Patent ID: 8833054

Claim:
A supersonic lean fuel combustion plasma arc turbine comprising: a plasma arc torch comprising: a cylindrical vessel having a first end and a second end, a tangential inlet connected to or proximate to the first end, a tangential outlet connected to or proximate to the second end, an electrode housing connected to the first end of the cylindrical vessel such that a first electrode is (a) aligned with a longitudinal axis of the cylindrical vessel, and (b) extends into the cylindrical vessel, a hollow electrode nozzle connected to the second end of the cylindrical vessel such that the center line of the hollow electrode nozzle is aligned with the longitudinal axis of the cylindrical vessel, and wherein the tangential inlet and the tangential outlet create a vortex within the cylindrical vessel, and the first electrode and the hollow electrode nozzle create a plasma that discharges through the hollow electrode nozzle; a cyclone combustor connected to the hollow electrode nozzle of the plasma arc torch, wherein the cyclone combustor has a tangential entry, a tangential exit, and an exhaust outlet; and a turbocharger having a turbine connected to a compressor via a shaft, wherein an turbine entry is connected to the tangential exit of the cyclone combustor, a compressor exit is connected to the tangential entry of the cyclone combustor.