Patent Application
20070283698
A more complete understanding of the various methods, systems and/or arrangements described herein, and equivalents thereof, may be had by reference to the following detailed description when taken in conjunction with the accompanying drawings wherein:
Turbochargers are frequently utilized to increase the output of an internal combustion engine. Referring to
The turbocharger 120 acts to extract energy from the exhaust and to provide energy to intake air, which may be combined with fuel to form combustion gas. As shown in
Referring to the turbine 126, such a turbine optionally includes a variable geometry unit 130 and a variable geometry controller 132. The variable geometry unit 130 and variable geometry controller 132 optionally include features such as those associated with commercially available variable geometry turbochargers (VGTs), such as, but not limited to, the GARRETT® VN™ and AVNT™ turbochargers, which use multiple adjustable vanes to control the flow of exhaust across a turbine.
Adjustable vanes positioned at an inlet to a turbine typically operate to control flow of exhaust to the turbine. For example, GARRETT® VNT™ turbochargers adjust the exhaust flow at the inlet of a turbine rotor in order to optimize turbine power with the required load.
A variety of control schemes exist for controlling geometry, for example, an actuator tied to compressor pressure may control geometry and/or an engine management system may control geometry using a vacuum actuator. Overall, a VGT may allow for boost pressure regulation which may effectively optimize power output, fuel efficiency, emissions, response, wear, etc. Of course, an exemplary turbocharger may employ wastegate technology as an alternative or in addition to aforementioned variable geometry technologies.
The turbocharger 120 optionally includes an electric motor 150 to drive the shaft 122 and thereby rotate a compressor wheel of the compressor unit 124. Technology described herein (e.g., an exemplary mixer) may be used in coordination with an electric motor to control inlet air characteristic to the engine 110 (e.g., temperature, pressure, etc.).
The system 100 also includes a flow path or conduit 140 between the compressor air inlet 134 and the exhaust port 116. Flow in the path 140 is controlled by a valve 142, for example, to allow for exhaust gas recirculation (EGR). This arrangement for EGR is sometime referred to as “long route” EGR; compared to shorter routes that may introduce exhaust into the inlet stream downstream from the compressor 124. One or more additional components may provide for cooling of the exhaust (e.g., heat exchanger 144).
While EGR can be beneficial in reducing emission of certain chemical species, EGR typically shifts the engine running line (the lugline) on a compressor map to the left toward a more unstable operating region of the compressor map. The shift increases with increasing amount of recirculation gas.
The exhaust turbine unit 260 includes a turbine housing 262 having an exhaust outlet portion 264 and a flange 266 associated with an exhaust inlet portion 267. The turbine housing inlet flange 266 often acts as the reference point for fixing turbocharger position relative to its installation and acts as the main load bearing interface for the turbocharger 220. The turbine housing 262 houses a turbine wheel 268 and defines one or more volutes that act to direct exhaust gas from the exhaust inlet to the wheel 268.
A shaft 222, which may be a multi-component shaft, operably connects the turbine wheel 268 and the compressor wheel 248. A center housing 225 houses at least a portion of the shaft 222 and connects the compressor housing 240 and the turbine housing 260. As described herein, a housing (e.g., compressor, turbine, center, etc.) may be a multi-component housing.
Intended direction of rotation of the compressor wheel 248 and the turbine wheel 268 is indicated as the mixer 310 is configured with respect to this intended direction of rotation. In the example of
The mixer 310 includes an exhaust gas inlet mount 312 joined to a substantially tubular wall 314 that defines a volute. The tubular wall 314 joins a substantially cylindrical upstream wall 316 and a substantially cylindrical downstream wall 318 that define an opening or slot that allows gas to exit the volute. The terms upstream and downstream refer to upstream the opening and downstream the opening. Gas exiting the opening enters the compressor unit 240 via the air inlet portion 244 of the compressor housing 242. In this example, the downstream wall 318 attaches to the air inlet portion 244 of the compressor housing 242 via an attachment mechanism (e.g., threaded, flanged, etc.).
While the opening may be less than 360° (e.g., along the entire inner circumference of the mixer 310), a circumferential opening of about 360° can help to deliver gas more evenly to the compressor unit 240. A circumferential opening can provide for good mixing ability and can deliver tangentially uniform flow to the compressor.
In an alternative arrangement, a compressor housing may include a mixer. For example, the inlet portion 244 of the housing 242 may include an upstream wall and a downstream wall that define one or more openings for exhaust gas provided by a volute. A tubular wall defining the volute may be integral with the inlet portion 244 or may be attachable to the inlet portion 244 for delivery of gas via the opening or openings.
As already mentioned, the mixer 310 is configured with reference to the intended direction of rotation of the compressor wheel. In operation, the mixer 310 generates a positive swirl as exhaust gas exits the volute where the positive swirl is in the same direction as the intended compressor wheel rotation. The positive swirl, as imparted to the mixture of the air and the gas, modifies angle of incidence at inducer portion of the compressor wheel, enabling the compressor to operate more stably.
