Patent Application
20240344524
The present disclosure relates to secondary air pumps for use in vehicle internal combustion engine systems.
Internal combustion engine systems are increasingly being held to stricter and stricture regulations on emissions from the system. Various strategies, generally employing one or more catalytic devices for treating exhaust gases, are in common use for reducing the levels of undesirable emissions. The use of secondary air injection (SAI) using a secondary air pump (SAP) is a known technique for assisting in the reduction of engine emissions. The SAP is employed for injecting fresh air into the exhaust stream from the engine during certain operating conditions to assist in burning or oxidation of pollutants (for example, unburned hydrocarbons) in the exhaust gases.
After a cold start of the engine, the amount of unburned hydrocarbons in the exhaust gases tends to be increased, and levels of undesirable emissions out the tailpipe are relatively high until the catalytic treatment device reaches its light-off temperature. By injecting fresh air into the exhaust gases ahead of the catalytic treatment device, pollutants such as unburned hydrocarbons can be oxidized through an exothermic chemical reaction that helps heat up the catalyst more quickly. Indeed, in some cases, fuel can be intentionally injected into the exhaust gas stream ahead of the catalyst, together with secondary air injection, to induce this exothermic reaction to more-quickly heat up the catalyst.
Secondary air pumps typically comprise centrifugal compressors. A challenge for secondary air pumps is that engine system designers are increasingly demanding higher pressures from them, but at very low flow rates. This is an operating regime that places the compressor near its surge line, and flow instabilities can occur. While techniques for delaying surge to lower flow rates are generally known for centrifugal compressors, these techniques tend to be ineffective at the very low flow rates that a SAP must operate at.
The present disclosure is directed to a secondary air pump for use in internal combustion engine systems, comprising:
In one embodiment, a radial gap extends between a radially outer periphery of the compressor wheel and leading edges of the vanes, and said radial gap is axially bounded between said first wall of the housing assembly and an opposite second wall of the housing assembly. The leading edges of the vanes extend radially inwardly of a radially inner periphery of the vane plate in one embodiment.
Optionally, the vaned diffuser ring can be press-fit to secure it within the housing assembly. In this case, the housing assembly defines a cylindrical surface and there is an interference fit between the radially inner periphery of the vane plate and said cylindrical surface to secure the vaned diffuser ring in place.
The volute can follow the vaned diffuser ring with respect to said axial direction along which the air flow enters the compressor wheel. Alternatively, the volute can precede the vaned diffuser ring with respect to said axial direction.
In come cases, the inclusion of the vaned diffuser ring can negatively affect flow stability. Therefore, in some embodiments, the pump can further comprise a recirculation channel defined in the housing assembly, the recirculation channel having one end connected downstream of an inducer portion of the compressor wheel and an opposite end connected to the air inlet to allow a fraction of the compressed air to be bled off and recirculated back to the air inlet as a surge suppression technique.
Having thus described the invention in general terms, reference will now be made to the accompanying drawings, which are not necessarily drawn to scale, and wherein:
The present inventions now will be described more fully hereinafter with reference to the accompanying drawings, in which some but not all embodiments of the inventions are shown. Indeed, these inventions may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will satisfy applicable legal requirements. Like numbers refer to like elements throughout.
A secondary air pump (SAP) 10 in accordance with one embodiment of the invention is illustrated in
The motor housing 40 contains a motor stator 42 and a motor rotor 44. The motor rotor is affixed to the shaft 18 for rotation therewith, and the motor stator surrounds the motor rotor. The shaft 18 is rotationally supported in bearings 19 contained within the motor housing. The motor housing also defines a volute 28 that receives and collects the air compressed by the compressor wheel, for onward delivery to a component of an internal combustion engine system (not shown). In alternative embodiments such as that of
Secondary air pumps must be able to operate at very low flow rates. At such flow rates, techniques that are typically employed with centrifugal compressors to shift the surge line of the compressor to lower flow rates (e.g., inlet adjustment mechanisms, A/R, inlet and outlet blade angles, etc.) no longer work effectively. In accordance with the present invention, stable pump operation is attainable at very low flow rates by virtue of the provision of a vaned diffuser ring 50 that is embedded within the volute 28.
With reference to
In conventional centrifugal compressors having diffuser vanes, the vanes and the volute are serially arranged with respect to the radial direction, such that the air first passes through the vanes and then exits from the vanes and enters the volute. In contrast, in accordance with the invention, the vaned diffuser ring 50 is embedded within the volute 28 and hence the air passing through the vanes has already entered the volute prior to exiting from the vane array.
The vaned diffuser ring 50 can be secured within the housing assembly in any suitable manner. In one embodiment, with reference to
The presence of the vanes in the diffuser significantly alters the aerodynamics of the air flow through the compressor wheel. The compressor wheel used in a secondary air pump is quite small, and the height of the compressor blades at the exduder of the wheel can be approximately 1 millimeter (a significant portion of which is occupied by the necessary blade fillets). The required clearance between the blade tips and the housing shroud surface can be 30 to 50 percent of the exducer blade height, which leads to significant aerodynamic losses. When the vanes are inserted into the diffuser, the air flow inside the wheel is changed so that the effect of flow through the clearance is reduced. Accordingly, the peak efficiency line on the compressor map is shifted to lower flow rates, and a slight increase in pressure ratio can be achieved in the region between the peak-efficiency line and the surge line.
The embodiment of
In some cases, there may be a desire to enhance flow stability through the compressor wheel, given that the pump operation typically will be at very low flow rates and relatively high pressure ratio, and hence in a region of the compressor map where the flow can potentially become unstable. In such cases, flow recirculation can be employed to enhance stability. As an example,
A vaned diffuser in accordance with the invention can shift the peak efficiency line of the compressor to lower flow rates without significant loss in the compressor wheel. This leads to more optimal aerodynamic parameters, which will slightly increase pressure ratio in the area from the surge-line to the peak efficiency line. On the other hand, the compressor capacity and the aerodynamic parameter will be significantly reduced from the peak efficiency line to the choke line. However, this may not matter for certain SAP applications such as those without a boost function. The surge line can also be negatively affected with respect to flow stability. However, in synergy with the recirculation channel, its constant position can be assumed relative to a vaneless diffuser compressor with low trim (smaller than T16) compressor wheel.
Many modifications and other embodiments of the inventions set forth herein will come to mind to one skilled in the art to which these inventions pertain having the benefit of the teachings presented in the foregoing descriptions and the associated drawings. Therefore, it is to be understood that the inventions are not to be limited to the specific embodiments disclosed and that modifications and other embodiments are intended to be included within the scope of the appended claims. Although specific terms are employed herein, they are used in a generic and descriptive sense only and not for purposes of limitation.
