AU4496200A - Self-compensated ceramic strain gage for use at high temperatures - Google Patents

Self-compensated ceramic strain gage for use at high temperatures Download PDF

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AU4496200A
AU4496200A AU44962/00A AU4496200A AU4496200A AU 4496200 A AU4496200 A AU 4496200A AU 44962/00 A AU44962/00 A AU 44962/00A AU 4496200 A AU4496200 A AU 4496200A AU 4496200 A AU4496200 A AU 4496200A
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strain
sensor
ito
self
tcr
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AU44962/00A
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Otto J. Gregory
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Rhode Island Board of Education
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Rhode Island Board of Education
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/16Measuring arrangements characterised by the use of electric or magnetic techniques for measuring the deformation in a solid, e.g. by resistance strain gauge

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measurement Of Length, Angles, Or The Like Using Electric Or Magnetic Means (AREA)

Description

PCT/USOO/11 3 3 4 WO 02/35178 1 Title of the Invention Self-Compensated Ceramic Strain Gage For Use at High Temperatures Background ofthe _Invention 1. Field of the Invention 5 The invention relates to thin film strain gages. 2. Description of the Relevant Art The accurate measurement of both static and dynamic strain, at elevated temperatures is frequently required to determine the instabilities and life-times of various structural systems, and in particular, advanced aerospace propulsion systems. 10 Conventional strain gages are typically applied to both stationary and rotating components for this purpose but are usually limited in scope due to their intrusive nature, severe temperature limitations and difficulties in bonding. Thin film strain sensors are particularly attractive in the gas turbine engine environment since they do not adversely effect the gas flow over the surface of a i5 component and do not require adhesive or cements for bonding purposes. Typically, thin film strain gages are deposited directly onto the surface of a component by f sputtering on other known thin film deposition technology and as a result are minie communication with the surface being deformed- In general te response or gage factor (g), of a strain gage is the finite resistance change of the 20 Sensing element when subjected to a strain and can result from (a) changes in dimension of the active strain element and/or (b) changes in the resistivity (p) of the active strain element. Further, the active strain elements used in a high temperature static strain gage, must exhibit a relatively low temperature co-efficient of resistance (TCR) and drift rate (DR) so that the thermally induced apparent strain is negligible 25 compared to the actual mechanical applied strain. One material of choice for high temperature thin film strain gages is a wide conductor, e.g. indium-tin oxide (ITO), due to its excellent electrical and band semiconutr erg athg eprtr-We sd chemical stability and its relatively large gage factor at high temperature. When unic alone it is usually limited by relatively high TCRs as is the case for mandated iTo 30 semiconductors. However, as disclosed herein the TCR of a self-compens PCT/US00/11334 WO 02/35178 2 strain sensor can be reduced using a metal, e.g. Pt as a thin film resistor placed in series with the active ITO strain element. However, the proper combination of materials, patterns and dimensions to fabricate a strain gage with a predetermined TCR is mostly a matter Of empirical 5 observation, i.e. trial and error. that the sensor is to With the present invention, knowing the temperature range a a seerence be operative at and the resistivities of the materials each at a working and a reference temperature one can automatically determine the TCR of a high temperature strain gage. sl- estdsri aesno aiga 10 Broadly the invention comprises a self-compensated strain gage sensor having an automatically determined TCR including a TCR of essentially zero. The sensor comprises a wide band semiconductor deposited on a substrate. A metal is deposited on the substrate and in electrical communication with the semi-conductor functioning as serial resistors, the length, width and thicknesses of the semi-COnductor and the metal 15 are selected based on their resistivities at selected working and reference temperatures and the TCR automatically determined. of silicon carbide, The semiconductors can be selected from the group consisting scn caride aluminum nitride, zinc oxide, gallium nitride, indium nitride, scandium nitride, titanium nitride, chromium nitide, zirconium nitirde, boron carbide, diamond, titanium titaiumnitide chomin n deziroemr e allium phosphide, aluminum gallium 20 carbide, tantalum carbide, zirconium carbide, i m selenide, cadiu nitride, zinc oxide doped with alumina, cadmium telleride, cadmium eleide, n sulfide, mercury cadmium telleride, zinc selenide, zinc telleride, magneslu- telleride, tin oxide, indium oxide, manganates-mangaese oxides witx iron Oxides, iron oxide-ihi chromium oxide, iron oxide-magneso oxide, rutheni oxide 25 doped nickel oxide, tantalum nitride, indium-tin oxide-gallium oxide-tin oxide and combinations thereof. consisting of platinum, The metal resistors can be selected from the, ting h i rhodium, palladium, gold, cbroiut, rhenium, irridu , tungsten, molybdenum, nickel, cobalt, aluminum, copper, tantalum, alloys of platinum and rhodium and 30 combinatiOns thereof. - tin oxide and a particularly A particularly preferred semi-conductor is indium preferred metal is platinum.
