Patent Application
20180149075
The present invention relates to a method of controlling a device feeding an amount of air to the intake of a supercharged internal-combustion engine, notably a stationary engine or an automotive or industrial vehicle engine.
As it is widely known, the power delivered by an internal-combustion engine depends on the amount of air fed to the combustion chamber of this engine, which is itself proportional to the density of this air.
Thus, it is usual to increase this amount of air through compression of the outside air before it is allowed into the combustion chamber. This operation, known as supercharging, can be carried out by any means such as a turbocharger or a driven compressor, which can be a centrifugal or a positive-displacement compressor.
In case of supercharging using a turbocharger, the latter comprises a rotary single-flow or double-flow turbine connected by a shaft to a rotary compressor. The exhaust gases from the engine flow through the turbine, which is then rotated. This rotation is thereafter transmitted to the compressor which, by its rotation, compresses the outside air before it is fed to the combustion chamber.
As is better described in French patent application No. 2,478,736, it is intended to increase the compression of the outside air by the compressor even further so as to be able to significantly raise this amount of compressed air in the compression chamber of the engine.
This is achieved in particular by increasing the rotational speed of the turbine and therefore of the compressor.
Part of the compressed air exiting the compressor is therefore diverted in order to be directly allowed to the turbine inlet while mixing with the exhaust gases. This turbine is then traversed by a larger amount of fluid (mixture of compressed air and exhaust gas), which allows the rotational speed of the turbine, and therefore of the compressor, to be increased. This compressor speed increase thus allows to raise the pressure of the outside air that is compressed in this compressor prior to being fed to the combustion chamber of the engine.
Thus, the compressed air has a higher density, which allows the amount of air contained in the combustion chamber to be increased.
This type of supercharged engine, although satisfactory, however involves some not insignificant drawbacks.
Indeed, the flow of compressed air admitted at the turbine inlet is not correctly controlled, which may lead to dysfunctional engines.
Thus, by way of example, in case of too large amounts of compressed air diverted to the turbine inlet, the exhaust gases entering the turbine are cooled too much by this air, which causes a decrease in the overall supercharging efficiency.
The present invention aims to overcome the aforementioned drawbacks with a method of controlling a device feeding an amount of air to the intake of a supercharged internal-combustion engine which can meet all engine power requirements, in particular in transient operation phases.
The present invention thus allows to manage and to conduct a compressed air transfer from the intake to the exhaust, even when the average pressure of the compressed air at the intake is lower than that of the gases at the exhaust. All that is needed is phases during the engine running cycle where the intake pressure is higher than the exhaust pressure.
Thus, the present invention relates to a method of controlling the amount of air fed to the intake of a supercharged internal-combustion engine, said engine comprising two exhaust gas outlets connected each to an exhaust manifold of a group of at least one cylinder, comprising a supercharging device including a turbocharger with a dual-inlet turbine connected to said exhaust gas outlets, as well as an outside air compressor, and a duct for partial transfer of the compressed air from the compressor to the turbine inlets, characterized in that two branches are provided on said partial transfer duct, said branches being connected to the turbine inlets and carrying each proportional throttling means, and in that the compressed air circulation in the branches is controlled during transient operation phases according to strategies applied to said throttling means and determined in accordance with the stabilized phase characteristics.
A non-return valve can be further arranged on each of said branches.
The branches can be connected by a connecting line.
The connecting line can be provided with throttling means.
The compressed air circulating in the transfer duct can be heated.
For a control strategy, the following steps can be carried out:
The initial state can be a low-load state and the final state a high-load state.
The throttling means opening setting states for the initial and final stabilized states can be identical.
Other features and advantages of the invention will be clear from reading the description hereafter, given by way of non limitative example, with reference to the accompanying figures wherein:
In
Preferably, this engine is a direct-injection internal-combustion engine, notably of Diesel type, which by no means excludes any other type of internal-combustion engine.
Each cylinder comprises intake means 14 with at least one intake valve 16, here two intake valves controlling each an intake pipe 18. Intake pipes 18 lead to an intake manifold 20 supplied with intake air, such as compressed air, through an intake air supply line 22.
