This invention pertains to fuel injection in an internal combustion engine.
One known engine configuration is a spark-ignited, direct-injection (SIDI) engine wherein a fuel injector directly injects fuel into a combustion chamber in close proximity to a spark plug. Known SIDI systems include a spark-ignition, direct-injection, spray-guided engine employing a fuel injector operative at a fuel-rail pressure in the range of 10-20 MPa and adapted to directly inject fuel into a combustion chamber. The engine utilizes optimized high-squish bowled pistons, and variable swirl valve control.
Known injectors used in a spray guided SIDI engine comprise either a multi-hole injector or a piezoelectric hollow-cone injector. In such known types of injectors, injected fuel mass is distributed along the outer edge of a conical spray pattern. As a consequence, little fuel remains around the spark plug, limiting ignition stability and combustion performance. Fuel injected from known multi-hole injectors penetrate deeply into the combustion chamber due to reduced contact area with the surrounding air, especially at heavy loads. Furthermore, fuel injection can be affected by conditions related to fuel temperature, cylinder pressure, and other conditions.
A fuel injector adapted to inject fuel directly into a combustion chamber of an internal combustion engine includes a spray nozzle mountable to direct a fuel spray into the combustion chamber from a plurality of spray discharge orifices. Each spray discharge orifice includes an opening through a tip of the spray nozzle and an elongated cross-section having a major axis orientable to a center electrode of a spark plug in the combustion chamber.
One or more embodiments will now be described, by way of example, with reference to the accompanying drawings, in which:
Referring now to the drawings, wherein the showings are for the purpose of illustrating certain exemplary embodiments only and not for the purpose of limiting the same,
Each combustion chamber 15 of the internal combustion engine comprises a cylindrical opening in an engine block 11 defining a cylinder, a moveable piston 14, and a cylinder head 12. The top of each piston preferably has a bowl formed therein. The piston is operable to move linearly within the cylinder. The combustion chamber 15 is formed in each cylinder between the bowl in the top of the piston and the cylinder head 12. The cylinder head contains one or more moveable air intake valves and one or more moveable exhaust valves (not shown), the fuel injector 20 and the spark plug 40. The fuel injector 20 injects a predetermined quantity of pressurized fuel directly into the combustion chamber in response to a command from the control module. An injector center line 25 is depicted, consisting of a line defined by a longitudinal axis of the fuel injector 20 and passing through a cross-sectional center thereof. The spark plug 40, comprising a center electrode 42 and a side electrode 46 which together form a gap 44, creates an electric arc in the gap in response to an output from the control module effective to ignite a combustible mixture formed in the combustion chamber. A spark plug center line 45 is depicted, consisting of a line defined by a longitudinal axis of the spark plug 40 and passing through a center of the center electrode 42. The intake valves are operable to open and allow inflow of air and fuel to the combustion chamber. The exhaust valves are operable to open and allow exhaust of products of combustion out of the combustion chamber. Each piston is mechanically operably connected to a crankshaft via a piston rod. The crankshaft is mounted on and rotates in main bearings, in response to linear force applied thereto by the piston rods, as a result of combustion events in each combustion chamber.
The fuel injector 20 preferably comprises an electro-mechanical solenoid device adapted to urge open a flow valve contained therein to meter pressurized fuel from a high pressure fuel line through a tip 30 of a nozzle inserted into an opening into the combustion chamber, in response to a control signal from the control module. The tip of the spark plug and the injector tip 30 are preferably in close proximity, as depicted in
Referring now to
The design of the tip of the injector nozzle with elongated openings 36, 36′, 36″ results in each fuel injection pulse being substantially shaped as an oval or a planar sheet, increasing the fuel surface area in the combustion chamber. The shaping of the fuel pulse enlarges the contact area between the fuel spray and intake air in the combustion chamber and distributes the fuel charge into the region where initial charge combustion occurs, i.e., the vicinity of the spark plug. The increased fuel spray contact area reduces spray penetration into the combustion chamber, thus retaining more fuel around the spark plug to accelerate combustion and reduce wall-wetting of the combustion chamber. In a further development, the shape of each fan output from the nozzle openings can be adjusted to provide fuel in a middle portion of each spray plume, adapted for different bowl geometries to provide optimum combustion charge conditions at the spark plug. Benefits associated therewith include improved ignition stability, reduced smoke at heavy load, faster and more complete combustion providing an opportunity to reduce hydrocarbons, lower engine-out NOx, and lower dependency on in-cylinder air flow levels. The fuel spray primarily controls the combustion charge for the engine. The fuel injector provides an ignitable mixture at the spark plug gap during spark ignition. Interaction between the fuel spray and surrounding air affects fuel vaporization and formation of the combustion charge, thus affecting ignition of the combustion charge.
The disclosure has described certain preferred embodiments and modifications thereto. Further modifications and alterations may occur to others upon reading and understanding the specification. Therefore, it is intended that the disclosure not be limited to the particular embodiment(s) disclosed as the best mode contemplated for carrying out this disclosure, but that the disclosure will include all embodiments falling within the scope of the appended claims.
This application claims the benefit of U.S. Provisional Application No. 60/824,507 filed on Sep. 5, 2006 which is hereby incorporated herein by reference.
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