The subject matter disclosed herein generally relates to exhaust gas recirculation systems, and more specifically to exhaust gas recirculation systems configured to control vapor content of exhaust gas used in EGR systems and to remove condensates, vapors, gases, ash, and particulates.
Internal combustion engines combust fuel with an oxidizer in a combustion chamber. The expanding gas produced by combustion applies direct force to pistons, turbine blades, or nozzles, transforming chemical energy into useful mechanical energy. Internal combustion engines are often required to meet strict standards for emissions including emissions of nitrogen oxides (NOx), hydrocarbon (HC), formaldehyde (HCHO), carbon monoxide (CO), ammonia (NH3), particulates and other emissions.
NOx emissions may be reduced by using exhaust gas recirculation (“EGR”) to dilute the charge air and depress the maximum temperature reached during combustion. Typically the exhaust is cooled to avoid increased intake temperatures that may adversely affect engine operation. In some cases, engine coolant is used as a low temperature fluid to cool exhaust gas temperatures in EGR systems.
A problem that arises with the cooling of exhaust gas used in EGR systems is the precipitation of water droplets out of the EGR exhaust gas during the cooling. The water droplets may contribute to bore washing of oil from the engine cylinder bore, thereby reducing lubrication. Water droplets may also have an adverse impact on turbocharger compressor blades. The water also promotes corrosion in the EGR system and the engine intake system. Another problem is the lack of control over the percentage of water vapor in the exhaust gas can make it difficult to control the amount of diluent required to operate consistently in the combustion window between misfire and knock. Still another problem is that ash and particulates present in the EGR exhaust gas may contribute to wear in the engine.
In accordance with one exemplary non-limiting embodiment, the invention relates to a system for recirculating exhaust gas including a cooling subsystem configured to cool the exhaust gas; a condensation removal subsystem; and a temperature adjustment subsystem. In some embodiments the cooling subsystem is configured to cool the exhaust gas to below a saturation temperature. In some embodiments the condensation removal subsystem is configured to remove condensed water droplets from the exhaust and absorb and scrub other exhaust constituents.
In another embodiment, an engine includes a combustion chamber wherein fuel is combusted producing an exhaust gas at a first temperature; an exhaust system coupled with the combustion chamber that collects the exhaust gas. An exhaust gas cooling system may be configured to reduce exhaust gas temperature to below the saturation temperature. A condensate removal system may be coupled with the exhaust gas cooling system configured to precipitate a condensate from the exhaust gas. An intake system may be coupled with the condensate removal system and the combustion chamber.
In another embodiment, a method of recirculating exhaust gas may include cooling the exhaust gas to a temperature below a saturation temperature; removing condensate from the exhaust gas; and heating the exhaust gas to a temperature above the saturation temperature.
Other features and advantages of the present invention will be apparent from the following more detailed description of the preferred embodiment, taken in conjunction with the accompanying drawings which illustrate, by way of example, the principles of certain aspects of the invention.
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Associated with the first stage cooler 27 are a first coolant inflow port 31 and a first coolant outflow port 33. In one embodiment the coolant flowing into the first coolant inflow port 31 may be jacket coolant from the engine 11. Associated with the second stage cooler 29 are a second coolant inflow port 35 and a second coolant outflow port 37. In one embodiment, the coolant flowing into the second coolant inflow port 35 may be coolant from an auxiliary coolant tank (not shown) which may be maintained at a temperature in the range of 40° C. to 75° C. or other appropriate temperature. The second stage cooler 29 reduces the temperature of the exhaust gas so that at least a portion of the exhaust gas temperature is reduced to a temperature below the saturation temperature or dew point thereby causing at least a portion of the water in the exhaust to condense into liquid. The temperature of the exhaust gas in the second stage cooler 29 may be used to vary the percentage water that condenses compared to water that remains as vapor. Additionally a valve in the one or more heat exchangers can vary the amount of cooling air or liquid flow rate into the heat exchanger to adjust the temperature of the exhaust gas. The condensate droplets may precipitate and be entrained in the exhaust gas. The cooling medium flow rate, cooling medium temperature and heat exchanger design may be chosen to obtain a preferred water condensation efficiency from the exhaust gas.
