![]() SENSOR ELEMENT
专利摘要:
The invention relates to a sensor element (1) having a substrate (2) which has a strain-sensitive element (3) which is preferably applied by thin-film technology and which serves to measure the deformation of the substrate (2) when pressure is applied or the force is applied. According to the invention, the strain-sensitive element of XAlOyN1-y, wherein X is a metal having a high melting temperature in the range greater than 1400 ° C and 0 <y <0.4. On the strain-sensitive element (3), a passivation layer (5) may be applied. 公开号:AT515945A4 申请号:T50612/2014 申请日:2014-09-05 公开日:2016-01-15 发明作者:Dietmar Dr Kröger;Peter Dipl Ing Schmid;Ulrich Dr Schmid;Alexander Dr Schricker;Christof Zarfl 申请人:Piezocryst Advanced Sensorics; IPC主号:
专利说明:
The invention relates to a sensor element comprising a substrate which has a strain-sensitive element which is preferably applied by means of thin-film technology and which serves to measure the deformation of the substrate upon pressurization or force introduction. In order to measure, for example, static pressures, common, mostly membrane-based sensor concepts use piezoresistive methods or so-called strain gauges (DMS) in order to be able to detect local mechanical strains with high precision. However, for high temperature applications (up to 700 ° C), common DMS materials (such as CrNi) are not applicable because they irreversibly alter their electro-mechanical properties after high temperature loading or show a strong tendency to oxidize. High melting point metallic materials, e.g. Pt. (See "A Robust Pressure Sensor for Harsh Environmental Applications", S.Fricke, A. Friedberger, H. Seidel, U. Schmid, Sensors and Actuators A: Physical, Volume 184, September 2012, pages 16-21), can in principle be used up to the temperature range given in the given, but have a very high temperature coefficient of electrical resistance (TCR), which requires a very precise temperature measurement at the sensor element, which is technically hardly feasible over the entire temperature range. The aim is thus the development of thin-film systems with high temperature stability, a TCR near zero and the highest possible K-factor, which is a measure of the change in the electrical resistance during mechanical strain. Ni: a-C: H thin films meet the latter two requirements, but are only stable up to about 300 ° C. Such layers are described, for example, in " Pressure sensitivity of piezoresistive nickel-carbon Ni: aC: H thin films ", SteffenUhlig, Hanna Schmid-Engel, Tobias Speicher, Günter Schultes, Sensors and Actuators A: Physical, Volume 193, 15 April 2013, Pages 129 -135, described. From EP 1 9918 49 B1, a high-temperature pressure sensor element for measuring pressures even above 400 ° C. has become known in this connection. The high-temperature pressure sensor element or the pressure sensor consists of a substrate in which an interior space is configured. Furthermore, a deformable membrane is provided, which in use separates the interior space from the exterior space and deforms in the event of a change in the external pressure relative to the pressure in the interior space. On the deformable membrane is arranged a structure of strain gauges forming a strain gauge for measuring the deformation of the membrane. In this case, the membrane, the substrate and the strain gauge are formed from one and the same high temperature stable material, preferably an alloy such as a nickel base alloy. Between the strain gauge and the diaphragm is disposed an electrical insulation layer consisting of BN, MgO or Al 2 O 3. Furthermore, the strain gauge element may have a passivation layer consisting of the material of the insulation layer. The disadvantage is that said metallic alloys have a relatively high TCR value. From "Strain sensitive Pt-SiO 2 nanocermet thin films for high temperature pressureand force sensors", H. Schmid-Engel, S. Uhlig, U. Werner, G. Schultes, Sensors and Actuators A: Physical, Volume 206, 1 February 2014, pages 17-21, thin-film high-temperature strain gages, for example made of Pt-SiO 2, are known which have a high K factor and low temperature coefficient of resistance (TCR) and can be used in a temperature range up to 300 ° C. The object of the invention is to develop a sensor element with a substrate having the strain-sensitive element in such a way that a high temperature stability, a TCR close to zero and the highest possible K factor can also be realized in the high temperature range. This object is achieved according to the invention in that the strain-sensitive element consists of XAIOyNi-y, where X is a metal with a high melting temperature in the range greater than 1400 ° C and 0 < y < 0.4 applies. Preferably, the strain-sensitive element consists of a composite layer applied to the substrate by the PVD method (for example sputtering or vapor deposition method) or CVD method, the strain-sensitive element containing at least one metal X selected from Ti, Ta and Pt. It is known that XAIOyNi_y layers have a high resistance to oxidation. It has now been shown that the electro-mechanical characteristics (K- Factor, TCR) for use as a strain gage. With the help of the additional oxygen content, a further degree of freedom is created in order to be able to set the electro-mechanical parameters in a targeted manner. According to the invention, the proportion of aluminum in the strain-sensitive element, which makes a dielectric connection with nitrogen and oxygen, to the proportion of the metallic component is weighted such that the TCR of the strain-sensitive element assumes minimum values, preferably approximately zero. Thus, in addition to the aluminum content, a metallic component is added during layering. The composite layer is preferably deposited by a thin-film sputtering technique whereby the combination of metallic portion (with TCR> 0) and dielectric matrix (with TCR <0) in one layer makes it possible to set the TCR to approximately zero and, in addition, to provide a high Factor (> 2). For use as a sensor for a prolonged period of time under extreme temperature loads, it is desirable to place a thin film in a defined atmosphere which ensures that at high temperatures, there are no conversion processes in the film. The strain-sensitive element