Patent Application
20120085091
The invention relates to four-stroke reciprocating internal combustion engines, in particular those that are turbocharged, of which the combustions are equally-distant in time and which comprise several groups of two or three cylinders of which the exhaust phases do not interfere with one another, such as the V12 and the V8 which have four groups of cylinders or the six and four cylinders in a V-configuration or in line which have two groups of cylinders.
The invention applies more particularly to engines with a high rate of burnt gas recirculation in order to reduce nitrogen oxide emissions by implementing the method of FR 2 909 7188A 1 which discloses an application with a group of four cylinders. This method consists substantially in separating the mass of hot gases emitted at each cycle by a cylinder into a first highly energetic puff resulting from the pressure drop at the time of the opening of the exhaust ports which will be expanded in a turbine and a second less energetic residual mass which will be discharged by the piston during its exhaust stroke into a bypass pipe communicating with the intake manifold and/or with the outlet of said turbine. It occurs that the puff expanded down to the intake pressure in the neighborhood of the bottom dead centre of the piston represents between 50% and 60% of the total mass emitted by the cylinder and that the remaining 50% to 40% fraction falls close to the recirculation rate required to remove the nitrogen oxides. This coincidence makes it possible to conclude that a selective use of the puff and of the mass of gas remaining in the cylinder provides simultaneously a maximum power to the turbine, a total removal of the nitrogen oxides and a pumping work of the pistons in the neighborhood of zero.
In the alternative where the bypass pipe does not communicate with the inlet manifold, the pressure in the bypass pipe can be much below the intake pressure and approach atmospheric pressure when it communicates with the outlet of the turbine. In this case, the second mass of hot gases discharged by the pistons represents only a low fraction of the total mass emitted at each cycle which will be almost entirely expanded in the turbine. This alternative makes it possible to improve the output of a four-stroke engine by generating a positive work during the intake-exhaust transfer cycle.
This invention has in particular for object to extend the application of this method to engines comprising several groups of cylinders supplying the same turbine through an undivided nozzle, and to optimize its impact on the reduction of the consumption of fuel and of polluting emissions.
It is already known to expand the puffs emitted by the exhaust manifold of a group of two or three cylinders in a turbine assigned to this group or in a turbine that is common to several groups, turbine of which the nozzle is divided. This method however loses its effectiveness when a port is opened permanently in the exhaust manifold in order to divert a fraction of the burnt gases towards the intake manifold or towards the outlet of a turbine. Indeed, this additional outlet swallows a portion of the puff which is not expanded in the turbine. The aforementioned document solves this problem by periodically closing the bypass port during the blow down period and by guaranteeing as well as that the entire puff is expanded in the turbine. The effectiveness of the concept increasing with the number of cylinders which supply the same turbine, it is advantageous to link all of the manifolds of the engine to a single turbine through a nozzle which is not divided. To do this, the confluence of the manifolds must be organized at the inlet of the turbine without creating communications which would allow the puffs or one of them to rise into another.
As a first approximation, the time needed for the expansion of a puff of exhaust gases is inversely proportional to the discharge area of the turbine. As such, for a fixed area turbine, the angular duration of the puff is proportional to the speed of rotation of the engine. Yet, the angular duration of the puff must not exceed 60 crank angle degrees surrounding the bottom dead centre of the piston in order to minimize the negative work of the exhaust stroke of the piston. An increase in the section of the turbine is therefore required in order to balance the effect of an increase in speed. The application of the invention to variable speed engines (road traction) will therefore be articulated, more preferably, around a variable area turbine of which the nozzle comprises pivoting vanes arranged around the rotor.
Moreover, as the duration of the puff is set to 60 crank angle degrees, the angular period separating two consecutive puffs, a period when the turbine is supplied with less energetic gases, is inversely proportional to the number of cylinders which supply the turbine. This period is respectively: 180 degrees for three cylinders; 120 degrees for four cylinders; 60 degrees for six cylinders: 40 degrees for eight cylinders; 0 degrees for twelve cylinders. These figures show the interest of increasing the number of cylinders supplying the same turbine in order to minimize the fraction of the low energetic gases that supply it. A single turbine will therefore receive the puffs of all of the cylinders of the engine.
As such the turbine of eight- or twelve-cylinder engines mostly expands highly energetic puffs. For smaller numbers of cylinders, either the turbine is partially supplied with less energetic gases, or the angular duration of the puffs is extended at the price of a larger pumping work of the pistons during exhaust strokes.
With the preceding constraints, the problem to be resolved is to supply a single turbine from several (in practice two or four) exhaust manifolds each linked to a group of two or three cylinders of which the exhaust phases do not interfere with one another, in such a way as to prevent a puff growing in one of the manifolds from flowing into another manifold.
