Patent Application
20170211587
This application claims priority to Great Britain Patent Application No. GB1601214.8, filed Jan. 21, 2016, which is incorporated herein by reference in its entirety.
The present disclosure generally pertains to turbomachinery and more particularly to a compressor housing configuration.
Compressors are used in wide variety of applications. For example, internal combustion engines may be provided with a forced air system such as a turbocharger to increase an engine efficiency and power by forcing extra air into the combustion chambers of the cylinders. The turbocharger includes a compressor rotationally coupled to a turbine.
Compressor operations at low mass flow rates are limited in pressure ratio by the surge limit, namely a threshold above which severe fluid dynamic instabilities may occur. Moreover, compressor operations close to surge may be associated with a noise which is known in the art as “whoosh” noise.
There is a need in art to enlarge the operative portion of the compressor map to achieve significant improvements on the compressor surge margin towards smaller flow rates. There is also a need in the art to reduce compressor noise, achieving significant dampening around a frequency range commonly used and improving customer satisfaction.
An embodiment of the present disclosure provides a compressor housing including a compressor inlet duct and an inlet for a compressor wheel. The compressor inlet duct has a longitudinal axis and connects an air intake duct with the compressor wheel inlet. The compressor housing includes at least one appendix positioned between an upstream portion of the compressor inlet duct and the compressor wheel inlet. The appendix includes a pipe closed at a distal end thereof with respect to the longitudinal axis of the compressor inlet duct. An advantage of this embodiment is that the introduction of an appendix including a closed pipe and integrated into the compressor housing at its inlet has proven to be effective in enlarging the operative portion of the compressor map by shifting the surge limit towards smaller mass flow rates. The fluid dynamic phenomenon induced by the proximal end of the closed pipe allows the achievement of higher pressure ratios at small mass flow rates. In automotive and heavy duty engines, this improvement is directly translated into higher low-end torque with no compromises in peak power performance. A further advantage is the achievement of significant noise dampening at different mass flow rates, especially in the frequency range related to the “whoosh” noise phenomenon that is particularly severe in automotive applications and is hereby reduced.
In another embodiment, the at least one appendix protrudes externally with respect to an external surface of the compressor housing inlet. An advantage of this embodiment is its effectiveness at any angular position along the surface of the compressor inlet duct, allowing a significant flexibility in packaging constrained applications.
In another embodiment, the at least one appendix has an axis that is inclined with respect to the longitudinal axis of the compressor inlet duct by an angle of inclination included between 10° and 90°. An advantage of this embodiment is that it allows to optimize the appendix inclination with respect to the longitudinal axis of the compressor inlet duct having regard to space constraints and performance.
In still another embodiment, the at least one appendix is inclined with respect to the external surface of the compressor housing by an angle of inclination included between 10° and 170°. The angle of inclination being included is defined between a plane tangent to the external surface of the compressor housing and passing through an intersection point between the axis of the at least one appendix and the external surface of the compressor housing, and a plane including the longitudinal axis of the compressor inlet appendix and perpendicular to a transversal section of the compressor inlet duct. An advantage of this embodiment is that it allows to optimize the appendix inclination with respect to the compressor housing having regard to space constraints and performance.
According to a further embodiment, a proximal part of the at least one appendix with respect to the longitudinal axis of the compressor inlet duct intersects the compressor inlet duct defining an upstream connection lip and a downstream connection lip.
According to still another embodiment, the minimum distance between the downstream connection lip of an internal surface of the compressor inlet duct and the compressor wheel inlet is between zero and three times the diameter of the compressor wheel at the compressor wheel inlet. An advantage of this embodiment is that it allows an optimal positioning of the appendix.
According to still another embodiment, the minimum distance between the upstream connection lip of an internal surface of the compressor inlet duct and the bottom wall of the at least one appendix is at least half of the diameter of the compressor wheel at the compressor wheel inlet. An advantage of this embodiment is that an optimal length of the appendix can be identified.
