INTERNAL COMBUSTION ENGINE AND A METHOD FOR OPERATING AN INTERNAL COMBUSTION ENGINE
20230167762 · 2023-06-01
Inventors
- Nikolaus Spyra (Innsbruck, AT)
- Herbert Schaumberger (Muenster, AT)
- Jochen Fuchs (Wattens, AT)
- Wolfgang Fimml (Maurach in Tirol, AT)
Cpc classification
F02D41/0027
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B19/1061
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M21/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B19/1052
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/024
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B19/1028
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/0644
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/12
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F02D41/0025
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/30
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F02M21/0275
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B2043/106
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B19/1047
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B43/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B19/1038
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B19/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B19/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/081
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B19/1057
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M21/0206
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02B19/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B19/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B19/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An internal combustion engine comprising: a main combustion chamber comprising at least one intake valve and at least one exhaust valve, wherein at least one intake port fluidically connected to an intake manifold is configured to supply an air and/or an air-fuel-mixture to the main combustion chamber via the at least one intake valve, and a pre-chamber which is in fluid connection with the main combustion chamber, wherein the pre-chamber is in fluid connection with the intake port and/or the intake manifold through a supply line, wherein at least one fuel injector is configured to enrich the air and/or air-fuel-mixture supplied to the main combustion chamber to have a lower ignition delay than an air-fuel-mixture supplied to the pre-chamber and/or air or air-fuel-mixture can be supplied to the pre-chamber to have a higher ignition delay than an air-fuel-mixture supplied to the main combustion chamber.
Claims
1. A system, comprising: an internal combustion engine, comprising: a main combustion chamber comprising at least one intake valve and at least one exhaust valve, wherein at least one intake port fluidically connected to an intake manifold is configured to supply an air and/or an air-fuel-mixture to the main combustion chamber via the at least one intake valve; a pre-chamber in fluid connection with the main combustion chamber, wherein the pre-chamber is in fluid connection with the intake port and/or the intake manifold through a supply line; and at least one fuel injector is arranged in the intake port and/or in the intake manifold and/or in the main combustion chamber, wherein the at least one fuel injector is configured to enrich the air and/or air-fuel-mixture supplied to the main combustion chamber to have a lower ignition delay than an air-fuel-mixture supplied to the pre-chamber, and/or air or air-fuel-mixture can be supplied to the pre-chamber to have a higher ignition delay than an air-fuel-mixture supplied to the main combustion chamber.
2. The system as set forth in claim 1, wherein the at least one fuel injector is arranged in a flow direction downstream of a branch of the supply line of the pre-chamber and the intake port and/or the intake manifold.
3. The system as set forth in claim 1, comprising at least one throttle valve disposed in the supply line of the pre-chamber.
4. The system as set forth in claim 3, wherein the at least one fuel injector is arranged in a flow direction upstream of a branch of the supply line of the pre-chamber and the intake port and/or the intake manifold, further comprising a control configured to control the throttle valve, wherein the control is configured to close the throttle valve when a volume of air or air fuel mixture enriched by the at least one fuel injector passes the branch of the supply line of the pre-chamber and the intake port and/or the intake manifold.
5. The system as set forth in claim 1, wherein the at least one fuel injector is configured as a hydrogen injector.
6. The system as set forth in claim 1, comprising a gas mixer and/or at least on further fuel injector configured to provide the air-fuel-mixture for the main combustion chamber, wherein a first fuel supplied by the at least one further injector and/or the gas mixer is different from a second fuel supplied by the at least one fuel injector.
7. The system as set forth in claim 1, wherein the internal combustion engine comprises a stationary gas engine coupled to a generator.
8. A method, comprising: supplying an air or air-fuel-mixture to a main combustion chamber of an internal combustion engine; and supplying an air-fuel mixture to a pre-chamber of the internal combustion engine, wherein the air or air-fuel-mixture suppled to the main combustion chamber has a lower ignition delay than the air-fuel-mixture supplied to the pre-chamber.
9. The method as set forth in the claim 8, comprising supplying a fuel enrichment to the air or air-fuel-mixture supplied to the main combustion chamber before it is supplied to the main combustion chamber, wherein the fuel enrichment comprises a second fuel having a lower ignition delay than a first fuel of the air-fuel-mixture supplied to the pre-chamber.
