ENGINE HAVING FUEL INJECTION INDUCED COMBUSTION CHAMBER MIXING

• US 20110239982A1
• Filed: 04/01/2010
• Published: 10/06/2011
• Est. Priority Date: 04/01/2010
• Status: Active Grant

• Current Assignee: GM Global Technology Operations LLC (General Motors Company)
• Original Assignee: GM Global Technology Operations Incorporated (Motors Liquidation Co. GUC Trust)
• Inventors: Straub, Robert D.
• Granted Patent: US 8,402,940 B2
• Time in Patent Office: Days
• US Class Current: 123/306
• CPC Class Codes: F02B 2023/103 the injector having a multi-hole nozzle for generating multiple sprays
• CPC Class Codes: F02B 2023/108 Swirl flow, i.e. the axis of rotation of the main charge flow motion is vertical
• CPC Class Codes: F02B 2275/14 Direct injection into combustion chamber
• CPC Class Codes: F02B 23/0624 Swirl flow
• CPC Class Codes: F02B 23/066 the injector being located substantially off-set from the cylinder centre axis
• CPC Class Codes: F02B 23/0669 having multiple fuel spray jets per injector nozzle
• CPC Class Codes: F02B 23/104 the injector being placed on a side position of the cylinder
• CPC Class Codes: F02B 25/08 Engines with oppositely-moving reciprocating working pistons
• CPC Class Codes: F02M 61/08 the valves opening in direction of fuel flow F02M61/047 takes precedence
• CPC Class Codes: F02M 69/045 for injecting into the combustion chamber F02M69/046 takes precedence
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

An engine assembly may include an engine structure, a piston, and a direct injection fuel system. The engine structure may define a cylinder bore and the piston may be disposed within the cylinder bore for reciprocal displacement between a top dead center position and a bottom dead center position. The direct injection fuel system may include a fuel injector that provides a fuel spray to a combustion chamber defined by the piston and the cylinder bore. The fuel flow may extend generally tangential to a circumference of the combustion chamber and may define a centerline extending in a direction radially across the combustion chamber.

Claims

1. An engine assembly comprising:

an engine structure defining a cylinder bore;

a piston disposed within the cylinder bore for reciprocal displacement between a top dead center position and a bottom dead center position; and

a direct injection fuel system including a fuel injector that provides a fuel spray to a combustion chamber defined by the piston and the engine structure, the fuel spray extending generally tangential to a circumference of the combustion chamber and defining a centerline extending in a direction radially across the combustion chamber.

2. The engine assembly of claim 1, wherein the centerline of the fuel spray extends in a direction from a circumferential starting point on the circumference of the combustion chamber to a first circumferential ending point on the circumference of the combustion chamber, the first circumferential ending point being rotationally offset in a rotational direction from the circumferential starting point by less than or equal to 135 degrees along the circumference.

3. The engine assembly of claim 2, wherein the fuel spray includes a spray pattern defining an inner and outer radial periphery extending around the centerline, the outer radial periphery extending in a direction from the circumferential starting point to a second circumferential ending point on the circumference of the combustion chamber, the second circumferential ending point being rotationally offset in the rotational direction from the circumferential starting point by less than or equal to 90 degrees along the circumference.

4. The engine assembly of claim 3, wherein the fuel spray defines an angular span of less than or equal to 30 degrees.

5. The engine assembly of claim 1, wherein the fuel injector is located in an opening extending through a sidewall of the combustion chamber defining the circumference of the combustion chamber.

6. The engine assembly of claim 5, wherein the piston includes a central domed region extending axially outward relative to an annular axial end surface of the piston surrounding the central domed region.

7. The engine assembly of claim 6, wherein the piston includes a seal ring engaged with an outer circumference of the piston and the circumference of the combustion chamber, the fuel spray being located axially outward from the seal ring when the piston is in the top dead center position.

8. The engine assembly of claim 1, wherein the fuel injector is located in an opening extending through an axial end of the combustion chamber.

9. The engine assembly of claim 8, wherein the piston defines an annular recess extending axially into an end surface of the piston and radially aligned with the fuel injector.

10. The engine assembly of claim 1, wherein the fuel injector is in fluid communication with a pressurized fuel supply at an operating pressure of at least 120 mega Pascal (MPa).

11. A method comprising:

providing a direct injection fuel injector in communication with a combustion chamber of an internal combustion engine defined by a cylinder bore in an engine structure and a piston disposed in the cylinder bore;

injecting a fuel spray from the fuel injector directly into the combustion chamber generally tangential to a circumferential sidewall of the combustion chamber; and

generating rotational flow of the fuel spray and an air charge within the combustion chamber from the injecting.

12. The method of claim 11, wherein the injecting defines a fuel injection period including an injection beginning and an injection termination for a combustion event, the generating including fuel spray from the injection beginning travelling approximately 360 degrees around the combustion chamber by the injection termination.

13. The method of claim 11, wherein the injecting provides fuel to the combustion chamber from a circumferential starting point relative to the circumferential sidewall of the combustion chamber, the generating including a fuel spray provided at an initial injection travelling rotationally around the combustion chamber to the starting location during the injecting.

14. The method of claim 11, wherein the generating includes a centerline of the fuel spray extending in a direction from a circumferential starting point on the circumference of the combustion chamber to a first circumferential ending point on the circumference of the combustion chamber, the first circumferential ending point being rotationally offset in a rotational direction of the rotational spray from the circumferential starting point by less than or equal to 135 degrees along the circumference.

15. The method of claim 14, wherein the fuel spray includes an outer radial periphery extending in a direction from the circumferential starting point to a second circumferential ending point on the circumference of the combustion chamber, the second circumferential ending point being rotationally offset in the rotational direction from the circumferential starting point by less than or equal to 90 degrees along the circumference.

16. The method of claim 15, wherein the fuel spray defines an angular span of less than or equal to 30 degrees.

17. The method of claim 11, wherein the fuel injector is located in an opening extending through a sidewall of the combustion chamber defining the circumference of the combustion chamber.

18. The method of claim 17, wherein the piston includes a central domed region extending axially outward relative to an annular axial end surface of the piston surrounding the central domed region and a seal ring engaged with an outer circumference of the piston and the circumference of the combustion chamber, the injecting including fuel spray being located axially outward from the seal ring when the piston is in a top dead center position.

19. The method of claim 11, wherein the fuel injector is located in an opening extending through an axial end of the combustion chamber and the piston defines an annular recess extending axially into an end surface of the piston and radially aligned with the fuel injector, the injecting including directing the fuel spray into the annular recess.

20. The method of claim 11, wherein the injecting includes providing a fuel spray to the fuel injector at an operating pressure of at least 120 mega Pascal (MPa).