DEVICE AND METHOD FOR CONTROLLING THE COMBINED INJECTION OF AIR AND EXHAUST GASSES AT THE INTAKE OF A SUPERCHARGED INTERNAL-COMBUSTION ENGINE
20190178173 · 2019-06-13
Inventors
Cpc classification
F02D2041/0017
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/164
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/0007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/025
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D9/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D17/105
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/05
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/168
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02D41/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D17/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/05
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D9/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The present invention relates to a device and to a method for controlling the amount of air fed to the intake of a turbocharged internal-combustion engine comprising a turbocharging system including a turbocharger (7) with a turbine (8) connected to at least one exhaust gas outlet of exhaust manifold (5) of said engine, as well as an outside air compressor (10), a line (15, 18) for partial transfer of the compressed air from the compressor to an inlet on the manifold communicating with the turbine, and an EGR line (21) connecting an exhaust gas outlet to a compressed air intake line (4).
Claims
1. A device for controlling the amount of air fed to the intake of a turbocharged internal-combustion engine comprising a turbocharging system including a turbocharger with a turbine connected to at least one exhaust gas outlet of the exhaust manifold of the engine, as well as an outside air compressor, a line for partial transfer of the compressed air from the compressor to an inlet on the manifold communicating with the turbine, and an exhaust gas recirculation line connecting an exhaust gas outlet and a compressed air intake line, wherein the compressed air inlet and the exhaust gas outlet are spaced apart on the exhaust gas manifold.
2. A device as claimed in claim 1, wherein the exhaust gas outlet from the manifold to the turbine is arranged between the inlet of the compressed air inlet and the exhaust gas outlet.
3. A device as claimed in claim 1, wherein the compressed air inlet and the exhaust gas outlet are arranged opposite each other on the exhaust manifold.
4. A device as claimed in claim 1, comprising a controlled throttling system on the compressed air transfer circuit and on the exhaust gas recirculation circuit EGR for controlling the exhaust gas circulation and the compressed air transfer.
5. A device as claimed in claim 4, wherein the throttling system includes at least one valve on recirculated exhaust gas circuit and a valve on partial transfer circuit.
6. A device as claimed in claim 4, wherein the throttling system comprises at least one four-way valve.
7. A method for controlling the amount of air fed to the intake of a turbocharged internal-combustion engine comprising a turbocharging system including a turbocharger with a turbine connected to at least one exhaust gas outlet of exhaust manifold of the engine, as well as an outside air compressor, a line for partial transfer of the compressed air from the compressor to an inlet on the manifold communicating with the turbine, and a recirculated exhaust gas line connecting an exhaust gas outlet and a compressed air intake line, wherein the compressed air inlet and the exhaust gas outlet are spaced apart on the exhaust gas manifold.
8. A method as claimed in claim 7, wherein the exhaust gas outlet from the manifold to the turbine is arranged between the inlet of the compressed air inlet and the exhaust gas outlet.
9. A method as claimed in any one of claim 7, wherein the compressed air inlet and the exhaust gas outlet are arranged opposite each other on the exhaust manifold.
10. Application of the device as claimed in claim 1.
11. A combination of a turbocharged internal-combustion diesel engine and the device as claimed in claim 1 for controlling the amount of air fed to an intake of the turbocharged internal-combustion diesel engine.
12. A method as claimed in claim 7, wherein the turbocharged internal-combustion engine is a turbocharged internal-combustion diesel engine.
Description
BRIEF DESCRIPTION OF THE FIGURES
[0026] 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:
[0027]
[0028]
DETAILED DESCRIPTION OF THE INVENTION
[0029] When operating the EGR circuit and the boost circuit, it should be considered that the average pressure at the intake is generally higher than the average pressure at the exhaust. However, it is known that the instantaneous pressure at the exhaust has phases where it is higher than the instantaneous intake pressure. Thus, it is possible to achieve exhaust gas recirculation but non-return valves are necessary in the EGR circuit.
[0030] To operate the boost circuit under such conditions and simultaneously with the EGR circuit according to the invention, the two circuits are connected on the exhaust manifold at two sufficiently distant points and the exhaust gas outlet towards the turbine inlet is positioned between said two points.
[0031] Thus, the air from the boost circuit will preferably flow towards the turbine inlet instead of substantially mixing with the EGR exhaust gas and disturbing the EGR circulation.
[0032] In
[0033] 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.
