ANNULAR COMBUSTION CHAMBER FOR A GAS TURBINE ENGINE WITH A SINGLE ANNULAR ROW OF INTAKE OPENINGS FOR PRIMARY AND DILUTION AIR

摘要

A turbomachine combustion chamber including coaxial walls forming surfaces of revolution that include inlet orifices for admitting primary air and dilution air into the chamber, the orifices in each wall being substantially in alignment with one another along the longitudinal axis of the chamber and forming a single annular row of orifices.