Fuel supply circuit for a combustion chamber of a turbomachine

The invention relates to a fuel supply circuit (1) for a combustion chamber (2) of a turbomachine (10), comprising: -a fuel supply pump (3) configured to provide a fuel flow at a predetermined flow rate, -a plurality of fuel injectors (4), and -a ramp (5) for connecting the pump (3) to the injectors...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	Keruzore, Nicolas Marie
Format:	Patent
Sprache:	eng
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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Beschreibung
Zusammenfassung:	The invention relates to a fuel supply circuit (1) for a combustion chamber (2) of a turbomachine (10), comprising: -a fuel supply pump (3) configured to provide a fuel flow at a predetermined flow rate, -a plurality of fuel injectors (4), and -a ramp (5) for connecting the pump (3) to the injectors (4), said circuit further comprising a device for the heat treatment of the fuel (6), having a chamber (60) connected to a fuel inlet (61) linked to the pump (3) and to a fuel outlet (62) linked to the ramp (5), wherein heating elements (60) are located in said chamber and are configured to heat the fuel flow to a predetermined temperature so as to cause coking of the fuel within the chamber (60) of the device (6).