or homogenization ultimately fuel passes through outlet 50 fig5 and into the combustion chamber 20 fig2 where an igniter 21 such as a spark plug ignites the processed fuel and a flame results which is held by the flame holder 22 heat is allowed to escape via apertures 52 formed in the cone shaped flame holder 22 the fuel air mixture passing through outlet 50 of the main fuel processing chamber 18 is moving in a vortical flow thus when the fuel air mixture passes into the combustion chamber 20 fig2 the fuel air mixture continues to flow in a vortical manner this vortical flow enhances combustion for a more efficient use of the fuel to be utilized by the turbine engine the vortical flow within the combustion chamber 20 ensures that the fuel air mixture continues to be broken down or atomized to the appropriate degree and that the fuel air mixture is circulated within the combustion chamber 20 for complete combustion with reference to fig2 the fuel processing apparatus and system 10 may be in one embodiment secured to a specialized housing 50 which envelopes the entire fuel processing system 10 a first flange 52 may be provided to allow the fuel processing system to be secured to any desired upstream mechanism such as a compressor a second flange 54 may be provided to secure the fuel processing system 10 to any appropriate downstream mechanism such as a turbine with reference to fig6 a turbine 60 is shown which.