Engines using supercritical syngas
10794340 ยท 2020-10-06
Assignee
Inventors
- Sage Kokjohn (Oregon, WI, US)
- David Wickman (Madison, WI, US)
- Flavio Dal Forno Chuahy (Madison, WI, US)
Cpc classification
F02D41/3035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/3047
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/3041
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/0649
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/0027
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/3023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/0692
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M31/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/0671
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/0689
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/0644
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B2275/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B51/00
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
F01N3/005
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
F02B2201/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2041/3052
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B45/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02D41/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M31/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B45/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B17/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B51/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A first engine fuel, for example diesel fuel, is reformed (preferably via steam reforming) to produce syngas for use as a second engine fuel, with the fuels then both being used in an internal combustion engine to perform Reactivity Controlled Compression Ignition (RCCI). The syngas is produced and supplied to the engine as a supercritical fluid, thereby avoiding the pumping losses that would occur if syngas was pressurized for supply/injection. The reforming is done by a reformer which is provided as a unit with the engine (e.g., both the engine and reformer are onboard a vehicle), thereby effectively allowing use of a single fuel for RCCI engine operation.
Claims
1. A combustion method for an internal combustion engine, the method including the steps of: a. producing syngas from hydrocarbons; and b. supplying the syngas to a combustion chamber of the internal combustion engine, c. supplying the hydrocarbons to the combustion chamber separately from the syngas, wherein: i. the step of producing syngas and the step of supplying the syngas are performed at a temperature and pressure at which the produced syngas is a supercritical fluid, and ii. both the syngas and the hydrocarbons are present in the combustion chamber during combustion.
2. The method of claim 1 wherein the syngas is supplied to the combustion chamber via direct injection.
3. The method of claim 1 further wherein the syngas is present in the combustion chamber at a stoichiometric air-fuel ratio during combustion.
4. The method of claim 1 wherein the hydrocarbons are supplied to the combustion chamber of the internal combustion engine after the syngas.
5. The method of claim 1 wherein the hydrocarbons and the syngas define a stratified mixture within the combustion chamber of the internal combustion engine during a compression stroke, whereby regions of higher hydrocarbon concentration are spaced from regions of higher syngas concentration.
6. The method of claim 1 wherein: a. the syngas is produced from the hydrocarbons in a reformer; and b. the method further includes the step of transferring heat to the reformer from the exhaust gas, wherein the transferred heat is the primary source of heat received by the reformer.
7. The method of claim 1 wherein: a. the syngas is produced from the hydrocarbons via steam reforming, and b. the steam reforming utilizes water captured from exhaust gas from the internal combustion engine.
8. The method of claim 1 wherein the syngas is produced from: a. the hydrocarbons, and b. water, wherein both the hydrocarbons and the water are in a supercritical state.
9. A combustion method for an internal combustion engine, the method including the steps of: a. reforming hydrocarbons to produce supercritical syngas; and b. supplying: (1) the supercritical syngas, and (2) the hydrocarbons separately from the supercritical syngas, to a combustion chamber of the internal combustion engine, whereby the supercritical syngas and the hydrocarbons are concurrently present in the combustion chamber.
10. The method of claim 9 wherein the supplying step includes directly injecting at least a portion of the supercritical syngas into the combustion chamber of the internal combustion engine.
11. The method of claim 9 wherein the supercritical syngas is supplied to the combustion chamber of the internal combustion engine prior to the hydrocarbons.
12. The method of claim 11 wherein the supercritical syngas and the hydrocarbons are stratified within the combustion chamber during a compression stroke, such that regions of higher syngas concentration are spaced from regions of higher hydrocarbon concentration.
13. A combustion method for an internal combustion engine, the method including the steps of: a. producing syngas from hydrocarbons, wherein the syngas is a supercritical fluid from production through injection; and b. separately and directly injecting: (1) the syngas, and (2) the hydrocarbons, into a combustion chamber of the internal combustion engine, whereby both the syngas and the hydrocarbons are present in the combustion chamber at the start of combustion.
14. The method of claim 13 wherein: a. the syngas is produced from the hydrocarbons in a reformer; and b. the method further includes the steps of: (1) transferring heat to the reformer from the exhaust gas, and (2) supplying water to the reformer from the exhaust gas.
15. The method of claim 14 wherein the hydrocarbons and the syngas define a stratified mixture within the combustion chamber of the internal combustion engine during a compression stroke, whereby regions of higher hydrocarbon concentration are spaced from regions of higher syngas concentration.
16. The method of claim 13 wherein the hydrocarbons are injected into the combustion chamber of the internal combustion engine after the syngas.
17. The method of claim 9 further wherein the syngas is present in the combustion chamber at a stoichiometric air-fuel ratio during combustion.
18. The method of claim 9 wherein: a. the syngas is produced from the hydrocarbons in a reformer; and b. the method further includes the step of transferring heat to the reformer from the exhaust gas, wherein the transferred heat is the primary source of heat received by the reformer.
19. The method of claim 9 wherein: a. the syngas is produced from the hydrocarbons via steam reforming, and b. the steam reforming utilizes water captured from exhaust gas from the internal combustion engine.
20. The method of claim 13 further wherein the syngas is present in the combustion chamber at a stoichiometric air-fuel ratio during combustion.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
DETAILED DESCRIPTION OF EXEMPLARY VERSIONS OF THE INVENTION
(3) The exemplary engine/reformer systems of the aforementioned drawings will now be reviewed. Throughout the following discussion, exemplary temperatures and pressures will be noted for the various fluids used in the systems. It should be understood that these temperatures and pressures may vary depending on the choice of components used in the systems, the fuels used in the systems, ambient conditions, and similar factors.
