Effervescent injector for an aeromechanical air/fuel injection system integrated into a gas turbine combustor

Effervescent injector for an aeromechanical air/fuel injection system integrated into a gas turbine combustor

The injector (2) has a tubular gas duct (16) arranged inside the fuel duct (6), with several orifices (18) opening out into fuel duct, to inject gas at a pressure greater than predetermined pressure and equal to pressure threshold so as to create effervescence in the fuel on being introduced into th...

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Bibliographische Detailangaben
Hauptverfasser: VASILEV, ALEXANDER JUR'EVICH, NOEL, THOMAS, ROLLIN, GILLES, YAGOGKIN, VICTOR IVANOVICH, FURLETOV, VICTOR IVANOVICH
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
BURNERS
COMBUSTION APPARATUS
COMBUSTION PROCESSES
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Beschreibung
Zusammenfassung:The injector (2) has a tubular gas duct (16) arranged inside the fuel duct (6), with several orifices (18) opening out into fuel duct, to inject gas at a pressure greater than predetermined pressure and equal to pressure threshold so as to create effervescence in the fuel on being introduced into the main structure (4). The orifices of the gas duct are arranged in at least one of the common transverse plane. Independent claims are also included for the following: (1) aeromechanical injection system; and (2) turbo machine.