Two-stroke uniflow turbo-compound internal combustion engine

1. A reciprocating two-stroke uniflow multiple cylinder internal combustion (IC) engine including a cylinder having a cylinder wall and a cylinder head, the cylinder head having an exhaust port, a fuel injector, and a spark means disposed through the cylinder head, a piston reciprocally mounted in the cylinder for movement alternately through compression and power strokes, and a scroll plenum extending unidirectional around the outside of the cylinder wall and having an inlet and a plurality of swirl ports disposed through the cylinder wall providing fluid communication from the scroll plenum into the cylinder chamber, wherein the plurality of swirl ports enter the cylinder chamber tangentially with respect to the axial centerline of the cylinder, and wherein the plurality of swirl ports are subject to opening and closing in response to movement of said piston.

2. The engine of claim 1 wherein the scroll plenum and the plurality of swirl ports extend substantially around the entire circumference of the cylinder wall.

3. The engine of claim 1 wherein the plurality of swirl ports are defined by a plurality of swirl vanes, each of the plurality of swirl vanes disposed at an angle tangential with respect to the axial centerline of the cylinder.

4. The engine of claim 1 wherein the lateral cross section of the scroll plenum reduces in area as the scroll plenum extends around the circumference of the cylinder wall.

5. The engine of claim 1 wherein the plurality of swirl ports are configured independently to provide the same mass rate of air at the same linear velocity therethrough.

6. The engine of claim 1 further including a high pressure air supercharger powered by an exhaust gas turbine.

7. The engine of claim 1 wherein the crown of the piston includes a plurality of auxiliary vanes extending radially to deflect scavenging air upward into the cylinder chamber.

8. The engine of claim 1 wherein the cross sectional shape of the plurality of swirl ports can include circular, oval, elliptical, rectalinear, and other polygonal.

9. The engine of claim 1 wherein the fuel injector injects the fuel in the downstream direction of the aforementioned swirl flow, and upstream of the spark ignitor, at a 10 to 30 degree angle with respect to the inside surface of the cylinder head.

10. The engine of claim 1 wherein the piston crowns and inside of cylinder heads include a thermal barrier coating (TBC) to reduce heat loss.

11. A reciprocating two-stroke uniflow internal combustion (IC) cylinder having a cylinder wall and a cylinder head, the cylinder head having an exhaust port, a fuel injector, and a spark plug disposed through the cylinder head, a piston reciprocally mounted in the cylinder for movement alternately through compression and power strokes, and a scroll plenum extending unidirectional around the outside of the cylinder wall and having an inlet and one or more swirl ports disposed through the cylinder wall providing fluid communication from the scroll plenum into the cylinder chamber, wherein the one or more swirl ports enter the cylinder chamber tangentially with respect to the axial centerline of the cylinder, and wherein the one or more swirl ports are subject to opening and closing in response to movement of said piston.

12. The engine of claim 11 wherein the crown of the piston includes a plurality of vanes having elongated sidewalls, extending radially from the center to proximate the edge of the crown.

13. A method for operating a reciprocating two-stroke uniflow multiple cylinder internal combustion (IC) engine including a high pressure supercharger inlet air system and a plurality of cylinders having a cylinder wall and a cylinder head, the cylinder head having an exhaust port, a fuel injector, and a spark ignitor disposed through the cylinder head, a piston reciprocally mounted in the cylinder for movement alternately through compression and power strokes, and a scroll plenum extending unidirectional around the outside of the cylinder wall and having an inlet and one or more swirl ports disposed through the cylinder wall and enter the cylinder chamber tangentially with respect to the axial centerline of the cylinder, and wherein the plurality of swirl ports are subject to opening and closing in response to movement of said piston, the method comprising the steps of:

a) passing high pressure inlet air through the scroll plenum and uncovered inlet ports and into the cylinder with the piston proximate the bottom of its reciprocal stroke within the cylinder, and swirling the inlet air in tangential turbulent unidirectional flow within the cylinder,

b) maintaining the exhaust port in an open position while the inlet air ports are uncovered to provide scavenging of the cylinder by the inlet air,

c) advancing the piston upward to cover the inlet ports,

d) closing the exhaust port,

e) compressing the inlet air between the piston and the cylinder head to a compression ratio of about 8:1 to about 12:1,

f) dispersing a fuel near the end of the compression stroke at a lean burning fuel to air ratio in the range of about 0.2 to about 0.8, the fuel being dispersed in the same tangential direction as the flow of the turbulent, swirling air, to obtain a stratified charge and intimate air-fuel mixing,

g) igniting and combusting the stratified charge of the air-fuel mixture to initiate the power stroke,

h) opening the exhaust value near the end of the power stroke to exhaust combustion gases, and

i) uncovering the inlet ports as the piston approaches the bottom of its power stroke.

14. The method of claim 13 , wherein the exhausting combustion gas drives an exhaust gas turbine that powers the supercharger.

15. The method of claim 14 , wherein the engine further includes a power turbine, and further includes the step of driving the low pressure exhaust turbine with the exhaust gas from the exhaust gas turbine to power the engine crankshaft.