초록 ▼

A method for operating an aircraft refueling system, where the aircraft refueling system has a computer system, a plurality of fuel tanks containing a fuel, a plurality of fuel pumps, a plurality of motor operated valves, and at least one refueling connection. The method may involve using the comput

A method for operating an aircraft refueling system, where the aircraft refueling system has a computer system, a plurality of fuel tanks containing a fuel, a plurality of fuel pumps, a plurality of motor operated valves, and at least one refueling connection. The method may involve using the computer system to signal at least one of the motor operated valves to open; initiating a flow of the fuel to the at least one of the refueling connections using at least one of the pumps; sensing a flow condition of the fuel; signaling the flow condition to the computer system; and varying an operating quantity of the pumps in response to the flow condition.

대표청구항 ▼

What is claimed is: 1. A method for operating an aircraft refueling system, the aircraft refueling system having a computer system, a plurality of fuel tanks containing a fuel, a plurality of fuel pumps, a plurality of motor operated valves, and at least one refueling connection, the method compris

What is claimed is: 1. A method for operating an aircraft refueling system, the aircraft refueling system having a computer system, a plurality of fuel tanks containing a fuel, a plurality of fuel pumps, a plurality of motor operated valves, and at least one refueling connection, the method comprising: using the computer system to signal at least one of the motor operated valves to open; initiating a flow of the fuel to the at least one of the refueling connections using at least one of the pumps; sensing a flow condition of the fuel; signaling the flow condition to the computer system; and varying an operating quantity of the pumps in response to the flow condition. 2. The method of claim 1, further comprising connecting the plurality of fuel tanks using a single wall manifold by operation of first ones of the valves. 3. The method of claim 2, further comprising joining individual ones of the fuel tanks located in manned spaces of an aircraft to the single wall manifold using a double wall pipe by opening second ones of the valves. 4. The method of claim 1, further comprising connecting a flow meter to the computer system prior to the signaling step. 5. The method of claim 1, further comprising further comprising connecting a pressure transducer to the computer system prior to the signaling step. 6. The method of claim 1, further comprising shutting off the at least one of the pumps upon completion of a refueling operation. 7. The method of claim 1, further comprising controlling a center of gravity of an aircraft by transferring the fuel into select ones of the fuel tanks.