Gas turbine engine with a multiple fuel delivery system

A multiple fuel delivery system (100) for use with a gas turbine engine includes a first fuel tank (110) with a first fuel (120) therein, a second fuel tank (170) with a second fuel (180) therein, a mixing chamber (130), and a flow divider (250) downstream of the mixing chamber. The first fuel tank...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	Fernandez, Paul Robert, Freeman, Thomas John, Scipio, Alston Ilford, Ekanayake, Sanji
Format:	Patent
Sprache:	eng ; fre ; ger
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A multiple fuel delivery system (100) for use with a gas turbine engine includes a first fuel tank (110) with a first fuel (120) therein, a second fuel tank (170) with a second fuel (180) therein, a mixing chamber (130), and a flow divider (250) downstream of the mixing chamber. The first fuel tank (110) may be in communication with the mixing chamber (130) via a first fuel pump (140) and the second fuel tank (170) may be in communication with the mixing chamber (130) via a second fuel pump (190).