10. The method as set forth in claim 9, wherein the air or air-fuel-mixture supplied to the main combustion chamber is enriched during an intake stroke by the second fuel supplied to an intake port and/or an intake manifold between a supply line of the pre-chamber and the intake port and/or the intake manifold; or directly to the main combustion chamber.
11. The method as set forth in claim 9, wherein the same air-fuel-mixture is used for the air-fuel-mixture supplied to the pre-chamber and the air-fuel-mixture supplied to the main combustion chamber before the fuel enrichment.
12. The method as set forth in claim 11, wherein a supply line of the pre-chamber comprises a branch from an intake port and/or an intake manifold of the main combustion chamber, wherein a fuel injector is configured to provide the fuel enrichment in the intake port and/or the intake manifold for enrichment of the air or air-fuel-mixture supplied to the main combustion chamber, wherein the supply of the pre-chamber via the supply line is stopped when a volume of air or air fuel mixture enriched by the at least one fuel injector passes the branch of the supply line of the pre-chamber and the intake port and/or the intake manifold.
13. The method as set forth in claim 9, comprising timing the fuel enrichment of the air or air-fuel-mixture supplied to the main combustion chamber 12 to stop when an intake valve of the main combustion chamber is closed, wherein after closing of the intake valve air or an air-fuel-mixture is supplied to the pre-chamber via an intake port and/or an intake manifold.
14. The method as set forth in claim 13, wherein the air-fuel-mixture is supplied to the main combustion chamber by the intake valve which is closed during an intake stroke before a piston in a cylinder reaches a bottom dead center position.
15. A method, comprising: controlling a first fuel-air mixture in a combustion chamber relative to a second fuel-air mixture in a pre-chamber of an internal combustion engine, wherein the first fuel-air mixture has a higher ignitability and/or a lower ignition delay relative to the second fuel-air mixture.
16. The system of claim 15, wherein controlling comprises enriching the first fuel-air mixture with a fuel enrichment.
17. The system of claim 16, wherein the fuel enrichment comprises a second fuel different from a first fuel of the first and/or second fuel-air mixtures.
18. The system of claim 17, wherein the first fuel is the same fuel in the first and second fuel-air mixtures.
19. The system of claim 16, wherein the fuel enrichment comprises hydrogen.
20. The system of claim 16, comprising supplying the fuel enrichment downstream from a fuel-air mixer and a branch supply line extending to the pre-chamber.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0096] Further details and advantages of the invention are apparent from the accompanying figures and the following description of the drawings. The figures show:
[0097]
[0098]
[0099]
[0100]
[0101]
[0102]
[0103]
[0104]
DETAILED DESCRIPTION
[0105] In the context of the invention it can be provided, that for all embodiments, the supply line 9 to the pre-chamber 4 can be either branched off the intake manifold 19 and/or the intake port 10. In the case of branching off from the intake port 10, the pre-chamber 4 can be directly fluidically connected to the respective intake port 10. It should be mentioned, that although not every drawing indicates the possibility regarding how the pre-chamber 4 can be supplied, any combination of the embodiments depicted in the drawings is conceivable.
[0106]
[0107] The cylinder 2 may be designed as part of a cylinder liner and/or a crank case. For the purpose of embodiments of the present invention, such components are collectively referred to as cylinder 2.
[0108] The intake port 10 can interface with the main combustion chamber 12 through an intake valve 6.
[0109] The exhaust manifold 11 can interface with the main combustion chamber 12 through an exhaust valve 7.
[0110] The intake valve 6 and the exhaust valve 7 can be actuated by the actuators 8. Example actuators for the intake valve 6 and exhaust valve 7 are a camshaft or hydraulic devices.
[0111] It can be provided that at least one gas mixer 22 is arranged upstream of the intake port 10, wherein by use of the gas mixer 22 a fuel-air-mixture (e.g., a mixture of air and natural gas) can be provided for the intake port 10. Furthermore, at least one compressor can be arranged upstream of the intake port 10, wherein the provided air or air-fuel mixture for the intake port 10 can be charged.
[0112] A pre-chamber 4 communicates with the main combustion chamber 12 via transfer passages 17 and has an ignition source 13 and a pre-chamber gas valve 5 in the form of a check valve, which is connected to a source for an air-gas mixture (as the air-fuel-mixture for the main combustion chamber 12 an the pre-chamber 4). In this embodiment, the source for an air-gas mixture is provided by a gas mixer 22 (indicated by the dotted square). Additionally or alternatively, a further injector 20 could be provided for introducing a gaseous fuel to the intake port 10.
