Internal combustion engine with afterburner, venturi cooler and exhaust turbine

Claim 2

A process which comprises burning hydrocarbon fuel in an internal combustion chamber to generate exhaust gases, burning additional fuel with excess compressed air in a secondary combustion chamber, commingling said exhaust gases in said secondary combustion chamber with said burning additional fuel and air under superatmospheric pressure, imparting spiral rotating circulation to the commingled gases in said secondary combustion chamber by directing said exhaust gases through a means tangentially disposed in said secondary combustion chamber and passing said commingled gases through a zone of reduced cross-sectional area, introducing cool air under superatmospheric pressure into said commingled gases in said zone, thereafter passing said mixture of gases and air through a zone of enlarged cross-sectional area further to cool the mixture, directing said cooled mixture into a turbine, discharging substantially completely oxidized gaseous effluent from said turbine, and coupling said turbine to an air compressor from which said air under superatmospheric pressure is derived.

Claim 3

A power plant comprising a hydrocarbon-fueled internal combustion engine having a primary combustion chamber, said engine discharging hot exhaust gases during operation thereof, means defining a secondary combustion chamber of fixed volume having a tapering conical shape, means for delivering to said secondary combustion chamber hydrocarbon fuel and air under superatmospheric pressure centrally axially disposed with respect thereto, means for directing hot exhaust gases tangentially disposed in said secondary combustion chamber so as to impart a circular cyclonic rotation to said exhaust gases in said chamber thereby increasing their transit path therethrough, means defining an injection chamber in which hot gaseous products discharged from said secondary combustion chamber are commingled with further air under superatmospheric pressure and at a temperature below that of said hot gaseous products to form a final gaseous mixture of reduced temperature, a turbine, means for directing said final gaseous mixture into said turbine thereby causing rotation thereof, and means for withdrawing mechanical power from said internal combustion engine and from said turbine.

Claim 4

A power plant comprising a hydrocarbon-fueled internal combustion engine having a primary combustion chamber, said engine discharging hot exhaust gases during operation thereof, means defining a secondary combustion chamber of fixed volume having a tapering conical shape, means for delivering to said secondary combustion chamber hydrocarbon fuel and air under superatmospheric pressure centrally axially disposed with respect thereto, means for directing hot exhaust gases tangentially disposed in said secondary combustion chamber so as to impart a circular cyclonic rotation to said exhaust gases in said chamber thereby increasing their transit path therethrough, means defining an injection chamber in which hot gaseous products discharged from said secondary combustion chamber are commingled with further air under superatmospheric pressure and at a temperature below that of said hot gaseous products to form a final gaseous mixture of reduced temperature, a turbine, means for directing said final gaseous mixture into said turbine thereby causing rotation thereof, and means for withdrawing mechanical power from said internal combustion engine and from said turbine.

Claim 5

A power plant as set forth in claim 2 which includes an air compressor, driven by said internal combustion engine and by said turbine, for supplying said air to said secondary combustion chamber under superatmospheric pressure.

Claim 6

A power plant as set forth in claim 3 in which said injection chamber is a venturi and which includes an injection nozzle disposed at the discharge end of said secondary combustion chamber and in proximity to the throat of said venturi for injecting gases at superatmospheric pressure into admixture with air at superatmospheric pressure from said compressor.

Claim 7

A power plant as set forth in claim 3 which includes a cooling and expansion chamber disposed between said injection chamber and said turbine.

Claim 8

A power plant as set forth in claim 3, including means for injecting alkaline aqueous coolant disposed near the outer periphery of the secondary combustion chamber.