The present invention relates to an exhaust system for a motorcycle engine. More particularly, the invention relates to a muffler assembly having a particular arrangement of parts and overall shape.
In one embodiment, the invention provides a muffler assembly for a motorcycle engine. The muffler assembly includes a downstream attenuation portion adapted to be positioned substantially rearward of the motorcycle engine and having a first height, an upstream portion adapted to be positioned substantially forward of the motorcycle engine and having a second height, and an intermediate attenuation portion between the upstream portion and the downstream attenuation portion. The intermediate attenuation portion is adapted to be positioned substantially below the motorcycle engine and has a third height less than half the first height.
In another embodiment, the invention provides a motorcycle including an engine, a transmission coupled to the engine and configured to receive power from the engine, a rear wheel coupled to the transmission and configured to receive engine power through the transmission, and a muffler assembly coupled to the engine and in communication therewith to receive exhaust gases from the engine. The muffler assembly includes a downstream attenuation portion positioned between the transmission and the rear wheel and an intermediate attenuation portion positioned forwardly of the downstream attenuation portion. The intermediate attenuation portion extends along an underside of the engine.
In yet another embodiment, the invention provides a motorcycle including an engine, two wheels defining a central axis of the motorcycle, and a muffler assembly in communication with the engine to receive exhaust gases from the engine, the muffler assembly being positioned substantially along the central axis. The muffler assembly includes a downstream attenuation portion, an upstream portion, an intermediate attenuation portion positioned substantially under the engine, and a recess at least partially defined by the downstream attenuation portion and the intermediate attenuation portion. The recess has a depth greater than a height of the intermediate attenuation portion, and the engine is positioned substantially within the recess.
Other aspects of the invention will become apparent by consideration of the detailed description and accompanying drawings.
Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the following drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. The use of “including,” “comprising,” or “having” and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. Unless specified or limited otherwise, the terms “mounted,” “connected,” “supported,” and “coupled” and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, “connected” and “coupled” are not restricted to physical or mechanical connections or couplings.
The exhaust system 18, as shown in
An upstream end 36A of each header 22 is coupled to the engine 14 to receive exhaust gases from a respective exhaust port of the engine 14. The headers 22 define exhaust flow passages that are separate from one another, each header 22 routing exhaust gases directly from an exhaust port of the engine 14 to a downstream exhaust component. A downstream end 36B of each of the headers 22 leads into an upstream end 35A of the muffler assembly 35, specifically, the collector section 26. The upstream end 35A of the muffler assembly 35 is positioned generally forward of the engine 14. The illustrated collector section 26 is an exhaust conduit defining a 2-into-1 exhaust flow passage joining the two separate exhaust flow passages of the headers 22 into a single, larger exhaust flow passage adjacent the catalytic converter 30. Therefore, exhaust gases from both combustion chambers are treated by the catalytic converter 30.
The second attenuation portion 34B defines an intermediate portion 35C of the muffler assembly 35 between the upstream end 35A and a downstream end 35B of the muffler assembly 35, along the underside of the engine 14. The first attenuation portion 34A, positioned generally at the downstream end 35B, is positioned generally rearward of the engine 14. A muffler shell or casing 35D (made up of one or more pieces) extends from the upstream end 35A to the downstream end 35B, defining an outer surface of the muffler assembly 35. Although, the casing 35D can be assembled from multiple pieces in some embodiments, it defines a generally continuous outer surface without abrupt transitions from one portion of the muffler assembly 35 to the next.
Downstream of the catalytic converter 30, exhaust gases flow through the intermediate portion 35C to the first attenuation portion 34A at the downstream end 35B. As described above, the intermediate portion 35C extends longitudinally underneath the engine 14, but alternate shaping and positioning of the exhaust components on the motorcycle 10 are optional. As described in further detail below, exhaust gases from the catalytic converter 30 are directed substantially straight through the intermediate portion 35C to the first attenuation portion 34A, and at least a portion of the exhaust gases flow back from the first attenuation portion 34A into the second attenuation portion 34B before exiting the muffler assembly 35 at a pair of outlets 35E.
Returning now to the treatment of the exhaust gases at the upstream end 35A, the catalytic converter 30 improves the emissions quality of the exhaust gases expelled from the engine 14 with the use of one or more known catalyst materials (referred to hereinafter simply as catalyst 38), which are contained within the catalytic converter 30. The catalyst 38 reacts with undesirable exhaust gas components to produce more desirable products before being exhausted to the atmosphere via outlets 35E. Specifically, nitrogen oxides (NOx) can be converted to nitrogen (N2) and oxygen (O2), while carbon monoxide (CO) can be converted to carbon dioxide (CO2).
