Method for operating an internal combustion engine
10337415 ยท 2019-07-02
Assignee
Inventors
Cpc classification
F02D41/3035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02P15/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D13/0226
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/3017
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/402
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/40
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F02D13/0207
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D9/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2041/001
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B17/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2041/0015
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/0002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02B3/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D13/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D9/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method for operating an internal combustion engine of a motor vehicle involves directly injecting fuel into a combustion chamber using an injection device, and a mixture of the fuel and air is ignited in the combustion chamber by an ignition device. The internal combustion engine is operated selectively in at least one first operating mode with at least one first valve lift of at least one gas exchange valve of the internal combustion engine, associated with the combustion chamber, or in at least one second operating mode with at least one second valve lift of the gas exchange valve, which is smaller than the first valve lift. For assisting a charge movement of the mixture in the second operating mode, at least one further injection of fuel directly into the combustion chamber is carried out prior to the ignition.
Claims
1. A method for operating an internal combustion engine of a motor vehicle, the method comprising: directly injecting fuel into at least one combustion chamber of the internal combustion engine using at least one injection device; and igniting, by a spark ignition device, a mixture of fuel and air in the combustion chamber, wherein the internal combustion engine is operated selectively in: at least one first operating mode with at least one first valve lift of at least one gas exchange valve of the internal combustion engine, associated with the combustion chamber, and at least one second operating mode with at least one second valve lift of the gas exchange valve, which is smaller than the first valve lift, wherein a charge movement of the mixture in the second operating mode is assisted by at least one further injection of fuel directly into the combustion chamber, which is carried out prior to the ignition, wherein the internal combustion engine is operated in homogeneous operation in the second operating mode, and wherein the spark ignition device performs the ignition in the second operating mode.
2. The method of claim 1, wherein the further injection is carried out after the at least one first injection.
3. The method of claim 1, wherein in the second operating mode the ignition is a multi-spark ignition.
4. The method of claim 1, wherein a load setting of the internal combustion engine in the second operating mode is performed selectively or as a function of speed-load point of the internal combustion engine using at least one throttle valve situated in an intake tract of the internal combustion engine, a phase adjustment of a camshaft for actuating the gas exchange valve, or a supercharging rate of at least one exhaust gas turbocharger associated with the internal combustion engine.
5. The method of claim 1, wherein the internal combustion engine is operated in the second operating mode when at least one value characterizing at least a temperature of the internal combustion engine exceeds a predefined threshold value.
Description
BRIEF DESCRIPTION OF THE DRAWING FIGURES
(1) The drawings show the following:
(2)
(3)
(4)
DETAILED DESCRIPTION
(5)
(6) As is apparent from
(7) The second characteristic map range 24 corresponds to a second operating mode of the gasoline engine in which the gasoline engine is operated with at least one second valve lift curve. The second valve lift curve brings about respective second valve lifts of the intake valves. The second valve lifts are smaller than the first valve lifts.
(8) The intake valves of the gasoline engine are actuated via at least one camshaft, for example. This means that the camshaft cooperates with the intake valves, so that the intake valves, depending on the operating mode, carry out their respective valve lifts and correspondingly open and close.
(9) For providing the various valve lifts, the camshaft includes, for example, respective first cams associated with the first valve lifts, and respective second cams associated with the second valve lifts. The camshaft cooperates with the intake valves via its cams.
(10) The gasoline engine is selectively operable in the first operating mode (first characteristic map range 22) or in the second operating mode (second characteristic map range 24). In a so-called fired operation of the gasoline engine, in both operating modes respective injections of fuel of the gasoline engine are carried out directly in combustion chambers, in particular cylinders, of the gasoline engine. For this purpose, at least one injector by means of which fuel is injected directly into the associated combustion chamber is associated with each of the combustion chambers.
(11) In addition, in each case at least one of the intake valves is associated with the combustion chambers. When the intake valves are in an open position, air flowing through an intake tract of the gasoline engine via intake ducts may flow into the respective combustion chambers and mix with the fuel that is injected directly into the combustion chambers. This results in a fuel-air mixture that is ignited and which subsequently combusts.
