Regulating Device With an Electronic Control Unit for Regulating Boost Pressure in a Supercharged Internal Combustion Engine
20250012225 ยท 2025-01-09
Inventors
Cpc classification
F02D41/0007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/013
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/162
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/183
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02D41/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/013
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A regulating device comprising an electronic control unit for regulating boost pressure in a supercharged internal combustion engine with two-stage supercharging, i.e. with a first low-pressure stage (ND) and a second high-pressure stage (HD). The high-pressure stage (HD) has a rigid high-pressure turbine and a controllable regulating flap (RK). The low-pressure stage (ND) has a variable adjustable turbine geometry (VTG). The electronic control unit contains a regulating module that is designed, in particular via an appropriately programmed computer program product, for basic adjuster regulation in such a way that the boost pressure regulation is carried out solely by way of the adjustable turbine geometry (VTG) of the low-pressure stage (ND), wherein the regulating flap (RK) of the high-pressure stage (HD) is controlled in the fully closed state.
Claims
1.-4. (canceled)
5. A regulating device comprising: an electronic control unit for regulating boost pressure in a turbocharged internal combustion engine having at least two-stage turbocharging, having a low-pressure stage and a high-pressure stage, wherein the high-pressure stage has a rigid high-pressure turbine and a controllable bypass regulating flap, and wherein the low-pressure stage has a turbine having variably adjustable turbine geometry, and a regulating module in the electronic control unit, configured for a fundamental one-actuator regulation in the form that boost pressure regulation is performed solely by way of the adjustable turbine geometry of the low-pressure stage to achieve a specified boost pressure target value, wherein the regulating flap of the high-pressure stage is controlled in the completely closed state.
6. The regulating device according to claim 5, wherein the one-actuator regulation is fundamentally activatable when a lower exhaust gas counter pressure is thus achieved than by a two-actuator regulation.
7. The regulating device according to any claim 5, wherein the regulating flap is used as an exception for a smaller defined high load part of the possible operating points as a second actuator for two-actuator regulation, wherein this smaller high load part of the possible operating points is definable in particular by exceeding a specified full load speed limiting value and/or a specified boost pressure limiting value and/or a specified mass flow limiting value related to component protection.
8. A motor vehicle having a regulating device according to claim 5.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0017] The disclosure is explained in more detail by way of an exemplary embodiment and on the basis of a drawing.
[0018]
[0019]
[0020]
[0021]
DETAILED DESCRIPTION OF THE DRAWINGS
[0022]
[0023] The internal combustion engine D and in particular also the boost pressure p1 is regulated by an electronic control unit 4. For example, the current boost pressure p1_ist is the input signal of the electronic control unit 4. The boost pressure target value p1_soll is also specified in the electronic control unit 4 as a reference variable of a regulating module 5. Those skilled in the art will appreciate that the electronic control unit 4 may comprise a suitable engine control unit (ECU) and/or engine control module (ECM) having a processing unit (e.g., a microcontroller or a microprocessor) and an associated memory (e.g., ROM, RAM, PROM, EEPROM, etc.) for storage of software, programs, and/or logic to be executed by the processing unit. The regulating module 5 may comprise software, programs, and/or logic to be executed by the processing unit.
[0024] The control unit 4 is shown in somewhat more detail in
[0025] The design (in particular programming) of the regulating module 5 and its effect will be explained in more detail in conjunction with
[0026] The regulating module 5 is designed for a fundamental one-actuator regulation in the form that the boost pressure regulation is performed solely by way of the adjustable turbine geometry ND-VTG of the turbine 3. The regulating flap RK is controlled via the valve 2 in the high-pressure stage HD in the completely closed state, for example, via a duty cycle of 100%.
[0027] This one-actuator regulation (regulator transfer) is fundamentally activated when a lower exhaust gas counter pressure p3 is thus achieved (see also
[0028]
[0029] Notwithstanding the fundamental one-actuator regulation according to the disclosure, the regulating flap RK is used as an exception via the duty cycle (see white numbers in the characteristic maps) at the valve 2 for a smaller defined high load part of the possible operating points as a second actuator (duty cycle<100%) for two-actuator regulation. This smaller high load part of the possible operating points is preferably defined here in particular by exceeding a specified full load speed limiting value n.sub.M_lim and/or a specified boost pressure limiting value and/or a mass flow limiting value m.sub.lim related to component protection. The limiting values can be empirically determined and stored in the control unit 4.