METHOD FOR OPERATING A SUPERCHARGED INTERNAL COMBUSTION ENGINE

Abstract

A supercharged internal combustion engine has cylinder groups with plural cylinders and plural exhaust gas turbochargers. Exhaust gas can be fed to at least one first exhaust gas turbocharger from first outlet valves of the cylinders of the first and second cylinder groups via at least one first exhaust manifold. Exhaust gas can be fed to at least one second exhaust gas turbocharger from second outlet valves of cylinders of the first and second cylinder groups via a second exhaust manifold. At low rotational speeds and/or in part load and/or non-steady state operation, exhaust gas can be fed via the first exhaust manifolds that are connected to the first outlet valves per cylinder group to a turbine of the first exhaust gas turbocharger in flows that can be divided in the inflow region of the turbine, while the second exhaust gas turbocharger is inactive.

Claims

1. A method for operating a supercharged internal combustion engine having a plurality of cylinder groups each of which has a plurality of cylinders and having a plurality of exhaust gas turbochargers arranged so that exhaust gas can be fed to at least one first exhaust gas turbocharger from first outlet valves of the cylinders of the first cylinder group and from first outlet valves of the cylinders of the second cylinder group via at least one first exhaust manifold, and so that exhaust gas can be fed to at least one second exhaust gas turbocharger from second outlet valves of cylinders of the first cylinder group and from second outlet valves of cylinders of the second cylinder group via a second exhaust manifold, wherein the method comprises, at low rotational speeds of the internal combustion engine and/or in part load and/or non-steady state operation, feeding exhaust gas via the first exhaust manifolds that are connected to the first outlet valves per cylinder group to a turbine of at least the first exhaust gas turbocharger in flows dividing the exhaust gas in the inflow region of the turbine, whereas the second exhaust gas turbocharger is inactive.

2. The method of claim 1, wherein the inactivity of the second turbocharger can be achieved as a consequence of a valve stroke=0 or a minimum valve stroke of the second outlet valves that are connected to the second exhaust manifolds.

3. The method as claimed in claim 1, further comprising combining the exhaust gas volumetric flow can be combined via an expansion tube, the second exhaust manifolds of the two cylinder groups being flap-controlled or valve-controlled.

4. An exhaust gas routing system for an internal combustion engine, comprising first exhaust manifolds having a small cross section and connected with a small length to the exhaust gas inlet into the turbine of the first exhaust gas turbocharger.

5. The exhaust gas routing system for an internal combustion engine of claim 4, wherein: the second exhaust manifolds are connected with a large cross section for generating a homogeneous volumetric flow to the exhaust gas inlet into the turbine of the second exhaust gas turbocharger.

6. The exhaust gas routing system of claim 1, further comprising separately running inflow ducts arranged at least in the turbine of the first exhaust gas turbocharger for introducing the divided exhaust gas flows.

7. The exhaust gas routing system of claim 1, wherein the inflow ducts of all turbines of the exhaust gas turbochargers are configured as separately running spiral ducts.

8. The exhaust gas routing system of claim 1, wherein the second outlet valves are designed for early opening for feeding the exhaust gas flow to the second turbine of the second exhaust gas turbocharger.

9. The exhaust gas routing system of claim 8, wherein the early opening of the second outlet valves takes place via a cam having a broad profile and disposed on a camshaft, the cam being operative to control the inlet and/or the outlet valves.

10. The exhaust gas routing system of claim 8, wherein the turbine of the exhaust gas turbochargers is configured as a radial, an axial or mixed flow turbine.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0023] FIG. 1 is a diagrammatic illustration of the course of the exhaust gas flows via the outlet valves of a six-cylinder internal combustion engine, arranged into two cylinder groups with the associated exhaust gas turbochargers.

[0024] FIG. 2 shows the boost pressure profile during operation with one turbocharger in contrast to the boost pressure profile during operation with two turbochargers.

[0025] FIGS. 3, 4, 5, 6 and 7 diagrammatically show a partial cross section of turbine housings and the inflow regions thereof for carrying out the inventive method.

DETAILED DESCRIPTION

[0026] An internal combustion engine 1 in accordance with one embodiment of the invention has two cylinder groups 2 and 3. The cylinder group 2 has three cylinders 2.1, 2.2 and 2.3, and the cylinder group 3 has three 3.1, 3.2 and 3.3. Each of the cylinders 2.1, 2.2 and 2.3 or 3.1, 3.2 and 3.3 has two inlet valves 4 and two outlet valves 5.1 and 5.2. The outlet valves 5.1 of all three cylinders 2.1, 2.2 and 2.3 of the first cylinder group 2 are connected in series via a common exhaust manifold 6 with regard to the exhaust gas flow after a combustion operation in the cylinders. The outlet valves 5.1 of the cylinders 3.1, 3.2 and 3.3 of the second cylinder group 3 likewise are connected via a common exhaust manifold 7 with regard to their exhaust gas flow after a combustion operation in the cylinders. In the exemplary embodiment of FIG. 1, the exhaust manifolds 6 and 7 open into an exhaust gas inflow region of the at least one turbine 8.2 or 12.2 of the at least one exhaust gas turbocharger 9.2 or 11.2. In the exemplary embodiment according to FIG. 1, the exhaust gas turbocharger 9.2 or 11.2 can be switched on or off depending on the operating conditions.

