Internal combustion engines and control

• US 6,854,440 B2
• Filed: 03/06/2001
• Issued: 02/15/2005
• Est. Priority Date: 03/03/2000
• Status: Expired due to Fees

• Current Assignee: Orbital Engine Company Pty Limited (Orbital Corporation Limited)
• Original Assignee: Orbital Engine Company Pty Limited (Orbital Corporation Limited)
• Inventors: Cathcart, Geoffrey Paul, Railton, Donald Andrew, Zavier, Christian Chandrakumar, McGrath, John Roy
• Primary Examiner(s): HUYNH, HAI H
• Application Number:
  US10/204,442
• Publication Number:
  US 20030140891A1
• Time in Patent Office: 1,442 Days
• Field of Search: 123/301, 123/305, 123/302, 123/306, 123/308, 123/90.15, 123/531, 123/298, 123/309
• US Class Current: 123/298
• CPC Class Codes: F02B 17/005 having direct injection in the combustion chamber
• CPC Class Codes: F02B 2023/106 Tumble flow, i.e. the axis of rotation of the main charge flow motion is horizontal
• CPC Class Codes: F02B 2075/125 Direct injection in the combustion chamber for spark ignition engines, i.e. not in pre-combustion chamber
• CPC Class Codes: F02B 23/101 the injector being placed on or close to the cylinder centre axis, e.g. with mixture formation using spray guided concepts
• CPC Class Codes: F02F 1/4214 specially adapted for four or more valves per cylinder
• CPC Class Codes: F02F 2001/245 the valve stems being orientated at an angle with the cylinder axis
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

Disclosed is an internal combustion engine comprising at least one cylinder with a reciprocating piston to provide said engine with at least one combustion chamber, said combustion chamber further comprising a delivery injector for injecting fuel directly into said combustion chamber, said engine further comprising at least one valved inlet air duct for delivering combustion air into said combustion chamber, wherein at least said inlet air duct and/or its valve is arranged to provide a low tumble inlet port to said at least one combustion chamber, said combustion chamber, in use, having low in-cylinder tumble gas motion of said combustion air and wherein said low in-cylinder tumble gas motion of said combustion air reduces over-enleanment of fuel in end gas regions of said combustion chamber.

Claims

1. An Internal combustion engine comprising at least one cylinder with a reciprocating piston to provide said engine with at least one combustion chamber, said combustion chamber further comprising a delivery injector for injecting fuel directly into said combustion chamber, said engine further comprising at least one valved inlet air duct for delivering combustion air into said combustion chamber, wherein at least said inlet air duct and/or its valve is arranged to provide a low tumble inlet port to said at least one combustion chamber, said combustion chamber, in use, being quiescent through having low in-cylinder tumble gas motion of said combustion air and wherein said low in-cylinder tumble gas motion of said combustion air reduces over-enleanment of fuel in end gas regions of said combustion chamber, wherein said engine is arranged for spray-guided combustion.

2. Engine according to claim 1, wherein the inlet air duct that terminates at an inlet port in the combustion chamber is arranged to create an air flow pattern, immediately behind and past the head of a poppet-type valve selectively closing said port whereby low tumble gas motion is produced within said combustion chamber.

3. Engine according to claim 1, wherein said inlet air duct is shaped so as to avoid small radii of curvature of the inlet duct in close upstream vicinity of the inlet port valve seat that otherwise contribute in generating air flow vectors in combustion air being delivered through said inlet port into the combustion chamber that lead to tumble gas motion in said combustion chamber.

4. Engine according to claim 1, wherein the engine is of spark-ignited, reciprocating-type in which a piston reciprocates within a cylinder substantially along a longitudinal axis thereof, and wherein the inlet air duct and/or valve selectively closing the inlet air duct is arranged to minimize inlet air flow vectors that have a substantial radial orientation with respect to the cylinder axis.

5. Engine according to claim 4, wherein the valve is a poppet-type valve, and wherein the intake air duct configuration upstream of the valve seat is such as to create an air flow past the back side of the poppet type valve head that is predominantly axial in orientation and substantially evenly distributed across the valve head back surface.

6. Engine according to claim 1 wherein the fuel injector is arranged as a central-injection direct fuel injector.

7. Engine according to claim 1, arranged for spray-guided combustion.

8. Engine according to claim 1 wherein said fuel delivery injector is adapted to generate a stratified charge within said combustion chamber.

9. Engine according to claim 1 wherein the valved inlet air duct is arranged to provide gas motion in said combustion chamber having a tumble ratio that is less than about 2.0 over the whole range of inlet port valve lift values.

10. Engine according to claim 1, further including an ignition timing system for selective ignition of a stratified charge delivered into the combustion chamber through said fuel delivery injector, said ignition timing system arranged to provide ignition timings in the range of about 5°

to 40°

BTDC during a compression stroke and over a defined engine load and speed range.

11. Stratified-charge, central-injection, spray-guided, spark-ignited engine according claim 10, wherein the ignition timing system is arranged for operation with a range of ignition timings of about 10°

to 35°

BTDC over an engine speed range of 400 RPM to 3600 RPM.

12. Stratified-charge, central-injection, spray-guided, spark-ignited engine according claim 10, wherein the ignition timing system is arranged for operation with a range of ignition timings of about 10°

to 35°

BTDC over an engine load range of 1 bar IMEP to 6 bar IMEP.

