Fuel pump driven by a variable displacement motor for aerial refueling operation
Fuel pump driven by a variable displacement motor for aerial refueling operation
- Neue Suche nach: BARTOV ASHER
- Neue Suche nach: LARSON GARY L
- Neue Suche nach: DELLER ROBERT W
- Neue Suche nach: BARTOV ASHER
- Neue Suche nach: LARSON GARY L
- Neue Suche nach: DELLER ROBERT W
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.
Dokumentinformationen
Fuel pump driven by a variable displacement motor for aerial refueling operation
2024-01-09
Patent
Elektronische Ressource
Englisch
| IPC: | F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F03C Verdrängerkraftmaschinen mit Flüssigkeitsantrieb , POSITIVE-DISPLACEMENT ENGINES DRIVEN BY LIQUIDS / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen |
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