The exhaust gas flowing through the second stage cooler 29 may then be passed through a mist eliminator 39 where condensate droplets entrained in the exhaust gas may be precipitated and removed through condensate output port 40. The mist eliminator 39 is a device with a large surface area and small volume to collect liquid without substantially impeding the exhaust gas flow. Alternately, a centrifugal mist eliminator may be used. The mist eliminator 39 collects the fine droplets and allows the collected liquid to drain away through condensate output port 40. The mist eliminator may have multiple stages.
Condensate droplets that remain temporarily attached to the surface of the mist eliminator may improve the efficiency of the mist eliminator 39, and may add functionality to the mist eliminator 39. The temporarily attached droplets may allow the mist eliminator 39 to capture fine condensed droplets from the exhaust gas that would otherwise slip through the mist eliminator 39. The temporarily attached droplets may also cause the mist eliminator 39 to act as a scrubber or an absorber. Solids and liquids that are commonly present in the exhaust gas, such as ash, phosphorus, sulfur, calcium, particulates, carbon, and compounds including such constituents in addition to metals present in the engine that may be in the exhaust due to engine wear may be captured or scrubbed from the exhaust gas by the temporarily attached droplets. Particulates are typically carbonaceous solids that result from the combustion process, that may themselves include dissolved liquids such as oil or volatile organic compounds. In addition, non-condensed water vapor may condense or be absorbed into the temporarily attached droplets. Soluble and non-soluble liquids present in the exhaust gas may also be absorbed or scrubbed from the exhaust gas including ammonia, formaldehyde, benzene, engine oil, and others. Some gaseous components of the exhaust may also be absorbed into the temporarily attached droplets, especially nitrogen oxides, sulfur oxides, and hydrocarbon gases. The mist eliminator 39 may be sized and configured to intentionally maintain temporarily attached droplets on the mist eliminator 39 to optimize scrubbing or absorbing. In particular, the mist eliminator 39 may be configured to optimize removal of ash and particulate compounds in order to prevent such compounds from entering and damaging the cylinders 13. Various mist eliminators operate with different technologies such as using high surface area mesh, alternating vanes, wavy plates, centrifugal forces, sonic energy, electromagnetic energy, or electrostatic forces. Any device or process that removes condensate from the exhaust gas flow may be used.
The exhaust gas flowing through the mist eliminator 39 may then be passed through a reheater 41 where it is reheated to above the saturation temperature. The reheater 41 may be a heat exchanger that includes a reheater fluid inflow port 43 and a reheater fluid outflow port 45. The reheater may alternatively be any device or process that imparts energy to the exhaust gas sufficient to raise the temperature of the exhaust gas, including a heat exchanger that receives its heating energy from engine exhaust, an electric heating element or a microwave generator. The exhaust gas passing through the reheater is then recirculated back into the intake manifold 15 of the engine 11.
EGR flow control valve 47 may be disposed on EGR conduit 21 after the reheater 41 to control the flow rate of the exhaust gas. Control of the EGR flow rate may be used to control the temperature or heat energy of the EGR, or to control the temperature of the combined fresh air and fuel and EGR intake charge after the EGR is introduced into the intake charge, or to control the temperature of the exhaust gas after the EGR is introduced and the charge is combusted, or to control the fraction of EGR that is recycled into the engine relative to the fresh air and fuel in the intake charge or to control the effectiveness of the EGR as an inert on the combustion process.
The EGR system 9 may be provided with one or more of EGR bypass instrumentation 49, stage 1 instrumentation 51, stage 2 instrumentation 53, mist eliminator instrumentation 55, and reheater instrumentation 57 (collectively “instrumentation”). Instrumentation may include temperature sensors, flow rate sensors and pressure sensors.
