TWO STAGE FUEL DELIVERY SYSTEM FOR AN AIRCRAFT

A two stage fuel delivery system for an aircraft includes a first stage pump including an inlet connected to a source of fuel and an outlet connected to a combustor assembly, and a second stage pump including an inlet portion connected to the source of fuel and an outlet portion connected to the com...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Susca, Ryan Prescott, Briggs, Eric, Stoicescu, Adrian L, Haugsjaahabink, Todd, LeDuc, Zachary Allen Ray, Mastrocola, Naison E, O'Rorke, Morgan
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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