An exemplary mixer can use a scroll or volute similar to that of a turbine housing to create the swirl and, for example, to circumferentially distribute the gas uniformly. As already mentioned, a mixer may be used in conjunction with an electric motor to regulate inlet air to an internal combustion engine. For example, an EGR mixer and an electric motor may be used to ensure stable flow at the inducer portion of a compressor wheel. An electric motor may be used to accelerate or decelerate rotational speed of a compressor wheel. A controller may provide for coordinated control of EGR and an electric motor to maintain flow stability at a compressor wheel.
An exemplary mixer includes a cylindrical wall having a center axis, a substantially tubular wall defining a volute or scroll oriented about the center axis, an inlet to the volute or scroll, an exit to the volute or scroll provided by one or more openings in the cylindrical wall where the volute or scroll imparts a tangential velocity component to gas exiting the volute or scroll and a mount or attachment mechanism to mount or to attach the mixer to an inlet to a compressor where the tangential velocity component imparted by the orientation of the volute is in the intended direction of rotation of a compressor wheel of the compressor.
A volute or scroll may be oriented about a center axis in a clockwise or counter-clockwise direction (e.g., clockwise spiral or counter-clockwise spiral). Thus, where the intended direction of rotation of a compressor wheel is clockwise, then the volute or scroll of the mixer will impart a tangential velocity component or positive swirl in a clockwise direction.
The plots 350, 360 show velocity triangles without (350) and with (360) positive swirl at the inducer portion of a compressor wheel blade. As indicated, the positive swirl reduces the incidence angle, which acts to stabilize flow at the inducer portion of the blade. Without the positive swirl (plot 350), when a compressor is operated at low mass flow rate region, the reduction of inlet absolute velocity results in a positive incidence angle at the inlet (I>0), this eventually leads to flow separation from the inducer suction surface and flow instability. With positive swirl (plot 360), the positive incidence angle is reduced and compressor remains stable. The exemplary mixer 310 can also self regulate; when the amount of EGR increases, positive swirl increases.
The system 500 includes an exemplary mixer 530 for introducing exhaust gas to the inlet 534 of the compressor assembly 540. The exhaust entering the mixer 530 has a temperature T4′, which may be approximately the same as T4. An optional heat exchanger 544 may be used to alter T4′, for example, to cool the exhaust to a temperature less than T4. Where the exhaust is to be cooled, parameters defining the mixer 530 may account for cooling and the increased density of the exhaust. Where the mixer 530 has one or more adjustable components, adjustment of such component(s) may be achieved by an actuator or controller 535 that optionally receives one or more signals from an engine control unit (ECU) or other controller, sensor or actuator. A mixer with an adjustable component is described with respect to
The system 500 includes a valve 573 that can adjust air flow to the exhaust stream or, more commonly, flow from the exhaust stream to the inlet stream (e.g., exhaust gas recirculation or “EGR”). Another valve 574 may be a wastegate valve or an EGR valve that allows at least some exhaust to bypass the turbine assembly 560 for purposes of reducing exhaust flow to the turbine assembly 560 or for purposes of EGR. As explained with respect to
The turbine assembly 560 receives at least some exhaust from the engine, which, again, is at temperature T5. In general, T5 is the highest temperature in the system 500. The temperature of the turbine assembly 560, T6, is generally less than that of the exhaust (i.e., T6<T5) because the turbine assembly 560 extracts energy from the exhaust and also because some lubricant cooling may be provided as well. Hence, where the wastegate valve 573 is closed (i.e., no bypass flow), the temperature T8 of exhaust exiting the turbine 560 via the conduit 536 is less than T5 as well.
The system 500 illustrates various mechanisms for use in temperature control of an exhaust turbine assembly 560 and for EGR of an internal combustion engine (e.g., the engine 110 of
The system 500 optionally includes one or more temperature sensors. For example, measurement of temperatures T0, T5 and T8 can provide information as to turbocharger efficiency and performance. As discussed herein, temperature measurements may be used to control EGR (e.g., amount, cooling of exhaust, etc.).
The system 500 optionally includes an electric motor and/or generator controlled by a controller 550. As already mentioned, such a unit may be used in conjunction with other features (e.g., the mixer, EGR valves, ECU, etc.) to control performance of the turbocharger for an internal combustion engine.
While various examples pertain to use of exhaust gas to impart positive swirl (or tangential momentum) to an inlet stream to a compressor, an exemplary mixer may be optionally operated using other gas or air. For example, if the inlet 312 of the mixer 310 was open to the atmosphere, air would be drawn into the volute by the compressor. As the air exits the volute, a positive swirl (or tangential momentum) will be imparted to the inlet stream to the compressor, which can improve compressor stability.
An exemplary method includes drawing gas through a volute to generate a tangential velocity component (tangent to a center axis of the volute), mixing the gas with inlet air to a compressor to thereby stabilize flow at an inducer portion of a compressor wheel of the compressor where the tangential velocity component and the intended direction of rotation of the compressor wheel are in the same direction about the center axis, compressing the gas and inlet air mixture and providing the gas and inlet air mixture to an internal combustion engine. Such a method may use exhaust gas for exhaust gas recirculation of an internal combustion engine.
Although some exemplary methods, devices, systems, etc., have been illustrated in the accompanying Drawings and described in the foregoing Detailed Description, it will be understood that the methods and systems are not limited to the exemplary embodiments disclosed, but are capable of numerous rearrangements, modifications and substitutions without departing from the spirit set forth and defined by the following claims.