PCT/USOO/11 3 3 4 WO 02/35178 3 Brief Description of the Drawings Fig. 1 is an illustration of a sensor design; Fig. 2 is a simulated circuit of the design of Fig. 1; and Fig. 3 is an illustration of an alternative sensor deisgn; and 5 Fig. 4 is a graph of the resistance (signal) of the sensor of Fig. 1 changing with temperature. Description ofg te Preferred EmbodimenLt(s To establish adequate design rules for the self-compensated strain gage, the TCR 10 of a self-compensated strain sensor is first modeled. The following approach is used to model the TCR of an ITO sensor with Pt self-compensation circuitry: TCRcow= (Rcowf - RCoMP,o)/ (Rcow,o * AT) Where Rcowf is compensated sensor resistance at a specific temperature, Rcow,o is compensated sensor resistance at a reference temperature, AT is the temperature 15 difference, and (2) RcoP,f= Rrt~f + Rrro,f(2 Rcowo =RP,o + Rrroo (3) Substituting equation (2) and (3) into equation (1), TCRcomp, results in - TCRCOMP = ((Rpt,f+ RITo,f) - (Rmto + Rrro,o)) / ((Rto + Rrro,o) * AT) (4) 20 The resistance R is related to resistivity (p) which is a constant at a specific temperature, R= p*L / (w * t) (5) Where L, w and t are length, width and thickness of sensor film. Substituting R into equation (4) TCRcow, results in a final format equation to model TCRcour 25 TCRcomv =(Aprt * Apt + Aprro * Arro) / ((ptO * APt + prTOO * Arro) * AT) (6) Where ApRt Pf - PrtO ApIo= Prrof - PITOO (8) Apt= LpI (Wpt * tpt) (9) 30 ATo = Lrro / (wrro * trro) (10) are resistivities of Pt and ITO at a working and reference ptf, pMt0 ,prroxf, prro'o WO 02/35178 PCT/USOO/11334 4 temperatures. In equation (6), all resistivities and AT are constants, Appt > 0 and Aprro < 0, a different length (L), width (w) and thickness (t) of ITO and Pt can be designed to let the TCR of self- compensated ITO-Pt sensor film be zero. Also from equation (4), the TCR of self-compensated sensor can be related to 5 TCR of Pt and ITO. TCRcomp = ((Rpt,f + Rrro,) - (Rpto + RiTo o)) /((Rpto + Rrro,o) * AT) (4) TCRcoup {[(Rpt~f - Rro)/(Rrto*RrroO*AT)]+{(Rro,f Rrro,o)/(Rpt,o*Rrro,o*AT)]}*B Where 10 B = (Rpt,o*Rrroo) / (Re,o + Rrro,o) simplify this equation, the TCR of self-compensated sensor related to constant TCR of Pt and ITO. TCRcouw = (TCRet*Rto + TCRrro*RTo,o)/(RPto + Rio) (11) The mathematical expressions set forth above were solved using commercially 15 available software such as Mat Lab or Math Cad software loaded into a personal computer. Sensor Preparation A self-compensated ITO sensor was fabricated by sputtering Pt and ITO films that were subsequently patterned. A sensor design embodying the invention is shown in Fig. 20 1. A sensor is shown generally at 10 comprises a wide band semiconductor e.g. ITO, 12 and a metal, e.g. Pt, compensation circuit 14, deposited on a substrate S. For purposes of generating experimental data, there are four Pt bond pads 16a, 16b, 16c and 16c. This self-compensated sensor 10 can be simulated as a circuit composed of resistors as shown in Fig. 2. Chl can measure the resistance of whole sensor, Ch2 is used 25 to measure resistance of the Pt, Ch4 is for ITO part, Ch3 and Ch5 are for contact resistance between Pt and ITO. Indium tin oxide (ITO) films were developed by rf reactive sputtering at low temperature using an MRC model 822 sputtering system. A high density target (12.7 cm in diameter) with a nominal composition of 90 wt% I203 and 10 wt% SnO 2 was 30 used for all depositions. Oxygen partial pressure was 30% while an rf power density of 2.4.W/cm 2 and a total pressure of 9 mtorr was mainatined during each sputtering run. Aluminum oxide constant strain beams were cut from rectangular plates (Coors PCTUS00/11334 WO 02/35178 5 Ceramics - 99.9% pure) using a laser cutting technique. The constant strain beams were then sputter-coated with 4 pm of high purity alumina prior to the deposition of the fTO strain gages. After spin casing 4 pm of ITO, a 2 pm thick layer of positive photoresiSt was spinoated onto the ITO film coating. After exposure and 5 development, the ITO films were etched in concentrated hydrochloric acid to delineate the final device structure. Sputtered platinum films (1.1 pm thick) were used to form ohmic contacts to the active ITO strain elements. Thic co tensions set forth above for the sensors were for experimental purposes to e eno and the mathematical model. One skilled in the art will recognize to prove the concept an h ahmtclto the teachings of the 10 that the dimensions of a commercially viable sensor according invention can be made at least an order of magnitude smaller using the current state-of the-art microelectronic fabrication techniques. wide band Referring to Fig. 3, a sensor 20 is shown and comprises a semiconductor 22 and a metal compensatig circuit 24 on a substrate S. In this design, 15 the G(-) of the semiconductor is maximize and the G(+) of the metal is minimized. Also shown are metal bond pads 26a and 26b. When the sensor is re , shown) connects to the bond pads 26. High Tem'erature _Strain Ri