The temperature of the catalyst 38 affects its performance. It is necessary to warm-up, or “light off”, the catalyst 38 above a minimum threshold temperature to obtain a desired level of performance from the catalytic converter 30 to effectively alter the undesirable exhaust gas components as described above. From a cold start of the engine 14, the catalyst 38 is generally below the minimum threshold temperature, and therefore it is desirable to heat up the catalyst as quickly as possible to obtain sufficient or optimal performance. One way to get quicker light off of the catalyst 38 is to place the catalytic converter 30 close to the engine 14, which is a source of heat via the hot exhaust gases flowing through the headers 22 to the catalytic converter 30.
However, placing the catalytic converter 30 at the downstream ends 36 of the headers 22 can have an undesirable effect on the exhaust gas pressure dynamics as compared to a placement further downstream. This undesirable effect can be somewhat reduced by using multiple catalytic converters 30 in parallel. However, the use of multiple catalytic converters 30 causes an undesirable increase in catalyst light off time (in addition to increasing cost, size, and weight). Regardless of its position in the exhaust system 18, the catalyst 38 is a substantial obstruction in the flow passage and, therefore, causes a sudden increase in flow resistance at its upstream end. This causes a positive pressure exhaust wave or pulse to be reflected back towards the engine 14 through the headers 22. The dynamics of the exhaust gases coming from the engine 14 and the reflected waves moving towards the engine impacts the engine performance (i.e., horsepower and torque output).
Under certain operating conditions, a reflected exhaust pulse hinders the exhaust scavenging process as well as the ability for the cylinder to become charged with fresh intake air (which can also affect the input of fuel into the cylinder). If the exhaust wave that is reflected off the catalyst 38 arrives at either combustion chamber during valve overlap (the time that both the intake and exhaust valves are open), there is a significant performance loss due to decreased volumetric efficiency. With high exhaust gas pressure downstream of the combustion chamber, the net pressure differential that draws fresh air into the cylinder is reduced. Hence, less air and fuel fills the cylinder, and volumetric efficiency is spoiled, resulting in a “hole” in horsepower and torque output. The reduced output occurs over the range of engine speeds where the positive exhaust wave returns during valve overlap. Generally, a longer distance between the cylinders and the catalyst 38 results in power loss at lower engine speeds, and a shorter distance between the cylinders and the catalyst 38 results in power loss at higher engine speeds.
In the illustrated exhaust system 18, the catalytic converter 30 is positioned within the first half of the total exhaust gas flow length between the engine 14 and the outlets 35E. Furthermore, as shown in
The resonator chamber 42 serves as a “dead end” expansion volume in that the only passageways into and out of the resonator chamber 42 are the openings 46. Thus, all the exhaust gases that enter the resonator chamber 42 through the openings 46 eventually flow out of the resonator chamber 42 through the openings 46 and subsequently pass through the catalytic converter 30. On the other hand, the exhaust gases that do not enter the resonator chamber 42 can pass directly into and through the catalytic converter 30. Flow into the catalytic converter 30 is unobstructed in that there are no physical obstructions to prevent exhaust flow straight from the headers 22 and through the catalytic converter 30, only the flow-restrictive nature of the catalytic converter 30, itself.
In the illustrated embodiment, the collector section 26 does not form a substantial length of the exhaust system 18. This is in contrast to an exhaust system with a long collector section, which typically runs from the front or alongside the engine to a location rearward of the engine. Rather, the collector section 26 of the illustrated exhaust system 18 serves to consolidate the exhaust gas flow passages of the headers 22 over a short length such that the perforated section 50 and the catalytic converter 30 are positioned at or substantially adjacent the downstream ends 36 of each of the headers 22 and within about the first 40% of the total flow length between the engine exhaust ports and the outlets 35E. For example, the length from the rear cylinder exhaust port to the perforated section 50 is about 612 millimeters, and the length from the perforated section 50 to the outlets 35E is about 950 millimeters.
The above description highlights some of the difficulties with simply taking a catalytic converter from a downstream location and moving it to a far upstream location for quicker light off. The resonator chamber 42 and the perforated section 50 of the present invention enable both quick light off and satisfactory power output of the engine 14.
