VARIABLE SPEED HYDRAULIC MOTOR DRIVEN FUEL SYSTEMS

In accordance with at least one aspect of this disclosure, a system (100), includes a fuel line (106) defining a fuel inlet (110) and a fuel outlet (112), configured to provide fuel from a fuel tank (102) to an engine (104). A boost pump (108), including a boost impeller (114), is disposed in the fu...

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Bibliographische Detailangaben
1. Verfasser:	GOY, Edward W
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	In accordance with at least one aspect of this disclosure, a system (100), includes a fuel line (106) defining a fuel inlet (110) and a fuel outlet (112), configured to provide fuel from a fuel tank (102) to an engine (104). A boost pump (108), including a boost impeller (114), is disposed in the fuel line (106) configured to drive fuel from the fuel inlet (110) to the fuel outlet (112) and operatively connected to the boost pump (108) via a drive shaft (119). The system includes a fluid line (118) defining a fluid inlet (120) and a fluid outlet (122), configured to provide fluid from a fluid source (124) to a fluid destination(126). A fluid turbine (128) is disposed in the fluid line (118) configured to alter a pressure of the fuel line (106) between the fuel inlet (110) and the fuel outlet (112).