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This present application claims priority from U.S. provisional application No. 60/922,152 having the same title as the present invention and filed on Apr. 7, 2007.
The present invention relates to systems and methods for reducing exhaust emissions from internal combustion engines, more particularly, to apparatus and methods for reducing Nitrogen Oxides (NOx), Carbon Monoxide (CO), Hydrocarbon (HC), and Particulate Matter (PM) from compression ignition engines.
Internal combustion engines are subject to limits for exhaust emissions. In addition to improving in-cylinder designs, using Exhaust Gas Recirculation (EGR), and better controlling combustion, an aftertreatment device is normally needed for reducing pollutants, which include Nitrogen Oxides (NOx), Carbon Monoxide (CO), Hydrocarbon (HC), and Particulate Matter (PM), to required levels. In spark ignitions (SI) engines, fuel and air can be pre-mixed stoichiometrically, therefore, not much PM is seen in exhaust air, while CO, HC, and NOx are major pollutants. However, in a compression ignition CI engine, due to heterogeneous fuel-air mixing, PM and NOx are major components in its pollutants, while CO and HC are relatively insignificant.
In CI engines, PM and NOx emissions have strong relations to peak combustion temperature. High peak combustion temperature decreases PM generation while increases NOx emission, and low peak combustion temperature affects emissions reversely. Consequently, in using EGR for adjusting peak combustion temperature, a tradeoff needs to be made between PM level and NOx emission. When both of PM and NOx need to be controlled, normally, two methods are used with an aftertreatment device. One is tuning NOx emission low, and using a high efficiency filter for removing PM. The other one is tuning PM level low, and using lean NOx removing technology, such as urea/ammonia Selective Catalytic Reduction (SCR), Lean NOx Trap (LNT)/NOx Absorber (NAC), and Lean NOx Catalyst (LNC), for controlling NOx emission. In the first method, since PM level is high, the filter needs to be regenerated periodically. The regeneration normally is achieved by heating up the filter to 400° C. to 600° C., and the heating energy is provided by burning fuel in an oxidation catalyst or a burner. Fuel penalty for filter regeneration depends on engine operating conditions and NOx emission level. When a low NOx emission level is required, e.g. according to US2010 standard, NOx emission cannot be over than 0.2 g/bhp·hour, fuel penalty could be a limiting factor for using the particulate filter method.
The other method needs to remove NOx from lean exhaust air. As oxygen, NOx is also an oxidant. Therefore, a selective environment must be created more favorably for reactions reducing NOx, since oxygen concentration is much higher than that of NOx. Among all technologies used in reducing NOx in lean exhaust air, SCR has the highest conversion efficiency, and thus is used broadly. However, a difficulty in developing selective catalyst is that there exist a tradeoff between conversion efficiency and selectivity. A catalyst with high selectivity normally has poor conversion efficiency. As a result, to have high selectivity, a device with a large volume is needed when high conversion efficiency is required.
Though SCR technology needs not dosing fuel, the hydrolysis of urea, which is used in generating ammonia for SCR reactions, is endothermic and needs extra energy. If this energy is provided by burning more fuel in engine, this fuel penalty could be 3% of total engine fuel consumption, depending on operating conditions. Additionally, urea is consumed in reducing NOx. The overall cost of urea consumption and fuel penalty for urea hydrolysis is comparable with cost of fuel penalty in using particulate filter. Combining the particulate filter method and lean NOx reducing method could achieve the best aftertreatment performance. However, the cost is system complexity and fuel penalty.
Different from that in CI engines, in SI engines, when air-fuel ratio is controlled at stoichiometric level, NOx could have a higher or comparable concentration as oxygen. As a result, even in an oxidation catalyst without selectivity, reductant is able to remove NOx from exhaust. This type of catalyst usually is called three-way catalyst, since it uses CO and HC as reductant in removing NOx, consequently, all three pollutants are removed from exhaust.
Compared to SI engines, the lean combustion nature of CI engines creates lean exhaust air, which causes the difficulties in using reductants in exhaust air to reduce NOx. Accordingly if the lean exhaust of a CI engine is converted to rich exhaust, an oxidation catalyst can be used to reduce NOx with reductants. It is a goal of the present invention to provide a means for reducing NOx and other pollutants in lean exhaust air by converting the lean exhaust air to rich exhaust air without significantly sacrificing fuel economy. Furthermore, it is a goal of the present invention to use solely fuel in exhaust air aftertreatment.
In the present invention, a new technology of reducing exhaust pollutants in a CI engine is developed. In this technology, oxygen is firstly removed and then an oxidation catalyst is used for reducing NOx, CO, and HC from exhaust air.
Normally, due to the lean combustion nature, air-fuel ratio in CI engines cannot be stoichiometric. In one embodiment of this invention, oxygen left in exhaust air is removed by using a fuel reactor in which fuel injected during expansion (in-cylinder late injection) or provided by a dedicated doser reacts with oxygen. The fuel reactor act as an air-fuel ratio controller, which adjusts the lambda value of the exhaust air close to 1, thus an oxidation catalyst can be used for effectively reducing NOx, CO and HC. Compared to SI engines, CI engines have better fuel economy: usually CI engines are 30% or more efficient than SI engines. Therefore, it is not economic if the dosing fuel is just used for reducing pollutants from exhaust though comparatively there could also be around 6% fuel penalty or equivalent fuel penalty when using other types of aftertreatment devices such as LNT and SCR.