When the exhaust valve (not shown) of one cylinder opens, a high pressure wave propagates down the associated header pipe 22. When this wave arrives at the perforated section 50, its pressure is dissipated by the expansion of the resonator chamber 42. A secondary wave (the remaining component of the original high pressure wave) is incident on the catalyst 38. A portion of the secondary wave of exhaust gases passes through the catalytic converter 30 and on toward the first attenuation portion 34A. The portion of the secondary wave that does not go through the catalytic converter 30 is reflected off the catalyst 38 and back toward the engine 14. Before propagating to the upstream ends 36A of the headers 22, the pressure of the reflected wave is further diminished by expansion that occurs as the reflected wave encounters the perforated section 50. Therefore, the reflected wave that eventually makes it back toward the engine 14 is dissipated through expansions at the perforated section 50 (in addition to the portion which is passed through the catalytic converter 30). In addition to dissipation, a wave cancellation effect occurs under certain operating conditions and is tuned at least in part by the number of openings 46 and the size of the volume within the resonator chamber 42. In the occurrence of wave cancellation, two waves traveling in opposite directions are incident upon one another and at least one of the waves is cancelled out. For example, a wave of fresh exhaust gases from the engine 14 can cancel the effect of a reflected wave traveling from the collector section 26 toward the engine 14.
In the twin-cylinder engine 14 of the illustrated embodiment, in which both cylinders feed the single catalytic converter 30, the reflected wave off of the catalyst 38 is split at the collector section 26 and continues up both header pipes 22. In any exhaust configuration with multiple header pipes feeding a single catalytic converter, the reflected wave off of the catalyst is split at the collector among the header pipes. Therefore, the combination of the perforated section 50 and the resonator chamber 42 can deliver particularly good performance in twin-cylinder, shared exhaust setups, such as on the motorcycle 10 of
Turning now to the structure and exhaust flow downstream of the catalytic converter 30, a first passage 60 (e.g., pipe) shown in
The flow of exhaust gases changes direction in the third chamber 72 of the first attenuation portion 34A and enters a second passage 76 (e.g., pipe). The second passage 76 passes through the first and second chambers 64, 68 of the first attenuation portion 34A and opens into the chamber 62 of the second attenuation portion 34B. The second passage 76 is perforated at the locations passing through the first and second chambers 64, 68 of the first attenuation portion 34A to allow communication of the exhaust gases from the first passage 60 into the first and second chambers 64, 68 and vice versa. The second passage 76 has a cross-sectional size approximately the same as that of the first passage 60.
Exhaust gases enter the chamber 62 of the second attenuation portion 34B, which is provided with an aperture plate 80 (
From the chamber 62 of the second attenuation portion 34B, exhaust gases exit the muffler assembly 35 through a pair of outlet passages 88 (e.g., pipes) shown in
The muffler assembly 35 is configured to substantially surround the engine 14 along a central axis in the longitudinal direction of the motorcycle 10 defined by the front wheel 15 and the rear wheel 16. The catalytic converter 30 and the resonator chamber 42 extend substantially upright in front of the engine 14 and the first sound attenuation portion 34A fits up between the engine 14 and the rear wheel 16 of the motorcycle 10 (
Even with a small space with which to work (below the engine 14), the muffler assembly 35 is configured to take advantage of the space by utilizing the intermediate portion 35C as the second attenuation portion 34B. Likewise, where there is more ample space on the motorcycle 10 (immediately in front of and behind the engine 14), the muffler assembly 35 is also configured to take advantage of that space via the catalytic converter 30, the resonator chamber 42, and the first attenuation portion 34A. The first attenuation portion 34A extends not only behind the engine 14, but also upwards above a lower edge 17A of the transmission 17 (
The muffler assembly 35 defines an indentation or recess 100, which is contoured to receive the lower part of the engine 14, substantially matching a contour of the lower edge 14A of the engine 14. The depth of the recess 100 is equal to the height H1 of the first attenuation portion 34A minus the height H3 of the second attenuation portion 34B. Thus, the engine 14 is received into the recess 100 to a depth about two times the height H3 of the second attenuation portion 34B.
Thus, the invention provides, among other things, a compact muffler assembly 35 having an attenuation portion 34B below the engine 14, and a recess 100 configured to receive a significant portion of the engine 14. Various features and advantages of the invention are set forth in the following claims.
This application claims priority to U.S. patent application Ser. No. 11/770,051 filed Jun. 28, 2007, the entire contents of which is incorporated herein.
Number | Date | Country | |
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Parent | 11770051 | Jun 2007 | US |
Child | 11772507 | US |