(4)
(5) Now considering the system's air intake, looking near the bottom middle of
(6) Now considering the system's exhaust, exhaust gas (P=1.0-4.0 bar, T=500-1150K) from the exhaust manifold 126 is first preferably provided to a catalytic converter 128, where an oxidation catalyst further converts any unburned CO and hydrocarbons (if present) to carbon dioxide and water vapor. The hot exhaust is then supplied to the reformer 110 so that its heat assists the reforming process, and then in turn goes to an exhaust heat exchanger 108 to further capture waste heat to assist in converting the input fuel and water into the supercritical state. As the exhaust gas cools in the heat exchanger 108, condensing water vapor may be captured and collected in a tank 130 for use in the reforming process, as will be described in greater detail below. Typically, during ordinary operation of the system, the exhaust will contain more than enough water for use in the reforming process, and any excess water may simply be jettisoned to the surrounding environment. (Conversely, the water tank 130 may be primed with a small amount of water upon first operation of the system so that sufficient water is present to execute reforming.) The water can then be filtered at filter(s) 100, and pumped to high pressure at pump 132 to elevate it closer to the supercritical state (P>250 bar, T=300K). The exhaust heat exchanger 108 can then heat the subcritical water to the supercritical state (P>250 bar, T=800-1150K) for supply to the reformer 110 for production of the supercritical syngas.
(7) Following removal of (at least some) water from the exhaust gas at the exhaust heat exchanger 108 (P=1.5-2.5 bar, T=450-750K), the exhaust drives the input turbine of the turbocharger 120 used to pressurize the engine's ambient air supply. After the exhaust leaves the turbocharger 120 (P=1 bar, T=400-650K), it may be further cooled in an exhaust-to-air aftercooler/condenser 134 to further condense any residual water for supply to the water tank 130. The exhaust is then released to the environment (P=1 bar, T=300K).
(8) Because combustion is at relatively low temperature compared to traditional diesel combustion, NOx emissions are low or negligible, which beneficially allows the omission of expensive NOx exhaust after-treatment equipment. Nonetheless, if desired, at least some of the exhaust may be used for exhaust gas recirculation (EGR) for further reduction of nitrogen oxide (NOx) emissions. Looking to the exhaust heat exchanger 108, the portion of the exhaust gas which does not drive the turbocharger 120 is cooled at exhaust-to-coolant cooler 136 via heat exchange with engine coolant (P=1.5-2.5 bar, T=350-450K). The cooled exhaust gas can then be admitted to the intake manifold 124 as needed via EGR valve 138.
(9) Beneficially, the reformer 110 can typically operate using waste exhaust/engine heat and water captured from the exhaust. At start-up or other conditions where there is low exhaust/engine temperature, heat may be provided to the reformer 110 via a supplemental (electrical or other) heater to heat the fuel and water.
(10)
(11) Looking to the bottom right of
(12) To produce syngas for use as an alternative or additional fuel, the gasoline is filtered at filter 200, and then further pressurized at pump 202 (P>250 bar, T=300K), and heated in heat exchanger 208, to reach a supercritical state (P>250 bar, T=800-1150 K). The supercritical fuel is then provided to a reformer 210 to generate supercritical syngas (P>250 bar, T>800-1150K) consisting of H2, CO, and other trace species. The supercritical syngas may then be provided to a syngas injector 212 for injection into the combustion chamber 206, where it might be ignited via compression ignition or spark ignition, and with or without gasoline in the chamber 206, with the ignition mode and fuel(s) being chosen in accordance with speed/load conditions.
(13) Now considering the system's air intake, looking near the bottom middle of
(14) Now considering the system's exhaust, exhaust gas (P=1.0-4.0 bar, T=500-1150K) from the exhaust manifold 226 is first preferably provided to a catalytic converter 228, where an oxidation catalyst further converts any unburned CO and hydrocarbons (if present) to carbon dioxide and water vapor. The hot exhaust is then supplied to the reformer 210 so that its heat assists the reforming process, and then in turn goes to an exhaust heat exchanger 208 to further capture waste heat to assist in converting the input fuel and water into the supercritical state. As the exhaust gas cools in the heat exchanger 208, condensing water vapor may be captured and collected in a tank 230 for use in the reforming process, as will be described in greater detail below. Typically, during ordinary operation of the system, the exhaust will contain more than enough water for use in the reforming process, and any excess water may simply be jettisoned to the surrounding environment. (Conversely, the water tank 230 may be primed with a small amount water upon first operation of the system so that sufficient water is present to execute reforming.) The water can then be filtered at filter(s) 200, and pumped to high pressure at pump 232 to elevate it closer to the supercritical state (P>250 bar, T=300K). The exhaust heat exchanger 208 can then heat the subcritical water to the supercritical state (P>250 bar, T=800-1150K) for supply to the reformer 210 for production of the supercritical syngas.
(15) Following removal of (at least some) water from the exhaust gas at the exhaust heat exchanger 208 (P=1.5-2.5 bar, T=450-750K), the exhaust drives the input turbine of the turbocharger 220 used to pressurize the engine's ambient air supply. After the exhaust leaves the turbocharger 220 (P=1 bar, T=400-650K), it may be further cooled in an exhaust-to-air aftercooler/condenser 234 to further condense any residual water for supply to the water tank 230. The exhaust is then released to the environment (P=1 bar, T=300K).
(16) The system of
(17) It should be understood that the versions of the invention described above are merely exemplary, and the invention is not intended to be limited to these versions. Rather, the scope of rights to the invention is limited only by the claims set out below, and the invention encompasses all different versions that fall literally or equivalently within the scope of these claims.