The present disclosure further includes a compressor assembly including a compressor housing and a compressor equipped with a compressor wheel fitted in a compressor wheel seat. The present disclosure further includes an automotive system equipped with a compressor assembly.
The present disclosure will hereinafter be described in conjunction with the following drawing figures, wherein like numerals denote like elements.
The following detailed description is merely exemplary in nature and is not intended to limit the invention or the application and uses of the invention. Furthermore, there is no intention to be bound by any theory presented in the preceding background of the invention or the following detailed description.
The various embodiments of the present disclosure are applicable to compressors in general. Some embodiments of the present disclosure will be now described with reference to an automotive system 100, however other compressor applications may be equipped with the compressor assembly according to the various embodiments of the present disclosure.
Some embodiments may include an automotive system 100, as shown in
A fuel and air mixture (not shown) is disposed in the combustion chamber 150 and ignited, resulting in hot expanding exhaust gasses causing reciprocal movement of the piston 140. The fuel is provided by at least one fuel injector 160 and the air through at least one intake port 210. The fuel is provided at high pressure to the fuel injector 160 from a fuel rail 170 in fluid communication with a high-pressure fuel pump 180 that increases the pressure of the fuel received from a fuel source 190. Each of the cylinders 125 has at least two valves 215, actuated by a camshaft 135 rotating in time with the crankshaft 145. The valves 215 selectively allow air into the combustion chamber 150 from the port 210 and alternately allow exhaust gases to exit through a port 220. In some examples, a cam phaser 155 may selectively vary the timing between the camshaft 135 and the crankshaft 145.
The air may be distributed to the air intake port(s) 210 through an intake manifold 200. An air intake duct 205 may provide air from the ambient environment to the intake manifold 200. In other embodiments, a throttle body 330 may be provided to regulate the flow of air into the manifold 200. In still other embodiments, a forced air system such as a turbocharger 230, having a compressor 240 rotationally coupled to a turbine 250, may be provided. Rotation of the compressor 240 increases the pressure and temperature of the air in the duct 205 and manifold 200. A charge air cooler 260 disposed in the duct 205 may reduce the temperature of the air. The turbine 250 rotates by receiving exhaust gases from an exhaust manifold 225 that directs exhaust gases from the exhaust ports 220 and through a series of vanes prior to expansion through the turbine 250. The exhaust gases exit the turbine 250 and are directed into an exhaust system 270. This example shows a variable geometry turbine (VGT) with a VGT actuator 290 arranged to move a rack of vanes 295 in different positions, namely from a fully closed position to a fully open position, to alter the flow of the exhaust gases through the turbine 250. In other embodiments, the turbocharger 230 may be fixed geometry and/or include a waste gate.
The exhaust gases of the engine are directed into an exhaust system 270. The exhaust system 270 may include an exhaust pipe 275 having one or more exhaust aftertreatment devices 280. The aftertreatment devices may be any device configured to change the composition of the exhaust gases. Some examples of aftertreatment devices 280 include, but are not limited to, catalytic converters (two and three way), oxidation catalysts, lean NOx traps, hydrocarbon adsorbers, selective catalytic reduction (SCR) systems, and particulate filters.
Other embodiments may include an exhaust gas recirculation (EGR) system 300 coupled between the exhaust manifold 225 and the intake manifold 200. The EGR system 300 may include an EGR cooler 310 to reduce the temperature of the exhaust gases in the EGR system 300. An EGR valve 320 regulates a flow of exhaust gases in the EGR system 300.
While the first EGR conduit defines a short route for the exhaust gas recirculation, in accordance with the present disclosure, a second EGR conduit 600 which fluidly connects the exhaust line downstream of the aftertreatment systems to the intake duct upstream the intake manifold and is connected therein by the interposition of a three-way valve 500, may be provided. The second EGR conduit 600 defines a long route which includes also a relevant portion of the exhaust line and a relevant portion of the intake duct.
