Method for operating a spark ignition internal combustion engine with an exhaust gas turbocharger

Abstract

A method for operating an internal-combustion engine includes increasing a torque demand, controlling a throttle valve, opening an air injection valve and continuously measuring first and second gas pressures with an electronic control unit. The method also includes closing the throttle valve, measuring a first gas mass flow, retarding an ignition angle, and closing the air injection valve. In the method the throttle valve is opened with the control unit when the first gas pressure p.sub.1 equals the second gas pressure p.sub.2. The method also includes continuously controlling the fuel system with the electronic control unit to have a stoichiometric fuel/air ratio of the internal combustion engine being constantly combusting in the internal combustion engine.

Claims

1. A method for operating an internal-combustion engine the method comprising: increasing a torque demand on the internal-combustion engine; wherein the internal combustion engine is a spark ignition internal-combustion engine having an ignition angle that is adjustable with an electronic control unit, the internal combustion engine has an exhaust gas turbocharger with a turbine arranged in an exhaust gas section that guides an exhaust gas away from the internal-combustion engine, the internal combustion engine has a compressor arranged in an intake air section that guides an intake air toward the internal-combustion engine, the internal combustion engine has a throttle valve provided in a flow direction of the intake air downstream of the compressor and upstream of the internal-combustion engine, and the internal combustion engine has a compressed-air injection device including at least one pressure tank and an air injection valve, the air injection valve being openable and closable with the electronic control unit, to thereby introduce compressed air into the intake air section between the throttle valve and the internal-combustion engine, within the intake air section, a first gas pressure (p.sub.1) between the compressor and the throttle valve and a second gas pressure (p.sub.2) between the throttle valve and the internal-combustion engine are measured, controlling the throttle valve with the electronic control unit, opening the air injection valve and continuously measuring the first and second gas pressure pi, p.sub.2 with the electronic control unit; closing the throttle valve with the electronic control unit at an earliest of either a time when the air injection valve opens, or a time when the second pressure p.sub.2 exceeds the first pressure pi; measuring a first gas mass flow, which corresponds to an amount of air that is delivered into the internal-combustion engine, and measuring a second gas mass flow, which corresponds an amount of air to obtain a desired torque, with the electronic control unit; retarding an ignition angle when the first gas mass flow is greater than the second gas mass flow beginning to close the air injection valve when the first gas mass flow multiplied by a factor e.sub.zw,min is equal to the second gas mass flow; completely closing the air injection valve when the exhaust gas turbocharger reaches a defined rotational speed; opening the throttle valve with the electronic control unit when the first gas pressure pi equals the second gas pressure p.sub.2; and continuously controlling the fuel system with the electronic control unit to have a stoichiometric fuel/air ratio constantly combusting, to operate the internal combustion engine.

2. The method according to claim 1, further comprising: a compressor bypass passage that bypasses the compressor and that is provided in the intake air section, the bypass passage being closed by an overflow valve, the method further comprising: controlling an opening of the overflow valve with the electronic control unit at a time when the compressor reaches a surge line.

3. The method according to claim 2, further comprising: further controlling the overflow valve to avoid exceeding the surge line.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a schematic view of a construction of a piston internal-combustion engine according to an embodiment of the invention for implementing the method according to the invention;

(2) FIG. 2A is a view of a first diagram of desired and actual values of a medium pressure of the piston internal-combustion engine in the case of a desired torque value jump;

(3) FIG. 2B is a view of a second diagram of a charge pressure, a suction pipe pressure and a scaled exhaust gas turbocharger rotational speed in the case of the desired torque value jump;

(4) FIG. 2C is a view of a third diagram of mass flows through an air injection valve, through a throttle valve into the piston internal-combustion engine; and

(5) FIG. 2D is a view of a fourth diagram of actuator signals of the throttle valve, of the air injection valve and of an ignition angle delay.