is thus preferably arranged in a closed sensor atmosphere with a defined oxygen content, preferably in a sealed sensor housing. By introducing the XAlOyN ^ y thin film into a closed sensor atmosphere, the environment of which is dominated by, for example, a nickel base material (eg Haynes 230), the high temperature behavior of the film can be maintained at a very stable level. The nickel-based alloy binds at high temperature ends residual oxygen in the sensor atmosphere, whereby the sealed structure prevents the backflow of atmospheric oxygen. As a result, there is a defined oxygen content in the sensor atmosphere, the oxidation behavior of the thin film can be controlled by the ratio of the oxydischen and nitridischen shares. Thus, changes in the layer over a long period of time can be minimized. According to the invention, the strain-sensitive element may comprise a passivation layer, preferably of Al 2 O 3 or AlN. By applying a high-temperature-stable passivation, the long-term stability can be further increased. The invention will be explained in more detail below with reference to drawings. Show it: 1 shows a sensor element according to the invention in a sectional view; FIG. 2 shows a top view of a sensor element according to the invention (without passivation layer); FIG. 3 shows an embodiment variant of the sensor element according to the invention in the housing of a pressure sensor; 4 shows a diagram of the K-factor for a strain-sensitive element of TiAlO.sub.2 N. 0.8 in the temperature range up to 350.degree. such as Fig. 5 is a TCR diagram for TiAIOo, 2N0,8 in the differential temperature range up to 350 ° C. FIGS. 1 and 2 show a sensor element 1 according to the invention with a substrate 2, which has a thin-film-applied, strain-sensitive element 3 which serves to measure the deformation of the substrate 2 upon application of pressure or introduction of force. The strain-sensitive element 3 consists of XAlOyN ^ y, where X is a metal having a high melting temperature, for example titanium. The factor y is in a range between 0 and 0.4. The strain-sensitive element 3 and the subsequent substrate region have a passivation layer 5, for example made of Al 2 O 3. In the plan view according to FIG. 2, the passivation layer has been omitted, so that the strain-sensitive element 3 becomes visible as a meandering strain gauge together with a connection contact. In the embodiment according to FIG. 3, the sensor element 1 according to the invention lies in a closed sensor atmosphere A with a defined sensor Oxygen content in a sealed sensor housing 4 of a pressure sensor 10vor. As the substrate 2, the membrane 11 of the pressure sensor 10 is used, on the inner side of which the strain-sensitive element 3 is applied as a thin layer. the housing 4bzw. the immediate environment for the strain sensitive element 3 is at least partially made of Ni base material. In the illustrated example, the diaphragm 11 and the pressure transmitting member 12 acting on the piezoelectric elements 13 may be made of Ni base material. In Figs. 4 and 5, for a strain-sensitive element made of TiAl0.21M0.8, the K-factor (gauge factor) and the TCR ((R-R0) / R0) are each in a differential temperature range between 0 and 350 ° C with respect to a reference temperature - shown, wherein the reference temperature here is the room temperature.
权利要求:
Claims (9) [1] PATENT CLAIMS 1. A sensor element (1) comprising a substrate (2) having a strain-sensitive element (3), preferably applied by thin-film technique, for measuring the deformation of the substrate (2) under pressure or application of force, characterized in that the strain-sensitive element (3 ) is made of XAIOyNi.y where X is a metal having a high melting temperature in the range greater than 1400 ° C and 0 < y < 0.4 applies. [2] Sensor element (1) according to claim 1, characterized in that the strain-sensitive element (3) consists of a composite layer which can be applied to the substrate (2) in the PVD method, preferably sputtering or vapor deposition method or by CVD method , [3] 3. Sensor element (1) according to claim 1 or 2, characterized in that the strain-sensitive element (3) comprises at least one metal X from the group Ti, Ta and Pt. [4] A sensor element (1) according to any one of claims 1 to 3, characterized in that the proportion of aluminum in the strain-sensitive element (3), which enters into a dielectric compound with nitrogen and oxygen to the proportion of the metallic component, is weighted as the TCR of the strain-sensitive element (3) assumes minimum values, preferably approaching 0. [5] Sensor element (1) according to claim 4, characterized in that the titanium content in a strain-sensitive element (3) of TiAION is between 0.4 and 0.5% by weight. [6] 6. Sensor element (1) according to one of claims 1 to 5, characterized in that the strain-sensitive element (3) is arranged in a closed sensor atmosphere with a defined oxygen content, preferably in a sealed sensor housing (4). [7] 7. Sensor element (1) according to claim 6, characterized in that the sensor housing (4) consists at least partially of Ni-base material [8] A sensor element (1) according to any one of claims 1 to 7, characterized in that the substrate (2) to which the strain-sensitive element (3) is applied consists of Ni base material, for example Haynes230, made of ceramic or a piezoelectric material. [9] Sensor element (1) according to one of Claims 1 to 8, characterized in that the strain-sensitive element (3) has a passivation layer (5), preferably of Al 2 O 3 or AlN.
类似技术:
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同族专利:
公开号 | 公开日 AT515945B1|2016-01-15| EP2993453B1|2017-02-22| US20160069758A1|2016-03-10| US9618406B2|2017-04-11| EP2993453A1|2016-03-09|
引用文献:
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2020-08-15| MM01| Lapse because of not paying annual fees|Effective date: 20190905 |
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申请号 | 申请日 | 专利标题 ATA50612/2014A|AT515945B1|2014-09-05|2014-09-05|SENSOR ELEMENT|ATA50612/2014A| AT515945B1|2014-09-05|2014-09-05|SENSOR ELEMENT| EP15181394.6A| EP2993453B1|2014-09-05|2015-08-18|Sensor element| US14/842,193| US9618406B2|2014-09-05|2015-09-01|Sensor element| 相关专利
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