SighTrainturetinn ereg a cantilever bending fixutre fabricated out Strain measurements were made using a oi lmn o a once 20 of a machinable zirconium phosphate ceramic. A sli able differential transducer between an alumina constant strain beam and a linear vari reitan ce (LVDT) to measure deflection of the strain beam. Corresponding resistance changes were monitored using a four wire method with a 6 and 1/2 digit Hewlett Packard multimeter and a Keithley constant current source. The high accuracy LVDT, 25 multimeter and constant current source were interface to an u/s board and an IBM PC employing an IEEE 488 interface. Lab Windows software was used for data acquisition. pih ereature Strain TesReut t Te ste properties of the active ITO strain gage used over To evaluate e piezoresistive port o acterize the variation in electrical 30 a wide temperature range, itisimotnt ca PCT/US00/11334 WO 02/35178 6 response with temperature. The electrical response of an ITO fim grown in a 30% 02 plasma as disclosed above and thermally cycled in air at temperatures up to 1200'C was observed. exhibit a Broad band semiconductors over a defined temperature range may exhbi a
.
single TCR or two or more TCRs. It will be understood that if two linear TCRS are exhibited in two distinct temperature ranges within the defied temperature range that a sensor will be fabricated based on each distinct temperature range in order that the strain can be measured over the defined temperature range. It is known for ITO films that there can be two distinct TCRs depending upon 10 temperature. T > 8000, a linear response with a TCR of -210 ppm/*C has been observed and that T > 800 0 C, a TCR of -2170 ppmIC has been observed. More recently, an ITO with a single TCR of -300 to -1,500 ppm/ 0 C has been measured. Example In the example, a four-wire method was used connecting to the bond pads 16. 15 This method is well known to one skilled in the art. The sensor was fabricated and tested as outlined in the sections above. Four cycles of heating and Cooling were measured, the results are shown below and in Fig. 4. After the first heating, the resistance changing with temperature is almost identical in four cycles, thus it shows the reproducibility is good. Table 1 20Temperature Resistance Of distance of Resistance of Resistance of Resstance Of
(
0 C) Chl (0) Ch2 (Q) Ch3 (0) Gh4 (0) Ch5 (0) 1200 437 379 5 40 12 30 442 160 26 225 TC iip oiRcOW', )' o * AT)= (437-442/(437*1170)= -9.8 (ppm/*C) TCRpt= (Rts-Rt,o)/ (R o * AT)= (379-160)/(160*1170)= +1169 (ppm/*C) TCRrro =(Rrro - Rro~o)/ (Rrroo * AT) = (40-225)/(225* 1170) =-702 (ppm/*C) Resistivity of Pt 25 At 30 C, Pt =R .o*(w * t)/L =160* (0.6 rm*0.Sx10- 3 )/500 =l.535xl0' (Q*m) WO 02/35178 PCT/USOO/11334 7 At 1200 *C, prf = Rptg*(w * t)/L = 379*(0.6*0.8x10 3 )/500 = 3.639x10 4 (Q*m) Resistivity of ITO At 30C, 5 prrO = Rrroo*(w * t)/L=225*(5*4.4x10 3 )/60 = 8.25x10a (Q*m) At 1200 "C, prTof= Rrro,*(w * t)/L = 40*(5*4.4x104 3 )/60 = 1.498x10 2 (Q*m) from eq.(6) TCRcoMP = (Appt * Apt + AprTo * ArTO) / ((pPto * Apt + prro,o * Arro) * AT) (6) 10 Where Appt = prig - PPto= * ( 3
.
63 9 -1.
53 5 )*(104(Q*mm) Aprro= PITo,f - PITo,O = * (1.498=8.25)* 10 (n*mm) Art = Lpt/ (wpt * tpt) = 500/(0.6*0.8x10 3 ) (mml) ArTo = LiTo / (wrro * trro) =75/(5mm*4.4x10 3 ) (mi) 15 TCRcomp = (ApPt * Apt + Aprro * ArTo) / ((ppto * Apt + pnoo * Arro) * AT)= -21.32 (ppm/ 0 C) From equation (11) TCRCOMP = (TCRpt*Rpt,o+TCRrro*Rrroo)/(Rto +RTo,o) TCRCOMp = -23.5 (ppm/"C) 20 The results of the self-compensated sensor are presented below. This sensor was thermally cycled to 1200 *C. The experimental data shows that the TCR of self compensated gage was almost zero (0 ppm/*C 20 ppm/C) over the temperature range RT-1200"C.
WO 02/35178 PCT/US00/11334 8 Cycle2 Cycle3 Cycle4 Cycle5 (30"C -1200 0 C) (30*C -1200 0 C) (30*C -1200 0 C) (30"C -1200 0 C) TCR of Pt resistor 1206.6 1179.8 1183.5 1171.4 TCR of ITO resistor -701.3 -688.4 -705.6 -699.5 TCR of self- -17.0 -24.1 -17.1 -10.8 compensated gage Calculated TCR -27.5 -16.8 -28.6 -21.4 from eq. (6) Calculated TCR -29.0 -11.8 -30.5 -23.5 from eq. (11) The dimensions of the platinum resistor 14 were (0.6mm x 500mm x 0.8 pm thick) and the dimensions of the ITO sensor 12 placed in series with the platinum resistor were (5mm x 60 mm x 4.4 ptm thick). These dimensions correspond to the (width x length x thickness) of each resistor and the results in the table were obtained for these particular 5 dimensions. The room temperature resistances can be read from Fig. 4, approximately 240 ohms for the ITO resistor and 160 ohms for the platinum resistor. The use of self-compensating resistors can be used in any electrical device which requires control of a TCR as a function of temperature, i.e. thermistors, temperature 10 sensors, RTD's, etc. The foregoing description has been limited to a specific embodiment of the invention. It will be apparent, however, that variations and modifications can be made to the invention, with the attainment of some or all of the advantages of the invention. Therefore, it is the object of the appended claims to cover all such variations and 15 modifications as come within the true spirit and scope of the invention. Having described my invention, what I now claim is:
AU44962/00A 1999-04-29 2000-04-27 Self-compensated ceramic strain gage for use at high temperatures Abandoned AU4496200A (en)

