Control device for engine

Patent metadata

Field	Value
Publication number	US-10711708-B2
Application number	US-201816052834-A
Country	US
Kind code	B2
Filing date	Aug 2, 2018
Priority date	Aug 25, 2017
Publication date	Jul 14, 2020
Grant date	Jul 14, 2020

Abstract

A control device for an engine is provided, which includes a fuel injector attached to the engine, a spark plug disposed to be oriented into a combustion chamber, a swirl control valve provided in an intake passage, and a controller connected to the fuel injector, the spark plug, and the swirl control valve and configured to control the fuel injector, the spark plug, and the swirl control valve. The swirl control valve closes in a given operating state of the engine. The fuel injector injects fuel after the swirl control valve is closed, between intake stroke and an intermediate stage of compression stroke. The fuel injector injects the fuel after the first fuel injection. The spark plug performs the ignition after the second fuel injection so that the mixture gas starts combustion by flame propagation and then unburned mixture gas self-ignites.

First claim

What is claimed is:

1. A control device for an engine including a cylinder, a piston, a cylinder head, and a combustion chamber formed by the cylinder, the piston, and the cylinder head, comprising:
a fuel injector attached to the engine;
a spark plug disposed to be oriented into the combustion chamber and configured to perform a forced ignition;
a swirl control valve provided in an intake passage connected to an intake port; and
a controller connected to the fuel injector, the spark plug, and the swirl control valve and configured to output a control signal to the fuel injector, the spark plug, and the swirl control valve, respectively, the controller including:
a processor configured to execute:
a swirl control valve controlling module configured to output the control signal to the swirl control valve to close in a given operating state of the engine;
a first fuel injection controlling module configured to output the control signal to the fuel injector to perform a first fuel injection at a predetermined first timing after the swirl control valve is closed and between intake stroke and an intermediate stage of compression stroke;
a second fuel injection controlling module configured to output the control signal to the fuel injector to perform a second fuel injection at a predetermined second timing set on a retarding side of the first fuel injection; and
a spark plug controlling module configured to output the control signal to the spark plug to perform the forced ignition at a given ignition timing after the second fuel injection so that a mixture gas starts combustion by flame propagation and then an unburned mixture gas self-ignites, the given ignition timing being stored in memory.

2. The control device of claim 1 , wherein, when the engine operates within a low load operating range in which an engine load is below a given load, spark-ignition (SI) combustion and compression-ignition (CI) combustion are performed, and
wherein, within the low load operating range, the controller controls the fuel injector to perform a second-stage injection later on a lower engine load side than on a higher engine load side.

3. The control device of claim 1 , wherein, when the engine operates within a low load operating range in which an engine load is below a given load, SI combustion and CI combustion are performed, and
wherein, within the low load operating range, the controller controls the fuel injector to perform a second-stage injection a larger number of times on a lower engine load side than on a higher engine load side.

4. The control device of claim 1 , wherein a swirl generating part forms an inclined swirl flow flowing obliquely with respect to a center axis,
wherein the fuel injector is disposed in a center portion of the combustion chamber and injects a plurality of fuel portions including a first fuel portion, a second fuel portion, a third fuel portion, and a fourth fuel portion of which sprays reach the swirl flow generated by the swirl generating part, simultaneously from a plurality of nozzle ports including a first nozzle port, a second nozzle port, a third nozzle port, and a fourth nozzle port, respectively, of which injecting directions are different from each other in a circumferential direction of the fuel injector, and
wherein, when a position at which the spray of the first fuel portion reaches the swirl flow is a first position and a position at which the spray of the second fuel portion reaches the swirl flow is a second position, the spray of the first fuel reaches the first position and then moves away from the second position by the swirl flow before the spray of the second fuel portion reaches the second position, and, after the spray of the third fuel portion reaches the swirl flow, the spray of the fourth fuel portion reaches a position to which the spray of the third fuel portion moves by the swirl flow.

5. The control device of claim 4 , wherein the swirl generating part generates the swirl flow at a swirl ratio of 2 or above.

6. The control device of claim 4 , wherein the controller controls the fuel injector to inject the fuel at a pressure between 30 MPa and 120 MPa.

7. The control device of claim 4 , wherein the controller controls the spark plug and the fuel injector so that a center of gravity of a mixture gas distribution formed by the fuel injected at each of the predetermined first timing and the predetermined second timing is located in the center portion of the combustion chamber at the given ignition timing.

8. The control device of claim 4 , wherein the plurality of fuel portions injected simultaneously include a fifth fuel portion that reaches a wall surface of the combustion chamber, and
wherein the spray of the fifth fuel portion reaches the wall surface and then moves therealong to reach the swirl flow.

9. A control device for an engine formed with a combustion chamber having a bottom surface, the bottom surface formed by a piston for reciprocating inside a cylinder along a center axis thereof, the device causing a mixture gas to start SI combustion through flame propagation and then causing unburned mixture gas to perform CI combustion by self-ignition, comprising:
a spark plug configured to perform an ignition in a center portion of the combustion chamber;
a fuel injector configured to inject fuel into the combustion chamber;
a swirl generating part configured to generate a swirl flow inside the combustion chamber; and
a controller configured to control the spark plug and the fuel injector,
wherein the controller controls the fuel injector to inject the fuel at a given injection timing after the swirl flow is generated, and controls the spark plug to ignite at a given ignition timing after the fuel is injected, and
wherein the controller controls the fuel injector to perform a plurality of injections of the fuel, at least including a first-stage injection in which the fuel is injected at a first injection timing from intake stroke to an intermediate stage of compression stroke, and a second-stage injection in which the fuel is injected at a second injection timing in the intermediate stage of the compression stroke or thereafter.

10. The control device of claim 9 , wherein, when the engine operates within a low load operating range in which an engine load is below a given load, the SI combustion and the CI combustion are performed, and
wherein, within the low load operating range, the controller controls the fuel injector to perform the second-stage injection later on a lower engine load side than on a higher engine load side.

11. The control device of claim 9 , wherein, when the engine operates within a low load operating range in which an engine load is below a given load, the SI combustion and the CI combustion are performed, and
wherein, within the low load operating range, the controller controls the fuel injector to perform the second-stage injection a larger number of times on a lower engine load side than on a higher engine load side.

12. The control device of claim 9 , wherein the swirl generating part forms an inclined swirl flow flowing obliquely with respect to the center axis,
wherein the fuel injector is disposed in the center portion of the combustion chamber and injects a plurality of fuel portions including a first fuel portion, a second fuel portion, a third fuel portion, and a fourth fuel portion of which sprays reach the swirl flow generated by the swirl generating part, simultaneously from a plurality of nozzle ports including a first nozzle port, a second nozzle port, a third nozzle port, and a fourth nozzle port, respectively, of which injecting directions are different in a circumferentia

Assignees

• Mazda Motor

Inventors

• Matsumoto Kota
• Urushihara Tomonori
• SUEOKA Masanari
• Maruyama Keiji
• Miyamoto Toru
• Koshiro Yudai
• Pak Gyetae

Classifications

• F02B31/085

  having two inlet valves · CPC title

• F02B2023/103

  the injector having a multi-hole nozzle for generating multiple sprays · CPC title

• F02B2023/108

  Swirl flow, i.e. the axis of rotation of the main charge flow motion is vertical · CPC title

• F02B2023/102

  the spark plug being placed offset the cylinder centre axis · CPC title

• F02D41/3029

  further comprising a homogeneous charge spark-ignited mode · CPC title