The automotive system 100 may further include an electronic control unit (ECU) 450 in communication with one or more sensors and/or devices associated with the ICE 110 and with a memory system and an interface bus. The ECU 450 may receive input signals from various sensors configured to generate the signals in proportion to various physical parameters associated with the ICE 110. The sensors include, but are not limited to, a mass airflow and temperature sensor 340, a manifold pressure and temperature sensor 350, a combustion pressure sensor that may be integral within glow plugs 360, coolant and oil temperature and level sensors 380, a fuel rail pressure sensor 400, a cam position sensor 410, a crank position sensor 420, exhaust pressure and temperature sensors 430, an EGR temperature sensor 440, and an accelerator pedal 447 position sensor 445. Furthermore, the ECU 450 may generate output signals to various control devices that are arranged to control the operation of the ICE 110, including, but not limited to, the fuel injectors 160, the throttle body 330, the EGR Valve 320, a Variable Geometry Turbine (VGT) actuator 290, and the cam phaser 155. Note, dashed lines are used to indicate communication between the ECU 450 and the various sensors and devices, but some are omitted for clarity.
Depending on the configuration of the automotive system 100, in the air intake duct 205 either fresh air or a gas mixture of fresh air and recirculated exhaust gas can be present. Rotation of the compressor 240 increases the pressure and temperature of the gas coming from the air intake duct 205. The gas exiting from the compressor assembly 570 is directed through the air intake duct 205 towards the engine block 120.
In the compressor assembly 570, the compressor 240 is connected to a compressor housing 500. The compressor housing 500 is provided with a compressor inlet duct 535 and an inlet 550 for a compressor wheel 520. The compressor inlet duct 535 has a longitudinal axis A-A (
The appendix 510 has an axis A′-A′ that is inclined with respect to the longitudinal axis A-A of the compressor inlet duct 535 by an angle of inclination α included between 10° and 90°. A preferred option for angle α is 45°.
The minimum distance b between a downstream connection lip 585 of an internal surface 565 of the compressor inlet duct 535 and the compressor wheel inlet 550 is included between 0 and three times the diameter Φ of the compressor wheel 520 at the compressor wheel inlet 550. A preferred option for the distance b is 0.5 Φ.
The minimum distance c between an upstream connection lip 575 of an internal surface 565 of the compressor inlet duct 535 and the bottom wall 560 of the appendix 510 is at least half of the diameter Φ of the compressor wheel 520 at the compressor wheel inlet 550. A preferred option for the above detailed minimum distance c is from 1 Φ to 3 Φ.
In other words, the appendix 510 is inclined with respect to the external surface 555 of the compressor housing 535 by an angle of inclination γ included between 10° and 170°, the angle of inclination γ being included between a plane tangent to the external surface 555 of the compressor housing 535 and passing through an intersection point P between the axis A′-A′ of the at least one appendix 510 and the external surface 555 of the compressor housing 535, and a plane perpendicular to a transversal section of the compressor inlet duct 535 including the axis A′-A′ of the appendix 510.
The position of the appendix 510 with respect to the compressor inlet duct 535 can be further defined by the angle β represented in
The appendix 510 described above and represented in
While at least one exemplary embodiment has been presented in the foregoing detailed description, it should be appreciated that a vast number of variations exist. It should also be appreciated that the exemplary embodiment or exemplary embodiments are only examples, and are not intended to limit the scope, applicability, or configuration of the invention in any way. Rather, the foregoing detailed description will provide those skilled in the art with a convenient road map for implementing an exemplary embodiment, it being understood that various changes may be made in the function and arrangement of elements described in an exemplary embodiment without departing from the scope of the invention as set forth in the appended claims and their legal equivalents.
| Number | Date | Country | Kind |
|---|---|---|---|
| 1601214.8 | Jan 2016 | GB | national |