[0034] Each cylinder comprises intake means with at least one intake valve controlling an intake pipe 2. The intake pipes lead to an intake manifold 3 supplied with intake air, such as compressed air, through a supply line 4.
[0035] Each cylinder also comprises burnt gas exhaust means with at least one exhaust valve controlling an exhaust pipe leading to an exhaust manifold 5.
[0036] Exhaust gas outlet 6 of the exhaust manifold leads to a turbocharger 7 used for air compression, and more specifically to the expansion turbine 8 of this turbocharger.
[0037] As illustrated in
[0038] The invention is not limited to a single-scroll turbocharger, it is also applicable to twin-scroll turbochargers.
[0039] Gas outlet 9 of turbine 8 is conventionally connected to the exhaust line of the engine.
[0040] Compressor 10 of turbocharger 7 comprises an outside air intake 11 supplied by a supply line. The compressed air outlet of this compressor is connected to supply line 4 of intake manifold 3 by a line 12. The junction point between lines 4 and 12 is denoted by 13.
[0041] Advantageously, a compressed air cooling radiator 14 may be provided on line 12, between compressor 10 and line 4.
[0042] As is better seen in
[0043] More precisely, this partial transfer line 18 originates from line 12, at an intersection point 16 between the compressor and cooling radiator 14. Branch 18 leads to exhaust manifold 5 and to exhaust gas outlet 6 towards turbine 8.
[0044] A line 21 connects exhaust manifold 5 to intake line 4. It preferably runs through an exchanger 22 suited for cooling the exhaust gases.
[0045] Preferably, this line 21, referred to as EGR line, is connected to an orifice of the exhaust manifold provided at a distance from the inlet intended for the air from the boost circuit delivered by transfer line 18. Furthermore, gas outlet line 6 is arranged between the outlet orifices of the EGR circuit and the inlet orifices of the boost circuit so as to be compatible with the fluid circulations induced by the EGR and boost circuits.
[0046] Lines 18 and 21 are respectively equipped with valves 23 and 24, preferably proportional valves.
[0047] Branch 18 also comprises a non-return valve 20, which prevents circulation of the fluids from the exhaust manifold to compressor 10, and EGR line 21 also comprises a non-return valve 25.
[0048] This configuration thus allows, during operation of the engine, to take advantage of the exhaust low-pressure zones occasionally prevailing in the exhaust manifold 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 turbocharging at low engine speeds, and notably to manage transient phases with suitable control strategies for the proportional valves.
[0049] During operation, in case a large amount of air is required in the cylinders, opening of valve 23 is controlled so as to feed compressed air from compressor 10 into turbine 8. Valve 24 is controlled concurrently in order to obtain recirculated exhaust gases if necessary at this operating point.
[0050] The compressed air exiting compressor 10 circulates in line 18 prior to reaching the exhaust gas inlet of turbine 8, thus providing surplus fluid supply to this turbine.
[0051] Thus, the turbine is traversed not only by the exhaust gases from manifold 5, 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.
[0052] In this configuration, the air of the boost circuit does not flow through exchanger 14.
[0053] In order to operate with recirculated exhaust gases, valve 24 is open. A portion of the exhaust gases is fed into intake line 4 after passing through exchanger 22. This operates when the average pressure at the exhaust is higher than the average pressure at the intake.
[0054] It can be noted that valves 23 and 24 may be replaced with a multi-way valve whose function is equivalent for controlling the various flow passage instances.
[0055] Furthermore, it is clear that valve 24 (EGR valve) can be arranged upstream (
[0056] Thus, in the present invention, the respective positions:of the branch connection of the EGR line,of line 6 communicating with the inlet of turbine 8, andof the inlet of the air transfer line 18 of the boost circuit enable optimized simultaneous operation of the EGR circuit and the boost circuit.
[0057] The variant of
[0058] Therefore, the four ways are: [0059] (a) inlet of the EGR line, [0060] (b) outlet of the EGR line towards intake 3, [0061] (c) inlet of the boost circuit air portion, [0062] (d) outlet of the boost circuit air towards turbine 8.
[0063] Depending on the position of the rotary ball, the following configurations can be selected: [0064] EGR and boost by communicating (a) and (b), (c) and (d), [0065] EGR alone by communicating (a) and (b), and (c) closed, [0066] Boost alone by communicating (c) and (d), and (b) closed, [0067] No EGR and no boost by closing all the ways.