13. An engine according to claim 1 wherein said combustion chamber is further arranged whereby said low tumble gas motion is produced within said combustion chamber.

14. An engine according claim 1 wherein said fuel delivery means for delivering fuel directly to said combustion chamber is adapted to deliver fuel with a mass flow rate that is not constant during a fuel delivery event.

15. An engine according to claim 14 wherein said mass flow rate provides rich mixtures during an initial portion of said fuel delivery event.

16. An engine according to claim 14 wherein said mass flow rate provides lean fuel mixtures during a latter portion of said fuel delivery event.

17. An engine according to claim 1 wherein said engine operates with a co-variance of indicated mean effective pressure of less than 4% for ignition timings in the range of at least 30 degrees before top dead centre to 40 degrees before top dead centre.

18. An engine as claimed in claim 17 wherein said covariance of indicated mean effective pressure of less than 4% occurs at least for part load operating points such as 2000 revolutions per minute and 3.0 bar indicated mean effective pressure.

19. An engine according to claim 1 wherein said engine operates with an ISNOX of less than 2.0 g/kWh for timings of start of a fuel delivery event in the range of at least 75 degrees before top dead centre to at least 95 degrees before top dead centre.

20. An engine as claimed in claim 19 wherein said timings for said start of said fuel delivery event are effective at least for part load operating points such as an engine load of 3.0 bar indicated mean effective pressure and for an engine speed of 2000 revolutions per minute.

21. An engine according to claim 1 wherein said engine operates with a covariance of indicated mean effective pressure of approximately 4% or less with a mass of exhaust gas recirculation in a combustion charge of less than approximately 40%.

22. An engine according to claim 21 wherein said mass of exhaust gas recirculation is maintained above approximately 15% whereby combustion smoke is maintained below approximately 0.07 FSN.

23. An engine as claimed in claim 21 wherein said mass of EGR is effective at least for part load operating points such as 2000 revolutions per minute and 3.0 bar indicated mean effective pressure.

24. An engine according to claim 1 wherein fuel spray issuing from said delivery means operates with fuel spray penetration rates of substantially 45 meters per second or less for combustion chamber pressures of greater than substantially 0.0 bar gauge.

25. An engine according to claim 1 wherein fuel spray issuing from said delivery means operates with fuel spray penetration rates of substantially 15 meters per second or less for combustion chamber pressures of substantially greater than 3.0 bar gauge.

26. An engine according to claim 1 wherein said combustion chamber comprises a spark plug located down stream of an outlet of said fuel delivery means whereby in operation at least a portion of fuel spray issuing from said fuel delivery means is directed into a spark gap of said spark plug and wherein said fuel spray has a low penetration rate whereby at least a portion of said fuel spray is maintained in the vicinity of said spark plug at ignition.

27. An engine as claimed in claim 26 wherein said low penetration rate is less than substantially 45 meters per second for a combustion chamber pressure of substantially 0.0 bar gauge or greater.

28. An engine as claimed in claim 26 wherein said low penetration rate is substantially 15 meters per second or less for combustion chamber pressures of substantially 3.0 bar gauge or greater.

29. An engine according to claim 1 wherein said fuel delivery injector is adapted to deliver fuel entrained in a gas into said combustion chamber, and in particular is a gas-assisted direct in-cylinder fuel injector.

30. An engine according to claim 29 wherein said fuel entrained in said gas is delivered with a mass flow rate that is not constant.

31. An engine according to claim 29 wherein said injector is a gas assisted direct in-cylinder fuel injector wherein fuel is metered to said injector separately to delivery of fuel from said injector to said combustion chamber entrained in said gas whereby said fuel is delivered with a mass flow rate that is not constant.

32. Engine according to claim 1 wherein the valved inlet air duct is arranged to provide gas motion in said combustion chamber having a tumble ratio that is less than 1.5 over a substantial part of inlet valve lift.

33. Engine according to claim 1 wherein the valved inlet air duct is arranged to provide gas motion in said combustion chamber having a tumble ratio that is about 1.0 over a substantial part of inlet valve lift.

34. Internal combustion engine comprising at least one combustion chamber having an inlet port with an associated inlet valve for inlet of combustion air to said chamber generally along a first axis, an ignition device and at least one fuel delivery means communicating fuel directly to said chamber in a direction generally parallel to said first axis and in the vicinity of said ignition device,

wherein said generally parallel direction of said inlet air and said fuel reduces over-enleanment of fuel in end gas regions of said combustion chamber, and wherein said generally parallel direction is axial to said combustion chamber,

wherein said engine is arranged for spray-guided combustion.

35. An engine as claimed in claim 34 wherein said fuel is delivered so as to provide a stratified charge in said combustion chamber having said end gas regions.

36. An engine as claimed in claim 34 wherein said inlet air has limited radial flow relative to said generally parallel direction.

37. Internal combustion engine comprising at least one combustion chamber with a fuel delivery injector and an ignition means arranged for spray guided injection of fuel into said combustion chamber, said engine further comprising at least one valved inlet air duct for delivering combustion air into said combustion chamber, wherein at least said inlet air duct and/or its valve is arranged whereby low tumble gas motion is produced to achieve quiescence within said combustion chamber such as to reduce over-enleanment of fuel in end gas regions of said spray guided fuel.

38. An internal combustion engine as claimed in claim 37 further arranged to inject stratified charges of fuel into said combustion chamber.

39. An internal combustion engine as claimed in claim 37 wherein said tumble motion is less than 2.0.