The invention relates to an assembly (1) for an annular combustion chamber with a longitudinal axis (A) for a turbomachine comprising an annular wall at the bottom of the chamber (8) traversed by a plurality of fuel injectors (14) regularly distributed around the longitudinal axis (A) and connected to fuel supply means, characterized in that it comprises means for controlling individual means for controlling the fuel flow (28) of each injector (14).
展开▼