In addition, the means to be provided must also make it possible to put into communication each cylinder with the bypass pipe during the discharge stroke of the piston, in accordance with the aforementioned document.
The invention proposes to this effect a reciprocating internal combustion engine operating on the four-stroke cycle with equally-distant combustions in time and comprising N groups of two or three cylinders of which the exhaust phases do not interfere with one another, cylinders of which the inlet ports are linked to an intake manifold that is common to the N groups and of which the exhaust ports are linked together by an individual exhaust manifold which communicates with a bypass pipe in such a way that the communication is cut off before the opening of the exhaust valves of each cylinder of the group and is re-established before the closing of said valves, characterized in that each individual exhaust manifold is linked to one of the N inlets of an N-channel distributing valve of which the single outlet is linked to the inlet of a turbine that is common to the N groups, valve controlled in such a way as to open an exclusive communication between the turbine and each individual exhaust manifold, at least during the duration of the puffs of exhaust gases emitted by one of the cylinders that it is emptying.
According to the invention, the gas inlet of the single turbine is therefore provided with a valve comprising several inlets ports (in practice two or four) each linked to an individual exhaust manifold and a single outlet linked to the gas inlet of the turbine. The valve is controlled in such a way as to periodically put the turbine in exclusive communication with each individual exhaust manifold at least during the puff of exhaust gases of one of the cylinders that it is emptying. The angular duration of the exclusive periods, which is common to all of the individual manifolds, therefore depends on the duration of the puff, ideally less than 60 degrees of rotation of the crankshaft. Outside of this exclusive period, the turbine may communicate with two manifolds which are not emitting puffs and wherein the pressure is that of the bypass conduit.
Optionally, the same valve can provide the periodical putting into communication of each individual exhaust manifold with the bypass pipe.
According to other characteristics of the invention:
In practice, the most common engines comprise an even number of cylinders divided into two or four groups of two or three cylinders. For the remainder of the description, this will therefore be limited to N=2 (four and 6 cylinders) and N=4 (eight and twelve cylinders).
In the case of an engine comprising two or four groups of two or three cylinders:
The invention shall be better understood and other characteristics, details and advantages of the latter will appear more clearly when reading the following description, provided by way of example in reference to the annexed drawings wherein:
Generally,
Reference will first be made to
The intake manifold 2 is supplied with air by a compressor 4 driven by a turbine 5 of which the nozzle 10 with variable geometry is comprised of a ring of pivoting vanes.
Two examples of routing of the recirculated burnt gases are shown in
On the cylinder bank at the top of the figure, a bypass pipe 7 common to the six cylinders links the exhaust ports 6 via isolation valves 8 to the inlet manifold 2. The isolation valves 8 of each group of cylinders close the communication between its manifold 3 and the bypass pipe 7 before the opening of the exhaust valves 9 of each cylinder of the group and open said communication before the closing of said valves 9. The positioning of the isolation valves 8 as close as possible to the exhaust valves 9 makes it possible to reduce to a minimum the volume of the manifolds 3 without creating resistance to the flow of the returned gases which do not pass through these manifolds. The valves 8 of each group of cylinders can be actuated simultaneously by a specific camshaft driven in synchronism by the crankshaft at 1.5 times the engine speed or be actuated successively by additional cams carried by the exhaust camshaft of the engine.
The other cylinder bank shows another routing of the returned gases which can be considered on the engines with a very high cylinder bore to piston stroke ratio and low piston speed of which each cylinder comprises two large exhaust valves discharging towards two separate cylinder head exhaust ports linked respectively to a manifold 3 and to the pipe 7. The valve linked to the manifold 3 opens before the bottom dead centre of the piston in order to discharge the pressure of the cylinder towards the turbine. The valve linked to the conduit 7 provides the function of the isolation valve 8 by opening after the puff in order to return the residual gases towards the inlet manifold 2. The communication between the manifolds 3 and the inlet manifold 2 then passes through the interior of the cylinders: This very simple solution has the disadvantage of increasing the pumping work of the piston and of reducing the effectiveness of the pressure pulses.
Optionally, a bypass conduit 12 provided with a regulating valve 13 of the flow which passes through it links the bypass pipe 7 to the outlet of the turbine 5. The valve 13 makes it possible to refine the recirculation rate of the burnt gases and the excess air for the combustion and to limit the inlet pressure at high speeds.
The exhaust ports 6 of the four groups of three cylinders are linked to four individual manifolds 3 located inside the V. Each exhaust manifold 3 is linked to one of the four inlets ports 19 of a rotating distributing valve 14. The configuration of the cranks of the crankshaft and the ignition order of the cylinders are chosen so that the manifolds 3 successively emit a puff in the order of the opening of the ports to which they are linked.