(12) For igniting the particular fuel-air mixture in the combustion chamber, at least one spark plug, for example, by means of which an ignition spark is generated is associated with each of the combustion chambers. The point in time at which the ignition spark is generated and the fuel-air mixture is thus ignited is referred to as the ignition point. The point in time at which the fuel is injected directly into the respective combustion chambers is referred to as the injection point.
(13) When the gasoline engine is operated in the second operating mode, the intake valves do not open as wide as in the first operating mode, since they carry out smaller second valve lifts. In other words, in the second operating mode the intake valves open up smaller opening cross-sections, via which the air may flow into the respective combustion chambers, than in the first operating mode. As is apparent from
(14) In the second operating mode the gasoline engine is operated for the most part in homogeneous operation, the second characteristic map range 24 having a hysteresis range 26 with regard to load and speed.
(15) In order to now compensate for or avoid a smaller charge movement of the fuel-air mixture in the second operating mode in comparison to the first operating mode due to the smaller second valve lifts, for assisting the charge movement of the fuel-air mixture in the second operating mode at least one further injection of fuel into the combustion chambers is carried out close to the time of ignition. A very advantageous charge movement or turbulence is thus achieved resulting in very high combustion stability of the combustion of the fuel-air mixture. Control times of the at least one camshaft may thus be achieved resulting in very low fuel consumption and thus low CO<59>2</59> emissions of the gasoline engine due to very low charge cycle work.
(16) In the present case, the second characteristic map range 24 has a sub-range 28 in which the internal combustion engine is also operated as a function of the load and/or speed, and in which the at least one further injection of fuel is carried out directly in the respective combustion chambers prior to the ignition, in particular close to the time of ignition, of the fuel-air mixture. In other words, a so-called ignition injection is carried out. The sub-range 28 also has a hysteresis range 29 with regard to load and speed.
(17) Further possible conditions for activating the second operating mode include, for example, the temperature of the gasoline engine, in particular of its lubricant and/or coolant, being higher than 50. In addition, a switch is made into the second operating mode, for example, only when a warm-up operation for heating up a catalytic converter of the gasoline engine as well as warm-up of the gasoline engine have concluded. Idling operation as well as start-stop operation are also carried out in the second operating mode with the lower valve lifts.
(18) At least one exhaust gas turbocharger by means of which the gasoline engine may be supplied with compressed air, i.e., supercharged, is preferably associated with the gasoline engine. This results in particularly efficient operation of the gasoline engine.
(19) As is apparent in particular with reference to
(20) In the second characteristic map range 24 with the second, smaller valve lifts, the load is adjusted by means of the throttle valve in a sub-range 30 of the second characteristic map range 24. The adjustment of the load via the camshaft, associated with the intake valves and referred to as the intake camshaft, takes place in a sub-range 32 of the second characteristic map range 24. The adjustment of the load (load control) via wastegate control in the supercharging range takes place in a sub-range 34 of the second characteristic map range 24. Wastegate control refers to the opening and closing of a valve element, referred to as a wastegate, of a bypass device of the exhaust gas turbocharger. The bypass device is associated with a turbine of the exhaust gas turbocharger, and includes a bypass duct via which exhaust gas from the gasoline engine flowing through the turbine can bypass, and thus cannot drive, a turbine wheel of the turbine.
(21) The bypass duct may be fluidically blocked and fluidically enabled by means of the valve element (wastegate). If the bypass duct is fluidically blocked in a closed position of the valve element, exhaust gas cannot flow through the bypass duct. This means that at least essentially all of the exhaust gas drives the turbine wheel. The bypass duct is fluidically enabled in at least one open position of the valve element, so that the exhaust gas may at least partially bypass the turbine wheel, whereby the exhaust gas bypassing the turbine wheel does not drive the turbine wheel. Due to this opening and closing of the valve element (wastegate control), the power of the turbine, and thus the pressure of the compressed air to be supplied to the gasoline engine (charge pressure), and thus the quantity or mass of air to be supplied to the gasoline engine, may be adjusted.
(22) The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.