Applicants claim priority under 35 U.S.C. §119 of German Application No. 102 40 671.5 filed on Sep. 4, 2002. Applicants also claim priority under 35 U.S.C. §365 of PCT/DE2003/001895 filed on Jun. 7, 2003. The international application under PCT article 21(2) was not published in English.
The invention pertains to a knock sensor for an internal combustion engine with an electronically evaluated vibration sensor.
The vibration sensor of known knock sensors is realized, for example, in the form of a piezoceramic element. Knock sensors of this type are known, for example, from EP 0 47 22 19 B1, EP 0 844 470 D1 and DE 195 39 919 C2. US 4,448,059 A discloses a knock sensor for an internal combustion engine with an electronically evaluated vibration sensor in the form of a piezoresistive layer that is rigidly applied onto a surface section of a base body.
DE 199 54 164 discloses sensors for determining state variables, particularly forces exerted by mechanical components, by utilizing amorphous carbon layers with a thickness between 10 nm and 500 μm. These amorphous carbon layers may consist, in particular, of DLC (Diamond-Like Carbon) layers and have piezoresistive properties. These layers can be applied onto surfaces with different geometries. For example, these layers may be applied by means of a PVD (Physical Vapor Deposition) or CVD (Chemical Vapor Deposition) method. A sensor provided with such carbon layers can be variably utilized and easily adapted to the different requirements of certain applications. A sensor of this type also makes it possible to measure Parameters in a reliable and reproducible fashion.
In other respects, DE 19 831 372 discloses washers that are provided with measuring layers and used for controlling non-positive connections.
In a knock sensor of the initially cited type, the invention aims to achieve a simple and reliable acquisition of measuring signals, as well as an equally simple and reliable transmission thereof.
This objective is attained with a knock sensor of the initially cited type that is realized in accordance with the characteristics disclosed in the characterizing portion of claim 1.
Advantageous and practical embodiments form the objects of the dependent claims.
The invention essentially proposes to eliminate, in comparison with the current state of the art, an additional component that usually consists of the vibration sensor in a knock sensor of this type, namely by directly applying a thin measuring layer onto the surface of a component that not only fulfills the vibration sensor function.
According to the invention, the measuring layer is applied onto a tensioning element in the form of the spring washer provided in the knock sensor. The spring washer may be realized, in particular, in such a way that the seismic mass of the knock sensor that is usually braced within the knock sensor by means of a spring washer is an integral part of the spring washer.
In the piezoresistive amorphous carbon layers to be utilized in accordance with the invention, the vibrations of the internal combustion engine cause voltage changes in the layer, when said vibrations act upon the spring washer, wherein these voltage changes can be conventionally evaluated. When utilizing a spring washer according to the invention with a piezoresistive amorphous carbon layer, the deformation of the spring washer is used for generating electrical measurable voltage changes in the layer.
The high measuring sensitivity of the measuring layer according to the invention is particularly well suited for a telemetric signal evaluation. With respect to the principle of telemetric signal evaluation methods to be considered for this purpose, we refer to the state of the art, for example, according to DE 40 34 019 C1, EP 0 533 709 B1 and DE 37 14 195 A1.
Advantageous and practical embodiments of the invention are illustrated in the figures.
The figures respectively show in the form of a longitudinal section:
The knock sensor according to
The face of the spring washer 4 that points to the head of the screw 2 is sectionally provided with a piezoresistive amorphous carbon layer in the form of a DLC layer. Electric lines 6 lead from this layer to an electronic evaluation unit that is not shown in the figures. The thickness of the layer preferably lies in the range between 1 and 10 μm.
If knocking of the internal combustion engine occurs, the seismic mass 3 realized in the form of an annular part is acted upon by the spring washer 4 and thusly stimulated. This causes the seismic mass to exert a corresponding load upon the spring washer 4 such that a corresponding voltage change occurs in the DLC layer 5 applied onto the spring washer 4. This voltage change is transmitted to an evaluation electronic via the electric lines 6 and evaluated therein. In order to realize a telemetric transmission, the measuring signals originating from the layer 5 can be transmitted by means of a telemetric signal tap, or a transponder 11 that is arranged on the component in question together with the DLC layer 5. Conventional transmission cables and their connecting means can be eliminated by utilizing this customary transmission principle.
In the embodiment according to
It would also be conceivable, in principle, to respectively apply a DLC layer 5 onto both sides of the spring washer 4. 7.
When utilizing such a special screw 8, a corresponding screw-on mounting body can be eliminated as shown in
In the embodiment according to
All knock sensors shown are provided with a cover housing 10.
Number | Date | Country | Kind |
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102 40 671 | Sep 2002 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/DE03/01895 | 6/7/2003 | WO | 00 | 3/3/2005 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2004/025238 | 3/25/2004 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
4448059 | Kondo et al. | May 1984 | A |
4463610 | Anderson, III et al. | Aug 1984 | A |
5753798 | Engeler et al. | May 1998 | A |
6487898 | Haefner et al. | Dec 2002 | B1 |
Number | Date | Country |
---|---|---|
37 14 195 | Nov 1988 | DE |
40 34 019 | Jul 1992 | DE |
195 39 919 | May 1996 | DE |
198 31 372 | Jan 2000 | DE |
199 54 164 | Jun 2001 | DE |
0 533 709 | Dec 1993 | EP |
0 472 219 | Dec 1994 | EP |
0 649 008 | Jun 1998 | EP |
0 844 470 | Feb 2002 | EP |
Number | Date | Country | |
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20050252276 A1 | Nov 2005 | US |