DETAILED DESCRIPTION OF THE DRAWINGS

(6) FIG. 1 is a schematic view of a construction of a piston internal-combustion engine 1 for implementing the method according to the invention. In the present embodiment, the internal-combustion engine 1 has two cylinders, schematically illustrated by two large, unnumbered circles. Inside the circles, four smaller, also unnumbered, circles are situated, which represent two charge cycle inlet valves and two charge cycle outlet valves. For each cylinder, an ignition device is illustrated by a lightning symbol between the charge cycle valves.

(7) By way of an electronic control unit (ECU) marked 13, an ignition angle adjustment to early or late can take place with respect to a crank angle position. A fuel system 19 is further provided for operating the internal-combustion engine. An unnumbered fuel injector is schematically illustrated by a triangle for each cylinder.

(8) For supplying the internal-combustion engine 1 with intake air and for discharging exhaust gases, an intake air section 6 and an exhaust gas section 4, respectively, are provided. An exhaust gas turbocharger 2 is arranged in the exhaust gas section 4 and in the intake air section 6. A turbine 3 of the exhaust gas turbocharger 2 is arranged in the exhaust gas section 4, and a compressor 5 of the exhaust gas turbocharger 2 is arranged in the intake air section 6. Furthermore, an emission control system 18, for example, a catalytic converter or particle filter, is situated in the exhaust gas section 4 behind the turbine 3 in the flow direction of the exhaust gas, illustrated by an arrow. For bypassing the turbine 3 with the exhaust gas, a turbine bypass 16 is further provided, having a closing element 17, such as an exhaust flap valve, arranged in the turbine bypass 16. In a further embodiment, the turbine bypass 16 may also not be present.

(9) On the intake air side, the intake air in the intake air section 6 first flows through an intake muffler not separately numbered, then through the compressor 5, and then through a charge air cooler 20. A throttle valve 9 for regulating the intake air quantity that flows into the internal combustion engine for the combustion is provided in the flow direction of the intake air downstream of the charge air cooler 20. After flowing through the throttle valve 9, the intake air flows into an intake manifold (unnumbered) and then through the charge cycle inlet valves into the cylinders. Furthermore, a compressor bypass 8 is provided for the compressor 5, by which the intake air bypasses the compressor 5. The bypass 8 has an overflow valve 7. In another embodiment, the compressor bypass 8 may also not be present.

(10) In order to, for example, effectively bridge the so-called turbo lag, a compressed-air injection device 10 is provided, which essentially consists of a pressure tank 11, and an air injection valve 12, which is operatively connected with the pressure tank 11 in a gas-carrying manner.

(11) The air injection valve 12 can be triggered by way of the electronic control unit 13, for example, an engine control device, so that the air injection valve 12 can be opened and closed according to demand. The overflow valve 7 can also be triggered by the control unit 13 for opening and closing the compressor bypass 8. Furthermore, the throttle valve 9 can also be controlled or automatically triggered by the control unit 13 to open or close it. For implementing the method according to the invention, a pressure measuring point is further provided between the compressor 5 and the throttle valve 9, and further a second pressure measuring point is provided between the throttle valve 9 and the internal-combustion engine 1. The first pressure is marked p.sub.1; the second pressure is marked p.sub.2. Both pressure signals are processed in the control unit 13.

(12) Even if nowadays almost all parameters of an internal-combustion engine 1 can be modeled or stored as performance characteristics in the control unit 13, in a further embodiment, additional sensors may be provided for measuring, for example, the following: Gas pressure upstream of the compressor 5 gas pressure downstream of the compressor 5 p.sub.1, gas pressure in the suction pipe (i.e. downstream of the throttle valve 9), p.sub.2, gas pressure in the pressure tank 11, gas pressure upstream of the turbine 3, gas pressure downstream of the turbine 3, rotational speed of the internal combustion engine 1, rotational speed of the exhaust gas turbocharger 2.

