Rich catalytic injection
A gas turbine engine includes a compressor, a rich catalytic injector, a combustor, and a turbine. The rich catalytic injector includes a rich catalytic device, a mixing zone, and an injection assembly. The injection assembly provides an interface between the mixing zone and the combustor. The injection assembly can inject diffusion fuel into the combustor, provides flame aerodynamic stabilization in the combustor, and may include an ignition device.
1. A gas turbine engine comprising:
compressor;
a turbine operatively coupled to the compressor by a shaft assembly;
a combustor downstream of the compressor; and
a rich catalytic injector disposed between the compressor and the combustor, wherein the rich catalytic injector comprises a rich catalytic device, a mixing zone downstream of the rich catalytic device, and an injection assembly disposed between the mixing zone and the combustor, the injection assembly operatively coupling the mixing zone with the combustor, wherein the injection assembly includes a center body having an end cap to provide flow blockage and flow directing in a central inlet portion of the combustor, and wherein the center body is surrounded by the rich catalytic device and the mixing zone.
2. A gas turbine engine comprising:
compressor;
a turbine operatively coupled to the compressor by a shaft assembly;
a combustor downstream of the compressor; and
a rich catalytic injector disposed between the compressor and the combustor, wherein the rich catalytic injector comprises a rich catalytic device, a mixing zone downstream of the rich catalytic device, and an injection assembly disposed between the mixing zone and the combustor, the injection assembly operatively coupling the mixing zone with the combustor, wherein the injection assembly comprises a second mixing zone.
3. The gas turbine engine of claim 2 , wherein the second mixing zone comprises at least an air and fuel turning or swirl device and an air and fuel conveyance device.