The invention relates to a sealing system, in particular for sealing of multipart exhaust-gas lines for an internal combustion engine, having at least first and second flange parts. The flange parts conduct a heat flow and delimit a receiving space for at least one sealing element between them.
Sealing systems of this type are known. DE 10 2004 060 845 A1 shows, for example, such a sealing system for the exhaust gas line of a reciprocating piston engine. The sealing element is a metallic gasket in the form of a profile body with a C-shaped profile cross section. Sealing elements on exhaust gas lines are subject to very high temperatures which can exceed 600° C. Even if materials are used with properties that are suitable with respect to heat resistance, the sealing elements at the prevailing high operating temperatures lose their functional properties required for sealing. Especially the elasticity of the sealing elements is reduced by creep processes due to overly high thermal loads.
Accordingly, an object of the invention is to provide a sealing system which, when used in a hot gas region, ensures reliable sealing even when high temperatures occur on the exhaust gas lines to be sealed.
According to the invention, this object is basically achieved by a sealing system having flange parts to be sealed against one another and to form an annular flange facing away from the heat flow and projecting transversely to the heat flow to the outside. A chambering is formed for the sealing element. The material of the annular flange forms a certain thermal shielding of the sealing element relative to the heat flow. The sealing element chambered in an annular groove is additionally protected by a cover element within the annular groove forming thermal shielding at least on the side of the sealing element facing the end face of the flange part, i.e., on the open side of the annular groove which is thermally most heavily loaded. The sealing element is protected especially effectively against overly high thermal loads such that the system according to the invention can also be reliably used on exhaust gas lines which are thermally highly loaded.
Preferably, the cover element is a metallic annular body.
When there is an annular body in the form of a flat ring, it is preferably inserted such that it extends between the sealing element and the facing end face of the flange part, and thus, forms a thermal barrier on the region of the annular groove most heavily thermally loaded and in which the sealing element is chambered.
Instead of a flat annular body, the cover element can be formed by a profile ring having an arched profile or an angled profile.
In such embodiments the annular body is preferably inserted into the annular groove such that it surrounds the sealing element both on the side facing the end face and on the side facing another wall of the receiving space.
Especially good thermal shielding of the sealing element in such embodiments can be achieved when the cover element also surrounds the sealing element on the side nearest the heat flow, that is, on that side facing the radially inside wall of the annular groove.
The sealing element is preferably a molded ring seal, with a C-shaped or V-shaped profile cross section. In this case, the sealing element with the C-profile is preferably installed in the annular groove such that the profile is open radially to the inside, that is, towards the pressure side of the system.
Instead of a V-shaped or C-shaped profile cross section, the sealing element could also have a meandering profile cross section, in the form of a bellows solution in which several folds lying on top of one another form the cross section.
Alternatively, metal bead seals can be installed in the receiving space. In any case, the invention ensures thermal protection for the respective sealing element so that for metallic sealing elements of a material available for high temperature use, reliable sealing in hot gas regions is ensured. The annular shape for the sealing element can be circular or nearly circular. Furthermore, ring shapes are conceivable in the form of an oval or a rectangular shape, preferably with rounded corner regions. The respective annular groove must then preferably follow the pertinent ring shape of the sealing element.
Other objects, advantages and salient features of the present invention will become apparent from the following detailed description, which, taken in conjunction with the annexed drawings, discloses preferred embodiments of the present invention.
Referring to the drawings which form a part of this disclosure:
In the figures, a first line section and a second line section of an exhaust gas line or other hot fluid conduit are designated as 1 and 3, respectively. In the operation of the pertinent internal combustion engine, the exhaust gas line conducts an exhaust gas-heat flow 5 with a correspondingly high exhaust gas temperature. The line sections 1 and 3 are sealed against one another by the sealing system according to the invention and are to be connected to one another. Each line section has a flange part 9 and 11 respectively projecting radially to the outside relative to the axis 7 of the line. The flange parts 9 and 11 together form an annular flange 13 and have end faces 15 and 17 facing one another. To connect the line sections 1 and 3 to one another, the flange parts 9, 11 of the annular flange 13 are braced to one another by suitable clamping means which may be conventional and which are therefore not shown. For example, the clamping means could be a clamping ring pulled onto peripheral bevels 25 of the flange parts 9 and 11 (not shown).