(13) The air mass requirement for the bridging of the turbo lag is very much dependent on the automatic control strategy that is used for actuating the throttle valve 9, the air injection valve 12, the overflow valve 7 and the ignition point. The object of the automatic control strategy according to the invention is to achieve a response that is as fast as possible to a demanded desired torque value jump. Simultaneously, the air mass consumption should be kept as low as possible. The desired torque value jump may be derived, for example, from a motor vehicle driver or, in the case of a hybrid vehicle, from a control device.

(14) For minimizing the reaction time to a desired torque value jump of the internal-combustion engine while the air consumption is minimal, the following actuators with the control signals are therefore available:

(15) TABLE-US-00001 Actuator: Control Signal: Throttle valve 9, u.sub.dk Air injection valve 12, u.sub.bv Possibly, overflow valve 7, u.sub.usv Ignition angle, u.sub.zw

(16) For the indirect air injection for eliminating turbo lag, automatic control strategies, as mentioned above, have already been developed. The automatic control strategy according to the invention presented here, however, results in a clearly lower air requirement. FIGS. 2A to 2D show the signal courses of the most important values in the case of a turbo lag bridging, by means of an indirect air injection according to the invention.

(17) In a first diagram, FIG. 2A illustrates the desired and actual values of the medium pressure of the internal-combustion engine 1 in the case of a desired torque value jump.

(18) In a second diagram, FIG. 2B illustrates the charge pressure p.sub.1 (pressure downstream of the compressor), the suction pipe pressure p.sub.sr and the scaled turbocharger rotational speed of the internal-combustion engine 1 in the case of the desired torque value jump.

(19) FIG. 2C illustrates the mass flows through the air injection valve 12 m.sub.bv, through the throttle valve 9 m.sub.dk, and into the internal-combustion engine 1 m.sub. in the case of a desired torque value jump.

(20) FIG. 2D illustrates the actuator signals of the throttle valve 9 u.sub.dk, of the air injection valve 12 u.sub.bv and of the ignition angle u.sub.zw.

(21) In the automatic control strategy according to the invention, the suction pipe (area between the throttle valve 9 and the charge cycle inlet valves) is intentionally overcharged in order to achieve a greater air mass flow than necessary through the internal-combustion engine 1. In order to nevertheless achieve the desired torque, the ignition angle is displaced to late (retarded). The advantage of this strategy is the increased exhaust gas enthalpy, which results in an increase of the exhaust gas turbocharger acceleration. The duration of the air injection can thereby be shortened. The details of the automatic control strategy according to the invention in the case of the desired torque value jump are the following.

(22) 1. Throttle valve 9 and air injection valve 12 completely open: In order to achieve a torque buildup of the internal-combustion engine 1 that is as fast as possible, the suction pipe pressure p.sub.sr has to be increased as fast as possible. This can be achieved by opening the air injection valve 12 and the throttle valve 9.

(23) 2. As soon as the suction pipe pressure p.sub.sr is greater than the charge pressure p.sub.1, close the throttle valve: As soon as the suction pipe pressure p.sub.sr is greater than the charge pressure p.sub.1, the throttle valve 9 is closed immediately in order to prevent the loss of air into the intake section as well as a surge of the compressor 5, which would occur because of the flowing-back of the injected air from the suction pipe via the throttle valve 9 to the compressor 5.

(24) 3. As soon as the mass flow through the internal-combustion engine 1 m.sub. is greater than the desired mass flow through the internal-combustion engine 1 m.sub.,des, displace the ignition angle to late: In order to obtain the desired torque despite the large mass flow, the ignition angle is displaced to late. The variable m.sub.,des corresponds to the mass flow, which is necessary in order to achieve the desired torque p.sub.me,des within an ignition angle adjustment. In FIGS. 2A to 2D, this takes place at t0.15 seconds.

