Aerodynamic system for injecting an air-fuel mix

F - Mech Eng,Light,Heat,Weapons – 23 – R

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F23R 3/34 (2006.01) F23R 3/14 (2006.01)

Patent

CA 2207834

L'invention concerne un système d'injection aérodynamique d'un mélange air carburant dans un foyer de combustion (2) d'un moteur de turbine à gaz. L'injecteur de carburant (43) est à double débit et délivre un cône de carburant secondaire (53) au delà d'un régime donné. Un vrille primaire (32) et une vrille secondaire (33) sont associées à un venturi (30) en amont d'un bol aérodynamique (20) monté dans le fond de chambre (3). Le cône de carburant primaire (51) ne frappe pas le venturi (30).

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