[0113] The ignition source 13 is in this embodiment a spark plug.
[0114] In this exemplary embodiment, the intake port 10 itself serves as the source for the air-gas-mixture.
[0115] The supply line 9, which is formed as a cavity in the cylinder head 16 realizes the source for the air-fuel-mixture for the pre-chamber 4.
[0116] To regulate the quantity of air-gas-mixture that can be fed into the pre-chamber 4, a throttle valve 14 is arranged in the supply line 9 in this exemplary embodiment.
[0117] Furthermore, a tempering device 15 is provided in the form of pre-heating by means of engine coolant, such as water, in order to keep the supply line 9 at a temperature that prevents condensation of the gas-air mixture.
[0118] In the intake port 10, a fuel injector 18 is arranged—in this embodiment provided as a hydrogen injector—wherein the fuel injector 18 is configured to enrich the fuel, air, or air-fuel-mixture supplied to the main combustion chamber 12 with molecular hydrogen.
[0119] During the intake stroke, the pre-chamber 4 is supplied with the same—but not enriched—air or air-fuel-mixture as it is directed to the main combustion chamber 12 before hydrogen enrichment through the fuel injector 18.
[0120] During the compression stroke, the enriched air or air-fuel-mixture of the main combustion chamber 12 is pressed into the pre-chamber 4 through the transfer passages 17, wherein the enriched air-fuel-mixture of the main combustion chamber 12 is mixed with the fuel, air, or air-fuel-mixture of the pre-chamber 4, wherein the same air-fuel-mixture is used for the air-fuel-mixture supplied to the pre-chamber 4 and air-fuel-mixture provided for the main combustion chamber 12 before enrichment.
[0121]
[0122] Furthermore, compared to
[0123] The remaining characteristics are analogous to
[0124]
[0125] The intake port 10 is connected to an intake manifold 19, wherein the intake manifold 19 provides an air-fuel-mixture (e.g., a mixture of air and natural gas) for the intake port 10.
[0126] Intake manifolds 19 are used to provide air or an air-fuel-mixture for more than one main combustion chamber 12 (see also
[0127] The fuel injector 18 is, in this embodiment, provided as a hydrogen injector, wherein the fuel injector 18 is configured to enrich the air-fuel-mixture—provided by the intake manifold 19—supplied to the main combustion chamber 12 with hydrogen.
[0128] During the intake stroke, the pre-chamber 4 is supplied with the air-fuel-mixture provided by the intake manifold 19 via the intake port 10 and the transfer passage 17. During this procedure, the main combustion chamber 12 is also supplied with the (same) air-fuel-mixture provided by the gas mixer 22 via the intake port 10.
[0129] During the intake stroke, the supply of the pre-chamber 4 is stopped by closing the throttle valve 14. This could also be done by closing the pre-chamber gas valve 5 (or e.g., an alternative valve which could be arranged in the transfer passage 17).
[0130] This stopping of a supply of the pre-chamber has to be timed in such a way that the pre-chamber 4 is only scavenged or supplied by an air-fuel mixture of the intake manifold 19.
[0131] After stopping the supply of the pre-chamber 4, the air-fuel mixture of the intake manifold 19 can be enriched by the fuel injector 18, wherein the enriched air-fuel-mixture is supplied to the main combustion chamber via the intake port 10.
[0132] It is not necessary to have this strict timing for stopping the supply of the pre-chamber 4 and starting the enrichment afterwards. It can also be provided that the enrichment is started during the supply of the pre-chamber 4, wherein the supply of the pre-chamber 4 is stopped in the moment when the enriched air-fuel-mixture reaches the throttle-valve 14 or the pre-chamber gas valve 5 or shortly before. Therefore, it is possible (for a short time) that the enrichment and the supply of the pre-chamber 4 happen in parallel.
[0133] Furthermore, it would also be possible to enrich the air-fuel-mixture provided by the intake manifold 19 the whole time, wherein also the enriched air-fuel-mixture would be supplied to the pre-chamber 4, wherein only a lightly enriched air-fuel-mixture could be supplied to the pre-chamber 4 and a more strongly enriched air-fuel-mixture is supplied to the main combustion chamber 12.