The sealing element for sealing between the flange parts 9 and 11 is a metallic molded ring seal 31 with a C-shaped profile cross section. As indicated above, a molded ring seal with a different profile cross section or a bead seal or the like could be used. In any case, the sealing element is at least partially chambered and is enclosed in a receiving space 33 formed between the flange parts 9 and 11. As shown in the drawings, in the embodiments of
According to the invention, additional heat protection for the molded ring seal 31 located in the receiving space 33 is a cover element 47 inserted into the annular groove 45. The cover element 47 forms a thermal barrier between the molded ring seal 31 and the thermally most heavily loaded region of the receiving space 33. In the embodiment of
In the embodiment of
Instead of the illustrated forms of the cover element 47, other profile cross sections could be used. For example, a U profile surrounding the sealing element along three sides can be used. In any case, the cover element 47 is installed in the annular groove 45 such that the molded ring seal 31 is covered at least on the side facing the junction site between the end faces 15 and 17 of the flange parts 9 and 11. Preferably, in addition, the correspondingly shaped cover element 47 extends over the molded ring seal 31 on at least one other thermally endangered site.
While various embodiments have been chosen to illustrate the invention, it will be understood by those skilled in the art that various changes and modifications can be made therein without departing from the scope of the invention as defined in the appended claims.
Number | Date | Country | Kind |
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10 2006 045 584 | Sep 2006 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2007/007644 | 9/1/2007 | WO | 00 | 2/4/2009 |
Publishing Document | Publishing Date | Country | Kind |
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WO2008/037330 | 4/3/2008 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
2733969 | Polk | Feb 1956 | A |
3058750 | Taylor | Oct 1962 | A |
3132870 | Pschera | May 1964 | A |
3140342 | Avery et al. | Jul 1964 | A |
3217922 | Glasgow | Nov 1965 | A |
3298794 | Mikesell, Jr. et al. | Jan 1967 | A |
3418001 | Rentschler et al. | Dec 1968 | A |
3561776 | Wilson | Feb 1971 | A |
3595588 | Rode | Jul 1971 | A |
3820799 | Abbes et al. | Jun 1974 | A |
3869132 | Taylor et al. | Mar 1975 | A |
3918725 | Dryer | Nov 1975 | A |
4188037 | Abbes et al. | Feb 1980 | A |
4218067 | Halling | Aug 1980 | A |
4261584 | Browne et al. | Apr 1981 | A |
4444403 | Morris | Apr 1984 | A |
4445694 | Flaherty | May 1984 | A |
4477085 | Bridges et al. | Oct 1984 | A |
4477091 | Adamek | Oct 1984 | A |
4603892 | Abbes et al. | Aug 1986 | A |
4747624 | Faber et al. | May 1988 | A |
4850521 | Servant | Jul 1989 | A |
4915925 | Chung | Apr 1990 | A |
5076591 | Gentile | Dec 1991 | A |
5112664 | Waterland, III | May 1992 | A |
5511828 | Kurek et al. | Apr 1996 | A |
5558344 | Kestly et al. | Sep 1996 | A |
5799953 | Henderson | Sep 1998 | A |
6517086 | Jamrog | Feb 2003 | B1 |
6540234 | Atkinson et al. | Apr 2003 | B1 |
6755422 | Potter | Jun 2004 | B2 |
7048201 | Kerchner et al. | May 2006 | B2 |
7128323 | Iguchi et al. | Oct 2006 | B2 |
7218323 | Halmshaw et al. | May 2007 | B1 |
7316762 | Lah | Jan 2008 | B2 |
7845649 | Kowalczyk | Dec 2010 | B2 |
20030080519 | Kerchner | May 2003 | A1 |
Number | Date | Country |
---|---|---|
1 944 582 | Jan 1972 | DE |
29 09 223 | Oct 1979 | DE |
198 16 862 | Oct 1999 | DE |
10 2004 060 845 | Jun 2006 | DE |
1 099 835 | May 2001 | EP |
11 210 886 | Aug 1999 | JP |
Number | Date | Country | |
---|---|---|---|
20090322039 A1 | Dec 2009 | US |