Antipollution combustion chamber

Claim 1

A combustion device for a turbojet engine, comprising: an annular casing, the upstream part of said casing defining a diffuser for air issuing from a compressor, two annular, coaxial flame tubes, located in the casing, with their radial heights being approximately the same, while their axial lengths differ, each tube consisting of an internal annular wall and an external wall, secured at their upstream ends to a base upon which fuel injectors are mounted, the external wall of the inner tube and the internal wall of the outer tube being connected to form a junction at their downstream ends, the external wall of the outer tube and the internal wall of the inner tube extending past said junction to define a common dilution and mixing zone for the gaseous flows emanating from the two tubes, the axial length of the inner tube being sufficient to permit the achievement of combustion reactions prior to the entry of the gases in the common dilution and mixing zone, the injectors of the inner tube being mounted on the base of said tube by the intermediary of a flared member of less volume than the tube, a large number of small orifices being formed in said intermediate member, allowing the injection of a portion of the air necessary for combustion in the immediate vicinity of the injector, the outer tube having an axial length less than that of the inner tube with its base being located downstream with respect to the base of the inner tube, said common dilution and mixing zone having on the upstream part of its walls orifices regularly distributed in coplanar rows, effecting the injection of a flow of air to assure the homogenization of the gaseous flows emanating from the two tubes.