This cylinder also comprises burnt gas exhaust means 24 with at least one exhaust valve 26, here also two valves controlling each an exhaust pipe 28.
In the example shown, the engine is designed to operate with a firing order 1-3-4-2. Considering this firing order, the exhaust pipes of first cylinder 121 and second cylinder 124 making up a first group of at least one cylinder are connected to a first exhaust manifold 30 with a first exhaust gas outlet 32. The exhaust pipes of the third and fourth cylinders 122 and 123 making up a second group of at least one cylinder are connected to a second exhaust manifold 34 comprising a second exhaust gas outlet 36.
The two exhaust gas outlets open into a turbocharger 38 for compression of the air and more particularly into expansion turbine 40 of this turbocharger.
As illustrated in
This type of turbocharger comprises expansion turbine 40 scavenged by the exhaust gas, which is connected in rotation by a shaft 42 with a compressor 44.
At the turbine, the exhaust gas inlet is divided into two sections, a first inlet section 46 connected to first exhaust gas outlet 32 of first manifold 30 and a second inlet section 48 connected to second exhaust gas outlet 36 of second exhaust manifold 34.
Gas outlet 50 of turbine 40 is conventionally connected to exhaust line 52 of the engine.
Compressor 44 of turbocharger 38 comprises an outside air intake 54 supplied by a supply line 56. Compressed air outlet 58 of this compressor is connected to supply line 22 of intake manifold 20 by a duct 60.
Advantageously, a compressed air cooling radiator 62 may be provided on duct 60, between the compressor and line 22.
As is better seen in
More precisely, this partial transfer duct originates from duct 60 at an intersection point 66 between the compressor and cooling radiator 62, and it divides at a bifurcation point 68 into two branches 70 and 72. Branch 70 leads to turbine inlet 46 through its junction with first exhaust gas outlet 32 and branch 72 leads to the other inlet 48 of this turbine through its junction with exhaust gas outlet 36.
Each branch carries throttling means 74 and 76, such as a proportional valve, controlled by a control means 78 that can be shared by the two throttling means. Each proportional valve thus allows to control the flow rate of the compressed air stream circulating in each branch 70 and 72.
Advantageously, each branch also comprises a non-return valve 80 and 82 preventing compressed air circulation from the branch to the compressor while preventing communication between the two branches.
This configuration thus allows, during operation of the engine, to take advantage of the exhaust low-pressure zones occasionally prevailing in the exhaust manifolds in order to feed compressed air into the turbine and thus to increase the flow rate of this turbine, and therefore of the compressor. This also allows to achieve more efficient supercharging at low engine speeds and notably to manage the transient phases with suitable proportional valve control strategies.
During operation, in case a large amount of air is required in the cylinders, opening of valves 74 and 76 is controlled so as to feed compressed air from compressor 44 into turbine 40.
The compressed air exiting compressor 44 circulates in duct 64, then in branches 70 and 72 prior to reaching exhaust gas inlets 46 and 48 of turbine 40, thus providing surplus fluid supply to this turbine.
Thus, the turbine is traversed not only by the exhaust gases from outlets 32 and 36, but also by compressed air that comes on top of these gases. Therefore, the rotation of the turbine is increased, which causes an increase in the rotation of the compressor and, consequently, an increase in the pressure of the compressed air exiting this compressor.
Valves 74 and 76 are controlled by control means 78 so as to allow the amount of compressed air into the turbine according to the engine supercharging requirements, in particular during the transient phases between two stabilized operation phases.
The variant of
One of the ends of this line is connected to branch 70 at a point between valve 74 and exhaust gas outlet 32, and the other end at a point between valve 76 and exhaust gas outlet 36.
This line allows to control the fluid communication between the two branches arriving at the turbine.
More precisely, this connecting line allows to divert part of the compressed air circulating in one of the branches so as to feed it into the other branch while mixing with the exhaust gases at the inlets of turbine 40.
Furthermore, the connecting line allows to put on a branch of the turbine the pressure differential of the exhaust gas (or exhaust pulsatile flow) of the other branch that is angularly offset in the engine combustion cycle.
