motor/pump, a drive system controller and a port cap and a method of determining hose velocity, hose position, motor/pump torque and hose tension using data gathered at port cap.

Abstract: A fuel pump system for an aerial refueling system including: a variable displacement motor operable to be driven by a hydraulic fluid pressure; a fuel pump operable to be driven by the variable displacement motor; and a drive system controller (DSC) connected to the variable displacement motor, wherein the DSC is operable to direct an operation of the fuel pump in modes comprising: a flow control mode operable to maintain an output fuel flow rate from the fuel pump to a predetermined maximum inlet pressure at a reception coupling for a receiver aircraft; a fuel pressure control mode operable to regulate the output fuel flow rate to not exceed the predetermined maximum inlet pressure; and a priority mode operable to reduce the output fuel flow rate in response to a decrease in the hydraulic pressure. Also a method of refueling a receiver aircraft.

Abstract: Apparatuses and systems that use a variable displacement motor-pump (VDMP) to control the position and speed of a hose for an aerial refueling system are disclosed. At displacements greater than required to hold a position of the hose, the VDMP operates in a motor mode to retract the hose. For lesser displacements, the VDMP operates in a pump mode to control extension of the hose. In accordance with some embodiments, a pump-motor relief valve operates to throttle hydraulic fluid flow from the VDMP and to control mixing of hydraulic fluid flowing from the VDMP with system hydraulic fluid.

Abstract: Apparatuses and systems that use a variable displacement motor-pump (VDMP) to control the position of a hose of an aerial refueling system are disclosed. At VDMP displacements greater than required to hold a position of the hose, the VDMP operates in a motor mode to retract the hose. For lesser VDMP displacements, the VDMP operates in a pump mode to control extension of the hose. In accordance with some embodiments, a dual orifice conveys hydraulic fluid at varying rates depending upon the VDMP operational mode.

Abstract: Apparatuses and systems that use a variable displacement motor-pump (VDMP) to control the position and speed of a hose for an aerial refueling system are disclosed. At displacements greater than required to hold a position of the hose, the VDMP operates in a motor mode to retract the hose. For lesser displacements, the VDMP operates in a pump mode to control extension of the hose. In accordance with some embodiments, a pump-motor relief valve operates to throttle hydraulic fluid flow from the VDMP and to control mixing of hydraulic fluid flowing from the VDMP with system hydraulic fluid.

Abstract: Apparatuses and systems that use a variable displacement motor-pump (VDMP) to control the position of a hose of an aerial refueling system are disclosed. At VDMP displacements greater than required to hold a position of the hose, the VDMP operates in a motor mode to retract the hose. For lesser VDMP displacements, the VDMP operates in a pump mode to control extension of the hose. In accordance with some embodiments, a dual orifice conveys hydraulic fluid at varying rates depending upon the VDMP operational mode.

Abstract: In an aerial refueling system for refueling a receiver aircraft in flight from a tanker aircraft, wherein the refueling system includes a hose reel rotatably coupled to the tanker aircraft's fuselage, a hose wound around the reel, said hose having an outlet end, and a drogue affixed to said outlet end, a hose reel drive system including a microprocessor electrically coupled to the reel; and a machine-readable program embodied in the microprocessor for directing operation of the system, the machine-readable program including instructions for establishing a refueling range. A method including receiving information of a receiver aircraft for aerial refueling; and establishing, in flight, a refueling range for an aerial refueling system coupled to a tanker aircraft based on the received information.

Abstract: The invention is a variable displacement hydraulic motor-controlled hose reel drive system (10) for aerial refueling of a receiver aircraft from a tanker aircraft. The system includes a variable displacement hydraulic motor (26), a tachometer (34), position sensor (34), a reaction torque sensor (36) and a microprocessor (29) which, depending upon data received from the system's position and reaction torque sensors, sends appropriate signals to the motor. The invention is also a method for deploying a hose and drogue so as to reduce the likelihood that the hose (22) would go into oscillation after initial engagement of a receiver aircraft's probe with the drogue (24). In an embodiment of the invention, the hose (22) is retracted prior to hook up of the probe and drogue (24), and the force required to retract the hose (22) is recorded.

Abstract: The invention is a variable displacement hydraulic motor-controlled hose reel drive system for aerial refueling of a receiver aircraft from a tanker aircraft. The system includes a variable displacement hydraulic motor, a tachometer/position sensor, a reaction torque sensor and a microprocessor which, depending upon data received from the system's position and reaction torque sensors, sends appropriate signals to the motor. The invention is also a method for deploying a hose and drogue so as to reduce the likelihood that the hose would go into oscillation after initial engagement of a receiver aircraft's probe with the drogue. In an embodiment of the invention, the hose is retracted prior to hook up of the probe and drogue, and the force required to retract the hose is recorded. After initial engagement of the probe with the drogue, the hose is retracted until the force required to retract the hose rises to about the same force previously recorded.

Abstract: The invention is a method for engaging the drogue of a hose and drogue refueling system with the probe of a receiver aircraft for aerial refueling from a tanker aircraft. The tanker aircraft and receiver aircraft approximately match speed and direction, with the probe of the receiver aircraft maintained at approximately a first predetermined distance behind the tanker aircraft. The hose and drogue are extended rearward from the tanker aircraft so that the drogue is positioned at a second predetermined distance (shorter than the first predetermined distance) behind the tanker aircraft. The drogue and probe are orthogonally aligned with each other, and the hose is extended back beyond the second predetermined distance so that the drogue moves away from the tanker aircraft to and into engagement with the probe. The force of the air stream on the drogue is sufficient to provide for secure engagement of the drogue with the probe.

Abstract: The invention is a variable displacement hydraulic motorcontrolled hose reel drive system for aerial refueling of a receiver aircraft from a tanker aircraft. The system includes a variable displacement hydraulic motor, a tachometer/position sensor, a reaction torque sensor and a microprocessor which, depending upon data received from the system's position and reaction torque sensors, sends appropriate signals to the motor. The invention is also a method for deploying a hose and drogue so as to reduce the likelihood that the hose would go into oscillation after initial engagement of a receiver aircraft's probe with the drogue. In an embodiment of the invention, the hose is retracted prior to hook up of the probe and drogue, and the force required to retract the hose is recorded. After initial engagement of the probe with the drogue, the hose is retracted until the force required to retract the hose rises to about the same force previously recorded.

Abstract: The invention is a variable displacement hydraulic motor-controlled hose reel drive system. The system includes a variable displacement hydraulic motor, having an electro-hydraulic control valve; a tachometer/position sensor; a reaction torque sensor; and a microprocessor which, depending upon data received from the system's position and reaction torque sensors, sends appropriate signals to the electro-hydraulic control valve.