The EGR system 9 may be provided with a control system 59 that receives instrumentation inputs 61 and provides exhaust gas valve control output 63 and EGR flow control output 65. Additional instrumentation inputs 62 may also be provided from the intake manifold 16 or air intake 70 to the exhaust gas valve output 63 or EGR flow control output 65. Control system 59 may include at least one processor. The control system 59 may be configured to automatically or continuously monitor the operation of the EGR system 9. The control system 59 may function as a stand-alone system or may be integrated as a component of a larger system, such as an internal combustion engine control or a plant control system.
EGR system 9 may include an EGR mixer 67 having an air intake port 69 that combines air from air intake 69 port with exhaust gas. The mixture of exhaust gas and air may be conveyed to a turbocharger 71 having a turbine 73 driven by exhaust provided through exhaust gas input port 75. The turbocharger 71 is optional, and the system may operate using variable exhaust gas control valve 23 and EGR flow control valve 47 without a turbocharger 71. The turbine drives a compressor 77 that compresses the mixture of exhaust gas and air. A secondary mist eliminator 79 having a condensate output port 81 may optionally be provided in high pressure EGR applications.
In operation, the EGR system 9 provides control of the percentage of water vapor provided to the intake manifold 15 of the engine 11 and maintains a more consistent combustion window between misfire and knock. The removal of water droplets from the recirculated exhaust gas reduces or eliminates “bore washing” of oil from the bore by liquid water droplet formed downstream of the compressor or aftercooler. The removal of water droplets from the recirculated exhaust gas prevents droplets from passing into the compressor thereby avoiding damage to the compressor blades resulting from water droplets impinging on the high velocity compressor blades. The reheating of the exhaust gas after it passes through the mist eliminator 39 ensures that the turbocharger compressor blades are not damaged by liquid water droplet impingement. The EGR system 9 improves compressor durability when using low pressure EGR and enables the reliable operation of an EGR engine. Removal of water droplets from the EGR minimizes or eliminates intake system corrosion.
EGR system 9 may be implemented in a low pressure EGR system illustrated in
In alternate EGR systems, the passage for EGR is routed to flow EGR from a higher exhaust pressure location to a lower inlet pressure location.
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The invention disclosed may be used with various types of reciprocating engine such as compression ignition and spark ignition engines that combust hydrocarbon fuels such as diesel fuel, natural gas fuel, gasoline and the like. Additionally the EGR system may be used with a turbine or other types of combustion engines that may benefit from an EGR system.
The flowcharts and step diagrams in the Figures illustrate the architecture, functionality, and operation of possible implementations of systems, and methods, according to various embodiments of the present invention. It should also be noted that, in some alternative implementations, the functions noted in the step may occur out of the order noted in the Figures. For example, two steps shown in succession may, in fact, be executed substantially concurrently, or the steps may sometimes be executed in the reverse order, depending upon the functionality involved. It will also be noted that each step of the step diagrams and/or flowchart illustration, and combinations of steps in the step diagrams and/or flowchart illustration, can be implemented by special purpose hardware-based systems which perform the specified functions or acts, or combinations of special purpose hardware and computer instructions.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. Where the definition of terms departs from the commonly used meaning of the term, applicant intends to utilize the definitions provided below, unless specifically indicated. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/ or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/ or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/ or groups thereof. It will be understood that, although the terms first, second, etc. may be used herein to describe various elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another. For example, a first element could be termed a second element, and, similarly, a second element could be termed a first element, without departing from the scope of example embodiments. As used herein, the term “and/or” includes any, and all, combinations of one or more of the associated listed items. As used herein. the phrases “coupled to” and “coupled with” as used in the specification and the claims contemplates direct or indirect coupling.
This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims.
This invention was made with Government support under contract number DE-FC26-01CH11080 awarded by the Department Of Energy. The Government has certain rights in this invention.