[0027] At low rotational speeds of the internal combustion engine and/or in part load and/or non-steady state operation, the outlet valves 5.1 in both cylinder groups 2 and 3 are closed via, for example, corresponding cams on a camshaft that actuates the inlet and outlet valves, that is to say are provided with a stroke=0 or at any rate with a minimum stroke. Thus, in these combustion cycles, the entire exhaust gas flow is fed exclusively or virtually exclusively via the outlet valves 5.2 and via exhaust manifolds 13.1, 13.2, 13.3 or 14.1, 14.2, 14.3 that are configured to be relatively short and with a low cross section. The exhaust gas flow then continues to the turbine/turbines 8.1 or 12.1 of the exhaust gas turbochargers 9.1 and 11.1 that are arranged parallel to the exhaust gas turbocharger/turbochargers 9.2 or 11.2. This achieves a situation where a pulse-like process of the supercharging takes place in the exhaust gas turbocharger via the combustion cycles of the internal combustion engine in low rotational speed ranges and leads to a satisfactory response behavior of the supercharged internal combustion engine.

[0028] In the exemplary embodiment of FIG. 1, the exhaust manifolds 13.1, 13.2, 13.3 or 14.1, 14.2, 14.3 are shown as lines that are routed separately to the inflow region into the turbines 8.1 or 12.1. However, it is also readily conceivable, in a similar manner to the exhaust manifolds 6 and 7, to combine the exhaust gas flow that is ejected from the outlet valves in one line or to route it within a common exhaust manifold into, for example, three separate line ducts, and then to divide the exhaust gas flow in the inflow region into the turbines 8.1 or 12.1 into a plurality of (for example, three) flows; see the following detailed explanation with respect to FIGS. 3 to 7.

[0029] The two exhaust manifolds 6 and 7 ideally are configured as a connection that is as direct as possible between the outlet region of the outlet valves 5.1 and the inflow region of the turbine 8.2 or 12.2 of the exhaust gas turbocharger/turbochargers 9.2 or 11.2. The exhaust manifolds 6 and 7 preferably are designed with a great cross section for large volumetric flows. The homogeneous supercharging or ram induction that is desired at high rotational speeds and/or at full load of the internal combustion engine is achieved first of all by virtue of the fact that the exhaust manifolds 13 and 14 are configured with a relatively great cross section. In addition, a correspondingly large volume can be produced by way of a corresponding adaptation of the length of the exhaust manifolds 6 and 7, with the result that a homogeneous volumetric flow is set.

[0030] In relatively high load operation of the internal combustion engine 1 and/or at full load, that is to say at correspondingly higher or high rotational speeds, the outlet valves 5.1 of the two cylinder groups 2 and 3 are opened, once again controlled via cams of the camshaft. The opening ideally takes place via a cam, configured with a very broad profile, for controlling the outlet valves 5.1, with the result that very early opening of the second outlet valves 5.1 takes place and therefore the switching on of the exhaust gas turbocharger/turbochargers 9.2 or 11.2 which are connected in parallel to the exhaust gas turbochargers 9.1 or 11.1 can be achieved via the feed of exhaust gas into their turbines 8.2 or 12.2. As a consequence of the early opening, the outlet pulses of the exhaust gas flow out of the cylinders initially are passed only to the exhaust manifolds 6 and 7 that are connected to the outlet valves 5.1 of the two cylinder groups 2 and 3 and are of large-volume configuration. As a result, pressure pulses are reduced or dissipated and a largely homogeneous mass flow in the exhaust manifolds is achieved.

[0031] Moreover, the exhaust manifolds 6 and 7 can be connected via an expansion tube 15 that can be opened or closed by way of flaps 16.1 or 16.2 (or valves). In part load operation and/or at low rotational speeds, the flaps can be closed (as are the outlet valves 5.1). Thus, the first exhaust manifolds 13.1, 13.2, 13.3 or 14.1, 14.2, 14.3, which have a short length and a small cross section to define a small volume, act for ram induction. In full load operation at high rotational speeds the volume for the exhaust gas flows is increased via the opening of the flaps 16.1 and 16.2, so that a corresponding support for the transition from one ram induction to another is achievable.