(25) 4. When necessary: As soon as the compressor 5 is at the surge line, open the overflow valve 7: When the pressure ratio over the compressor 5 for the present compressor mass flow is close to the surge line, the overflow valve 7 will be opened in order to prevent a surging of the compressor 5. The thereby caused air mass flow-off leads to a reduction of the pressure ratio by way of the compressor 5. The mass flow-off is regulated by way of the overflow valve 7 such that the pressure ratio comes to be situated slightly under the surge line. The operating point of the compressor 5 therefore extends along the surge line.

(26) In the load variation in FIGS. 2A to 2D, the overflow valve 7 is not required. Its course is therefore not shown.

(27) 5. As soon as the mass flow through the internal-combustion engine m.sub.=m.sub.,des/e.sub.zw,min, slowly close the air injection valve 12:

(28) Although the suction pipe is to be overcharged, the mass flow m.sub. should not exceed the value m.sub.,max=m.sub.,des/e.sub.zw,min because otherwise the desired torque can no longer be achieved by the ignition angle adjustment alone. In order to achieve this, the inflow through the air injection valve 12 into the suction pipe is throttled. In FIG. 2A, this takes place at t0.21 seconds. The variable e.sub.zw,min indicates the reduction of the thermodynamic efficiency which can maximally be achieved by the adjustment of the ignition angle. In the illustrated embodiment, its value was selected to be equal to e.sub.zw,min=0.66.

(29) 6. As soon as the rotational speed of the exhaust gas turbocharger 2 is greater than 0.9.sub.des, completely close the air injection valve 12:

(30) As soon as the exhaust gas turbocharger 2 is close to the desired rotational speed, the air injection valve 12 will be closed. The suction pipe will subsequently be discharged.

(31) 7. As soon as the suction pipe pressure p.sub.sr is equal to the charge pressure p.sub.1, open the throttle valve: As soon as the suction pipe pressure p.sub.sr has fallen to the level of the charge pressure p.sub.1, the throttle valve will be opened again.

(32) The medium-pressure buildup illustrated in FIGS. 2A to 2D takes place extremely rapidly. 90% of the desired medium pressure p.sub.me,des is reached in only 132 milliseconds. The displacement of the ignition angle to late is suitable for fashioning the medium pressure rise to be slow. The exhaust gas enthalpy is thereby additionally increased, which results in a reduction of the air requirement.

(33) The operating method according to the invention for an internal-combustion engine 1 of the above-mentioned type is thereby advantageously used for minimizing a reaction time to a desired torque value jump of an internal-combustion engine 1 while the compressed-air consumption is minimal.

LIST OF REFERENCE NUMBERS AND SYMBOLS

(34) 1 Internal-combustion engine 2 Exhaust gas turbocharger 3 Turbine 4 Exhaust gas section 5 Compressor 6 Intake air section 7 Overflow valve 8 Compressor bypass 9 Throttle valve 10 Compressed-air injection device 11 Pressure tank 12 Air injection valve 13 Control unit 14 First gas pressure measuring point 15 Second gas pressure measuring point 16 Turbine bypass 17 Third closing element 18 Emission control system 19 Fuel system 20 Charge air cooler P.sub.1 First gas pressure P.sub.2 Second gas pressure p.sub.sr Suction pipe pressure p.sub.1 Charge pressure p.sub.eff Effective medium pressure p.sub.eff,des Desired medium pressure (desired torque) {dot over (m)} (Numbering in FIG. 2c), identical with {dot over (m)}.sub.dk {dot over (m)}.sub. Mass flow through the internal-combustion engine {dot over (m)}.sub.,des. Desired mass flow through the internal-combustion engine {dot over (m)}.sub.bv Mass flow through air injection valve {dot over (m)}.sub.dk Mass flow through throttle valve u.sub.dk Control signal throttle valve u.sub.bv Control signal air injection valve u.sub.zw Control signal ignition angle distortion .sub.tl Exhaust gas turbocharger rotational speed .sub.tl,des Desired exhaust gas turbocharger rotational speed e.sub.zw,min Maximal reduction of the thermo-dynamic efficiency by ignition angle adjustment

(35) 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.