The valve 14 comprises a fixed casing with a vertical axis forming a cylindrical cavity closed downwards by a bottom 16, which carries the bearing 17 of the rotor 18 and the pair 21 of bevel gears driven by the crankshaft, and opens upwards on the gas inlet of the turbine 5. The interior cylindrical surface 15 of the casing comprises four rectangular ports 19 with areas substantially equal to the section of the manifolds 3 and arranged angularly every 90 degrees. For the remainder of the description, the angular development of each port 19 is arbitrarily set to 20 degrees. Each of the ports 19 is linked to a manifold 3 according to the ignition order.
The rotor 18, which rotates at 1.5 times the engine speed, comprises a cylindrical shutter 20 coaxial to the inside surface 15 of the casing and adjusted on the latter with a minimal clearance. The shutter 20 of the rotor is open on a sector of 90 degrees in such a way as to close three ports 19 when the fourth is fully open and to maintain the same area supplying the turbine during the transition from one port to the next one. In these conditions, the turbine is supplied by a single manifold 3 over 70 degrees of rotor, which is 47 degrees of crankshaft rotation and supplied by two manifolds 3 during 20 degrees of rotor, which is 13 degrees of crankshaft rotation.
It is clear that the rotor is wedged so that its opening coincides with the axes of two adjacent ports at the time when the pressures in the corresponding manifolds cross. The area of the nozzle of the turbine can be adjusted, in a known manner, by the simultaneous pivoting of the vanes 25 on their axis in order to adjust the angular duration of the puffs according to the recirculation rate/excess air compromise required by the combustion. The turbine is as such supplied with successive puffs in the order that they are emitted by the twelve cylinders of the engine. The rotating valve hereinabove can be used on an eight-cylinder engine when it is made to rotate at the engine speed.
For four and six cylinders, the wall 15 would contain only two ports 19 arranged at 180 degrees and the shutter 20 would be open over 180 degrees, the rotor rotating at the engine speed for four cylinders and at 1.5 times the engine speed for six cylinders.
Reference will now be made to
It is also possible to make use of the invention without modifying the cylinder head of the engines by using an alternative of the rotating valve 14 which, in addition to their communication with the turbine, also manages the communication between the exhaust manifolds 3 and the inlet manifold 2.
The alternative of the valve 14 shown in
This alternative is distinguished from the previous valve by the fact that the cylindrical wall 15 of the fixed casing comprises a second outlet 24 located axially between the ports 19 and the bottom 16. In addition, the disk 23 of the rotor 18 is located axially substantially at mid-height of the inlet ports 19 and carries a second cylindrical shutter 22 on its lower face. This cylindrical sector 22 is developed over 90 degrees and its axial height stops at the upper edge of the outlet port 24. The sector 22 extends the opening of the sector 20 in such a way that, simultaneously, the rotor 18 opens the communication between a manifold 3 and the turbine and closes the communication between this manifold 3 and the bypass conduit 7 and vice versa.
As previously, this alternative can be adapted to four-, six- and eight-cylinder engines with the modifications already described. In addition, the angular development and the wedging of the shutter 22 must be adapted so that it closes a half-port 19 during the duration of the puff. This angular development will therefore be limited to 90 degrees for four and eight cylinders and to 120 degrees for six and twelve cylinders.
Reference will now be made to
Reference will now be made to
In the cases where burnt gases must be recirculated in order to limit NOx emissions, a return conduit 18 links the outlet of the turbine 5 to the inlet of the compressor 4 via a particulate filter 16 and a cooler 17. The non-returned gases are discharged into the atmosphere via a post-treatment device 15. In an alternative, the return conduit 18 can tap its gases downstream of the device 15 and join the inlet of the compressor via a simple refrigerant 17. The pressure in the bypass conduit 7 is then the atmospheric pressure increased by the pressure loss created by the device 15 which must be reduced to the minimum.
The turbine 5 can comprises two turbine stages and the compressor 4 can comprise two compression stages. In this case, it can be advantageous to provide a conduit linking the conduit 12 to the inter-turbine space via a throttling valve 13.
Reference will now be made to
When the totality of the power of the turbine 5 (single-stage or two-stage) is absorbed by the compressor 4 (single-stage or two-stage) that it is driving, the pressure in the inlet manifold 2 can exceed the threshold compatible with the mechanical resistance of the engine when the latter is operating at high load. It is advantageous in this case to prematurely close the inlet valves in order to partially expand the intake air at the end of the intake stroke (Miller cycle).
The additional power can also be tapped on the shaft of the turbine 5 as described above.
| Number | Date | Country | Kind |
|---|---|---|---|
| 09 01538 | Mar 2009 | FR | national |
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/FR2010/000247 | 3/23/2010 | WO | 00 | 12/12/2011 |