Heat generated in exhaust lambda control needs to be recovered. Both turbines and heat exchange devices can be used for energy recovery and the energy recovery efficiency determines overall fuel penalty. Ideally, if the energy recovery efficiency is higher than engine efficiency, there will be no fuel penalty in using the fuel reactor.
In another embodiment, oxygen in exhaust air is removed by using an oxygen sorption device, through which oxygen is separated from exhaust. The result rich exhaust air then passes through an oxidation catalyst where NOx, CO and HC are reduced. Once the oxygen sorption device reaches a saturation level, a regeneration process is triggered. During the regeneration, oxygen adsorbed and/or absorbed in the device is removed and the device is ready for the next sorption process. A wheel structure and/or a valve-controlled structure can be used for continuous operation.
As depicted in
An embodiment of the oxygen-removing device is shown in
The reactor can also improve aftertreatment performance at cold-start. When engine starts, the exhaust pressure and temperature is not enough to effectively drive turbo-charger. As a result, large amount of PM could be generated. The reactor can be used for increasing the exhaust temperature and thus improves the transient performance of the turbo-charger and burns PM in exhaust air.
Heat released in the reactor increases exhaust temperature. Suppose the overall temperature gained by exhaust is Tg. When fueling rate in lambda control is small compared to exhaust mass flow,
T
g
=m
fuel
·*LHV/(Cp*mexh·) (1)
where mfuel· is the fuel injection mass flow rate in lambda control, LHV the low heat value of fuel, Cp the specific heat at constant pressure, and mexh· is the exhaust mass flow.
To control the exhaust lambda value at 1, the fueling rate can be calculated using the following equation:
where λ1 is the engine out lambda value, and AF0 is the stoichiometric air fuel ratio.
Based on equation (1) and (2), the exhaust temperature increase across the reactor is
According to the equation (3), the temperature gained by the exhaust air is determined by the lambda value of engine out exhaust air. When the air fuel ratio is high, a very high temperature can be generated. Consequently, the lambda value of engine out exhaust air needs to be carefully controlled, otherwise, a complex and expensive reactor and turbo that can work at very high temperature are needed. In addition to tuning EGR fraction, a heat exchanger or multi-stage turbine can be used for lowering the temperature at turbine inlet.
As depicted in
Another method for lowering the turbine inlet exhaust temperature is using multi-stage turbines. As shown in
The exhaust air with lambda controlled at stoichiometric level flows into an oxidation catalyst, where HC and CO in the exhaust react with NOx and generate N2, CO2, and H2O. To remove PM in the exhaust air, referring to
Normally the soot filter 502 needs to be regenerated after a period of time. During regeneration, the exhaust lambda value at the inlet of the soot filter 502 cannot be controlled below 1.0, otherwise, soot in the filter is not able to be effectively removed, since oxygen in the exhaust is not enough for soot oxidation. A doser 501 can be used for further controlling lambda during filter regeneration, in which the fueling injected from the doser 501 reacts with the oxygen left in the regeneration in the front area of the catalyst 503 for lowering lambda to stoichiometric level.
Through turbines, heat energy is recovered into mechanical energy or electric energy. When the energy recovery efficiency is ηr, we can define the fuel penalty rp as the ratio of the net fuel loss in lambda control and the overall fueling, i.e.:
where mfuel
The equation (5) shows that the fuel penalty actually is determined by the engine out exhaust lambda value and the difference between the energy recovery efficiency and the engine efficiency. As an example, if λ1=1.4, then to have a fuel penalty of 5%, which is normally the value of an RPF system, assuming engine energy efficiency is 40%, the required energy recovery efficiency will be only 22.5%. If a turbine system has an energy recovery efficiency higher than 40%, there will be no fuel penalty.
In another embodiment of the present patent, referring to
The structure of an embodiment of the oxygen sorption device 602 is depicted in
A variety of materials can be used for absorbing and/or adsorbing oxygen. Among them, perovskite-related oxides has a good oxygen sorption capacity at temperature range of 200° C. to 400° C., and can be regenerated at temperature at 600° C. [Kusaba, H., Sakai, G., Shimanoe, K., Miura, N., Yamazoe, N., Solid State Ionics, 152-153 (2002)689-694]. Extra energy is needed in regenerating the oxygen absorption material and in rotating the device. This part of energy contributes to the overall fuel penalty for exhaust aftertreatment.
In addition to the rotating device, a valve-controlled system can also be used for removing oxygen in exhaust air. In such a system, as depicted in
For better removing NOx, referring to
One skilled in the art will appreciate that the present invention can be practiced by other than the preferred embodiments which are presented in this description for purposes of illustration and not of limitation, and the present invention is limited only by the claims that follow. It is noted that equivalents for the particular embodiments discussed in this description may practice the invention as well.
Number | Date | Country | |
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60922152 | Apr 2007 | US |