[0134] This could be done—for example—by controlling the fuel injector 18 in such a way, that after providing the air-fuel-mixture of the pre-chamber 4 the injection volume supplied by the fuel injector 18 is increased (to provide an enriched air fuel mixture for the main combustion chamber 12, having a lower ignition delay than the fuel of the air-fuel-mixture provided to the pre-chamber 4).
[0135]
[0136] Additionally, a compressor 23 (illustrated by the dotted lines) can be arranged at the intake manifold 19 for providing charged boost pressure in the intake manifold 19 to increase the combustion efficiency. A compressor 23 can be part of a turbo charger or can be mechanically driven (e.g., by connecting the compressor 23 to the crankshaft of the internal combustion engine 1). The compressor 23 could also be arranged downstream of the gas mixer 22 and/or can be provided with more than one compressor stage.
[0137] The supply line 9 for supplying the pre-chambers 4 with an air-fuel-mixture branches in this embodiment from the intake manifold 19 downstream of the gas mixer 22 and upstream of a single fuel injector 21.
[0138] This single fuel injector 21—in this embodiment provided as a hydrogen injector—is configured to enrich the air-fuel-mixture provided by the gas mixer 22 which is supplied to the main combustion chambers 12. Using a single fuel injector 21 in the intake manifold 19, high pressure injections can be performed to enrich the air-fuel-mixture supplied to the main combustion chambers 12.
[0139] Furthermore, in the supply line 9 of the pre-chambers 4, an optional additional fuel or air supply 24 can be provided. If desired, the additional fuel and/or air supply 24 can be used to modify the air-fuel-mixture supplied and/or ignited in the pre-chambers 4.
[0140]
[0141] Furthermore, in this embodiment, it is illustrated that the supply line 9 can also branch from the intake ports 10 upstream of the additional fuel supply 25. Of course, the supply lines 9 can be provided for each pre-chamber 4 separately (as indicated in
[0142] In
[0143]
[0144]
[0145] The air or air-fuel-mixture (depending if the additional dotted illustrated gas mixer 22 is present and/or active) provided by the compressor 23 can be supplied from the intake manifold 19 by the supply line 9 to the pre-chambers 4.
[0146] Downstream of the supply line 9, a single fuel injector 21 is arranged in the intake manifold 19 for enrichment of the air-fuel-mixture or the air provided by the compressor 23. This enriched air-fuel-mixture can further be enriched in the cylinder 2 individually by activating the fuel injectors 18 in the intake ports 10, which intake ports 10 branch downstream of the single fuel injector 21.
[0147] The supply line 9 can additionally branch from the intake ports 10 or the intake manifold 19.
[0148] The remaining components and additional components correspond to the already mentioned ones of the previous Figures.
[0149] The embodiment shown by
[0150] Also, with such an arrangement of the single fuel injector 21, an air or an air-fuel-mixture (depending if the additional dotted illustrated gas mixer 22 is present) can be enriched, and the same enriched air-fuel-mixture can be supplied to the pre-chambers 4 and the main combustion chambers 12, wherein the enriched air-fuel-mixture [0151] is further enriched in the intake ports 10 by the fuel injectors 18 before it is supplied to the main combustion chambers 12 and/or [0152] is mixed with a further fuel or air by the supply 24 before it is supplied to the pre-chambers 4.
USED REFERENCE SIGNS
[0153] 1 internal combustion engine [0154] 2 cylinder [0155] 3 piston [0156] 4 pre-chamber [0157] 5 pre-chamber gas valve [0158] 6 intake valve [0159] 7 exhaust valve [0160] 8 actuators [0161] 9 supply line [0162] 10 intake port [0163] 11 exhaust manifold [0164] 12 combustion chamber [0165] 13 ignition source [0166] 14 throttle valve [0167] 15 tempering device [0168] 16 cylinder head [0169] 17 transfer passages [0170] 18 fuel injector [0171] 19 intake manifold [0172] 20 further fuel injector (intake port) [0173] 21 single fuel injector (intake manifold) [0174] 22 gas mixer [0175] 23 compressor [0176] 24 additional fuel or air supply for the pre-chamber [0177] 25 additional fuel supply for the main combustion chamber