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1. Field of the Invention
The present invention relates generally to exhaust systems for internal combustion engines, and, more particularly, to a flange for connecting an exhaust conduit to a marine engine wherein the exhaust conduit is prevented from being positioned in certain improper configurations.
2. Description of Related Art
Marine vessels are typically configured with a propulsion system having an internal combustion engine mounted internally within the vessel hull. Exhaust generated by the engine is commonly routed through exhaust conduit to the stern or rear of the vessel via one or more exhaust ducts and is discharged through one or more exhaust ports formed in the transom. In a large number of applications the exhaust is routed through a turbo charger that has an outlet in communication with an exhaust conduit. Water is often injected into the exhaust stream to cool the exhaust gas flowing through the exhaust system, and one or more silencers may be installed within the exhaust conduit to silence noise associated with the engine and exhaust gases.
A variety of structures are known in the background art for use in silencing marine exhaust noise. The present inventor has invented a number of novel marine exhaust components that have greatly improved the silencing and efficiency of marine exhaust systems. Among those inventions developed by the present inventor are: U.S. Pat. No. 4,918,917 for a Liquid Cooled Exhaust Flange; U.S. Pat. No. 5,196,655, for a Muffler for Marine Engines; U.S. Pat. No. 5,228,876, for a Marine Exhaust System Component comprising a heat resistant conduit; U.S. Pat. No. 5,262,600 for an In-line Insertion Muffler for Marine Engines; U.S. Pat. No. 5,444,196 for an improved In-line Insertion Muffler for Marine Engines; U.S. Pat. No. 5,504,280, for a Muffler for Marine Engines; U.S. Pat. No. 5,616,893, for a Reverse Entry Muffler With Surge Suppression Feature; U.S. Pat. No. 5,625,173, for a Single Baffle Linear Muffler for Marine Engines; U.S. Pat. No. 5,718,462 for Muffler Tube Coupling With Reinforcing Inserts; and U.S. Pat. No. 5,740,670, for a Water Jacketed Exhaust Pipe for Marine Exhaust Systems.
Problems have been experienced, however, when the exhaust conduit is installed or otherwise positioned in a manner that allows for water to flow back to the turbocharger outlet and/or engine exhaust manifold. More particularly, since water is injected into the exhaust conduit for cooling purposes, it is important that the exhaust conduit be angled downward away from the engine and turbo charger to prevent cooling water in the conduit from flowing back toward the turbocharger when the engine in shut down. Due to space limitations invariably found in marine engine rooms, most exhaust conduits are connected to the turbo charger by an elbow section so as to route the conduit close to the engine. As a result, mechanics and/or installers have been known to install or move the elbow/conduit in rotated configurations wherein the conduit follows and ascending path from the turbo charger rather than a descending path. When the exhaust conduit is installed in the ascending configuration cooling water in the conduit will flow back toward the engine turbocharger when the engine is shut down. As should be apparent, exposing the engine and/or turbocharger to the corrosive effects of saltwater leads to rapid failure.
Accordingly, there exists a need for an improved flange for use in mounting an exhaust elbow conduit to a marine engine and/or turbocharger so as to prevent rotational positioning of the elbow/conduit in an ascending configuration.
The present invention provides an improved flange particularly adapted for use in mounting marine exhaust conduit to the turbocharger of a marine engine. The flange comprises a rigid mounting ring having a plurality of radially projecting stop blocks circumferentially positioned at approximately 0, 90, 180, and 270 degrees. The radially projecting blocks function to limit rotation of the flange within 60 degrees of travel. The flange is connected to an exhaust conduit, typically an elbow and mounted directly to the outlet of the engine turbocharger using suitable fasteners and brackets. The turbocharger mounting brackets engage the flange between circumferentially adjacent radially projecting blocks thereby preventing rotation of the exhaust conduit/flange assembly to positions wherein cooling water would tend to flow into the turbocharger/engine.
Accordingly, it is an object of the present invention to provide an improved flange for use in connecting a marine exhaust conduit to a turbo charger.
Another object of the present invention is to provide an improved marine exhaust conduit mounting flange that limits positioning of the exhaust conduit so as to prevent cooling water from migrating into the turbo charger and/or engine.
In accordance with these and other objects that will become apparent hereinafter, the instant invention will now be described with particular reference to the accompanying drawings.
With reference now to the drawings
A significant aspect of the present invention involves adapting the above-referenced structure with radially projecting stop blocks, referenced as 20. In a preferred embodiment four (4) stop blocks 20 are circumferentially positioned at approximately at circumferentially spaced locations, preferably 0, 90, 180, and 270 degrees respectively. Each stop bock 20 preferably has opposing sides spaced in correspondence with a 30 degree angular segment projected onto the outer circumference of flange 10. Accordingly, there exists 60 degrees of circumference between circumferentially adjacent stop block sides. Radially projecting stop blocks 20 function to limit rotation of the flange within 60 degrees of travel.
As best depicted in
The instant invention has been shown and described herein in what is considered to be the most practical and preferred embodiment. It is recognized, however, that departures may be made therefrom within the scope of the invention and that obvious modifications will occur to a person skilled in the art.
This application claims the benefit of U.S. Provisional Patent Application Ser. No. 60/539142, filed Jan. 26, 2004.
Number | Date | Country | |
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60539142 | Jan 2004 | US |