COMBUSTION CHAMBER FOR A TURBINE ENGINE WITH HOMOGENEOUS AIR INTAKE THROUGH FUEL-INJECTION SYSTEMS
The invention relates to a combustion chamber for a turbine engine, including an annular bottom wall (18) provided with injection systems (20) each centred on a respective axis (24) and each having an upstream end forming a socket (26') intended for receiving a head of a fuel injector, and an a...
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Sprache: | eng ; fre |
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