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US13158499P 1999-04-29 1999-04-29
US60131584 1999-04-29
PCT/US2000/011334 WO2002035178A1 (en) 1999-04-29 2000-04-27 Self-compensated ceramic strain gage for use at high temperatures

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GB201012656D0 (en) * 2010-07-28 2010-09-15 Eosemi Ltd Compensation for stress induced resistance variations
JP5900883B2 (en) * 2012-01-25 2016-04-06 国立研究開発法人物質・材料研究機構 Device using single crystal tin oxide wire
CN103900460A (en) * 2012-12-28 2014-07-02 华东理工大学 Semiconductor film high-temperature deformation sensor
JP6119703B2 (en) 2014-09-04 2017-04-26 横河電機株式会社 Sensor device, strain sensor device, and pressure sensor device
CN104864840A (en) * 2015-06-14 2015-08-26 安徽圣力达电器有限公司 Novel embedded strain meter
CN105755438B (en) * 2016-03-30 2018-12-18 上海交通大学 A kind of high-temperature self-compensating multi-layer compound film strain gauge and preparation method thereof

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US4217785A (en) * 1979-01-08 1980-08-19 Bofors America, Inc. Erasable-foil-resistance compensation of strain gage transducers
US4299130A (en) * 1979-10-22 1981-11-10 Gould Inc. Thin film strain gage apparatus with unstrained temperature compensation resistances
US4325048A (en) * 1980-02-29 1982-04-13 Gould Inc. Deformable flexure element for strain gage transducer and method of manufacture
DE3176209D1 (en) * 1980-11-29 1987-06-25 Tokyo Electric Co Ltd Load cell and method of manufacturing the same
JPS59217375A (en) * 1983-05-26 1984-12-07 Toyota Central Res & Dev Lab Inc Semiconductor mechanic-electric conversion device
US5375474A (en) * 1992-08-12 1994-12-27 The United States Of America As Represented By The United States National Aeronautics And Space Administration Compensated high temperature strain gage
DE19703359A1 (en) * 1997-01-30 1998-08-06 Telefunken Microelectron Process for temperature compensation in measuring systems

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CA2391164A1 (en) 2002-05-02
JP2004512515A (en) 2004-04-22

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