FUEL INJECTOR DEVICE FOR A TURBINE ENGINE

Fuel injection device for a turbine engine such as an airplane turboreactor, including a high-pressure pump (10), supplying the means (16) to control the flow whose output is connected by a pressurisation and cut-off valve (20) to a supply conduit (22) for the fuel injectors (18), the valve (20) bei...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BRETTES, FREDERIC, CAPPELLARI, JEAN CHARLES, HUET, SANDRINE, HODINOT, LAURENT GILBERT YVES
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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