1. Field of the Invention
The subject invention relates generally to multi-layered metal gaskets for use in internal combustion engines.
2. Related Art
Multi-layered steel gaskets are traditionally used to form a seal between two mating components of a mechanical system or device, such as an internal combustion engine, to prevent leakage of combustion gases, cooling water, lubricating oil, or the like. Common applications involve placing a multi-layered steel gasket assembly between the engine block and cylinder head and between the engine block and exhaust manifold. Cylinder head gaskets typically extend around the cylinder bores of an engine to seal high-pressure combustion gases within the cylinder bores as well as seal oil and coolant passages. Exhaust manifold gaskets typically extend around the exhaust ports of an engine to seal high temperature exhaust gases flowing into the exhaust system. Once installed, the multi-layered steel gasket assembly bears the load from a bolted connection of the engine components and relies upon this load to provide an adequate seal therebetween.
Such prior art multi-layered steel gaskets typically have a plurality of steel gasket layers stacked in relation to one another including at least a first gasket layer and a second gasket layer. The first gasket layer and second gasket layer each have an inboard edge defining at least one aperture to be sealed. Each gasket layer also presents an outboard region radially spaced from the aperture. In cylinder head gasket applications, the aperture typically corresponds with cylinder bores of the internal combustion engine. Alternatively, in exhaust manifold gasket applications, the aperture typically corresponds with exhaust ports of the internal combustion engine. The gasket layers define at least one sealing bead between the inboard edge and the outboard region to provide an area of increase gasket thickness for greater sealing capability. Typically, the sealing bead extends annularly about each aperture.
Some of the prior art multi-layered gaskets further include a stopper layer disposed between the gasket layers. In accordance with U.S. patent application Ser. No. 11/812,113 to Umehara, the stopper layer may be welded to the outboard region of the first gasket layer at a weld joint. In accordance with U.S. Pat. No. 5,277,434 to Kestly et al., the stopper layer may extend from the outboard region of the gasket layers to the inboard edge of the gasket layers. At least one coating of sealing material may be applied between the gasket layers such that the coating is substantially coextensive with the plurality of gasket layers. Despite the presence of the coating, small combustion gas leaks can develop between the gasket layers and the stopper layer. This problem can occur because the stopper layer and the gasket layers do not directly contact the coating in the area immediately surrounding the apertures.
A gasket assembly has a plurality of metal gasket layers including at least a first gasket layer and a second gasket layer each having an inboard edge circumscribing at least one aperture to be sealed and an outboard region radially spaced from the aperture. At least one sealing bead is disposed along at least one of the gasket layers between the inboard edge and the outboard region. A stopper layer is disposed between the gasket layers and attached to the outboard region of the first gasket layer at an attachment joint wherein the stopper layer extends from the attachment joint to the inboard edge of the gasket layers. A coating of sealing material is applied between the first gasket layer and the stopper layer. The coating extends from the inboard edge of the first gasket layer to present a contact region adjacent to and immediately surrounding the aperture defined by the first gasket layer. The stopper layer is in direct continuous contact with the coating applied therebetween for preventing gas leakage between the first gasket layer and the stopper layer and for preventing metal to metal contact between the first gasket layer and the stopper layer in the region of the coating.
Such a gasket is advantageous in that the coating is sandwiched between the first gasket layer and the stopper layer in a contact area immediately surrounding the aperture and is thus free of gaps, voids, or pockets between the coating and the first gasket layer and the coating and the stopper layer that would otherwise allow for possible fluid leakage. Accordingly, such a gasket assembly has improved service life and sealing performance compared to prior known gaskets of this general type because of the specific configuration of the contact region that eliminates gas leaks between the first gasket layer and the stopper layer.
These and other advantages and features of the subject invention will be readily appreciated, as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings, wherein:
Referring to the Figures, wherein like numerals indicate corresponding parts throughout the several views, a gasket assembly for providing sealing between an engine block and a cylinder head of an internal combustion engine is presented.
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Obviously, many modifications and variations of the present invention are possible in light of the above teachings and may be practiced otherwise than as specifically described while within the scope of the appended claims. These antecedent recitations should be interpreted to cover any combination in which the inventive novelty exercises its utility.
This application claims the benefit of U.S. Provisional Application Ser. No. 61/654,435, filed Jun. 1, 2012.
Number | Name | Date | Kind |
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5277434 | Kestly et al. | Jan 1994 | A |
5431418 | Hagiwara et al. | Jul 1995 | A |
6796562 | Stapel | Sep 2004 | B2 |
20050189724 | Schmitz | Sep 2005 | A1 |
20070090608 | Ueta | Apr 2007 | A1 |
20080023922 | Umehara | Jan 2008 | A1 |
20080042371 | Flemming | Feb 2008 | A1 |
20080093808 | Quick et al. | Apr 2008 | A1 |
20110192369 | Schmitz | Aug 2011 | A1 |
Number | Date | Country |
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H06207672 | Jul 1994 | JP |
H0741140 | Jul 1995 | JP |
2007139177 | Jun 2007 | JP |
2008520917 | Jun 2008 | JP |
Number | Date | Country | |
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20130320630 A1 | Dec 2013 | US |
Number | Date | Country | |
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61654435 | Jun 2012 | US |