In
Transfer duct 64 therefore carries a compressed air heating means 88, here a heat exchanger in form of a heating radiator, arranged between intersection point 66 and bifurcation point 68 included in this duct. This radiator is traversed by the compressed air circulating in the duct while being traversed by the engine exhaust gases. These exhaust gases come from outlet 50 of the turbine and they are carried by a pipe 90 to inlet 92 of the radiator. The exhaust gases flow through this radiator by transferring the heat they contain to the compressed air prior to exiting this radiator through outlet 94 where they are sent to the engine exhaust line.
Thus, part of the energy of the exhaust gases is recovered by the compressed air that is fed to the turbine through either of inlets 46 and 48.
This heated compressed air thus allows to provide additional energy to the turbine, which consequently rotates at higher speed. This high rotational speed is then transmitted to the compressor, which will perform greater compression of the outside air.
The present invention is particularly well suited for managing the transient operation phases between two stabilized operation phases. “Stabilized operation” is understood to be a state wherein all of the engine actuators are not modified, for example when the amounts of fuel injected are constant over time, the EGR rate remains constant, the actuator of the turbocharger is in the same position, etc. Conversely, “transient operation” is understood to be the phase wherein some actuators are activated in response to an evolution of the user's power request. One example is the case of a “load build-up” where the user requests the engine to switch from a low-load state (low torque, low power) to a high-load state (high torque, high power). This load build-up can be achieved either at constant engine speed, or with simultaneous load and engine speed increase. The example of a “slowdown”, i.e. a more or less sudden decrease in torque request, can also be considered. In each case, the engine actuators need to be controlled in order to ensure optimal operation of the powertrain.
The present improvement consists in optimizing the engine dynamics during transient operation by controlling the opening and closing of the proportional throttling means allowing gas passage from the compressed air partial transfer duct to the inlets of turbine 40.
In general, these transient phases can be defined as transition phases between two stabilized states where the scavenging level, enabled by proportional valves 74 and 76, is stabilized and optimum as regards the engine performances expected at each of these operating points. Optimum control of the partial transfer loop throttling means consists in applying a predetermined strategy for the evolution of the throttling means closing or opening trajectory, for switching from one stabilized state to another stabilized state under optimized conditions.
In
Selection of the optimum proportional valve management method during the transient phase essentially depends on the characteristics of the initial stabilized operating point (point A) and on those of the targeted stabilized operating point (point B). In other words, the throttling means control strategy needs to be optimized so as to best match the characteristics of the engine operating points (load, speed, flow, richness, time spent at each operating point, etc.) and of the supercharging operating points (rotational speed, surge margin, etc.).
The case of a load build-up, i.e. a fast increase in the engine power request, can be described by way of example. We consider for this example a case of transient operation with three main phases:
“Scavenging” is considered to be active both at the first low-load operating point (first phase) and at the second high-load operating point with a level that may be different from the first phase depending on the engine requirements specific to this load level. It is also envisaged to allow scavenging during the transient phase, at variable levels, according to the examples illustrated above.
The implementations show that a compromise needs to be found between:
A previously identified optimum strategy consists:
This optimum strategy, as well as other simulated cases, is illustrated in
The other curves correspond to a single-supercharged engine equipped with a compressed air partial transfer system, or so-called “scavenging” system, according to the invention. Curve RBE (Reference External Scavenging) corresponds to the case allowing continuous scavenging, i.e. at the low-load point, during the transient phase and at the high-load point.
Curve 1RBE-OFF0.01-STAB2.0-ON0.01 corresponds to a case where the scavenging cut-off delay is 0.01 second, the scavenging ban time is 2.0 seconds and the scavenging restart delay is 0.01 second. It has been observed in this case that a torque “hole” appears when scavenging is restarted after being stopped for too long.
Curve 2RBE-OFF0.01-STAB0.3-ON0.2 finally corresponds to an optimum case where the scavenging cut-off delay is 0.01 second, the scavenging ban time is 0.2 second and the scavenging restart delay is 0.2 second. As can be seen in the figure, this scavenging control strategy allows fast load build-up to be obtained.
| Number | Date | Country | Kind |
|---|---|---|---|
| 1553583 | Apr 2015 | FR | national |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/EP2016/057986 | 4/12/2016 | WO | 00 |