[0032] FIG. 2 shows a diagram (the boost pressure d is plotted against the rotational speed n) of the relationship between the rotational speed and the boost pressure that can be provided by the exhaust gas turbochargers 9.1 and 11.1. If the outlet valves 5.1 are closed and the exhaust gas turbocharger 9.2 or 11.2 is inactive, a very rapid rise in the boost pressure d in the exhaust gas turbocharger 9.1 or 11.1 is set as a consequence of the low volume and the direct attachment that takes place on the shortest path possible of the exhaust manifolds 13.1, 13.2, 13.3 or 14.1, 14.2, 14.3 to the regions of the outlet valves 5.2 with the inlet region of the turbine 8.1 or 12.1 of the exhaust gas turbocharger 9.1 or 11.1—see curve k1 in FIG. 2. As a consequence of the low volume and the low volumetric flow in the first exhaust manifolds 13.1, 13.2, 13.3 or 14.1, 14.2, 14.3, the boost pressure d could drop abruptly when the rotational speed n of the internal combustion engine rises. To prevent this so-called “turbo lag”, the outlet valves 5.1 are switched on/opened (switch-on range Z in FIG. 2) and therefore the second turbocharger/turbochargers 9.2 and/or 11.2 of the second turbocharger group are/is switched on before the boost pressure d drops. A considerable increase in the volumetric flow to the turbochargers is set by way of the second exhaust manifolds 6 and 7 of correspondingly large-volume configuration, and therefore a transition from the shockwave supercharging to homogeneous ram induction.

[0033] The increase in volume for routing the exhaust gas flow also can be supplemented by opening of the flaps 16.1 and 16.2 in the expansion tube 15. FIG. 2 shows the opening of the expansion tube 15 with the arrows A and B: in the case of arrow A, the expansion tube is closed; it is opened (see arrow B) as soon as the boost pressure d is on the verge of dropping at very high rotational speeds.

[0034] As has already been described, it is expedient to overlap the switch-on range for the second turbocharger 9.2 or 11.2 via early opening of the outlet valves 5.1 with the operating range of the turbocharger/turbochargers 9.1 and/or 11.1. This can be achieved by way of outlet valves 5.1 with a correspondingly broad profiling to make early opening of the second outlet valves 5.1 possible.

[0035] The method according to the invention and/or the exhaust gas routing system for carrying out the inventive method can be assisted appropriately by virtue of the fact that the inflow region of the exhaust gas flow into the turbines of the exhaust gas turbochargers is of corresponding design. Thus, for example, the volumetric flow of the exhaust manifolds 13, 14 and possibly also the exhaust manifolds 6, 7 in the inflow region of the turbine 8.1, 8.2, 12.1, 12.2 can be divided into a plurality of flows. This can take place via a double flow duct 20 or 21 (see FIG. 3; for example, in the case of a four-cylinder internal combustion engine) or via a triple flow with ducts 22, 23 and 24 (for example, in the case of a six-cylinder internal combustion engine; see FIG. 4). The impeller L of the turbine is loaded homogeneously in a manner distributed over its circumference by way of a volumetric flow division of this type.

[0036] FIGS. 5, 6 and 7 diagrammatically show housing designs for turbines of exhaust gas turbochargers. FIG. 5 shows the arrangement of flow ducts in twin form (ducts 25 and 26). FIGS. 6 and 7 show a somewhat different arrangement in twin form using the ducts 27, 28 or 29 and 30.

[0037] It is particularly expedient in every case (this also applies to the twin arrangements of the ducts shown in FIGS. 5-7) to distribute the opening of the ducts onto the impeller L of the turbine in a manner which is offset spirally onto the outer circumference of the impeller L.

[0038] The impeller of the turbine of the exhaust gas turbocharger can be configured as a radial, axial or a “mixed flow” version (radial-axial) by a person skilled in this art.

TABLE-US-00001 List of Designations 1 Internal combustion engine 2 Cylinder group 2.1, 2.2, 2.3 Cylinder 3 Cylinder group 3.1, 3.2, 3.3 Cylinder 4 Inlet valve 5.1 Second outlet valve 5.2 First outlet valve 6 Second exhaust manifold, cylinder group 2 7 Second exhaust manifold, cylinder group 3 8.1 Turbine of exhaust gas turbocharger 9.1 9.1 Exhaust gas turbocharger 9.2 Exhaust gas turbocharger 11.1 Exhaust gas turbocharger 12.1 Turbine of exhaust gas turbocharger 11.1 12.2 Turbine of exhaust gas turbocharger 11.2 13.1, 13.2, 13.3 First exhaust manifold, cylinder group 2 14.1, 14.2, 14.3 First exhaust manifold, cylinder group 3 15 Expansion tube 16.1, 16.2 Flap/valve 20, 21, 22, 23 24, 25, 26, 27 {close oversize brace} Channels in the inflow region, turbine 28, 29, 30 31 Catalytic converter 32 Catalytic converter 33 Muffler 34 Muffler A Closed expansion tube 15 B Open expansion tube 15 Z Switch-on range n Rotational speed d Boost pressure k1 = Curve 1 in FIG. 2 k2 = Curve 2 in FIG. 2 L Impeller