US3918019A - Miniature absolute pressure transducer assembly and method - Google Patents

Miniature absolute pressure transducer assembly and method Download PDF

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US3918019A
US3918019A US449900A US44990074A US3918019A US 3918019 A US3918019 A US 3918019A US 449900 A US449900 A US 449900A US 44990074 A US44990074 A US 44990074A US 3918019 A US3918019 A US 3918019A
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diaphragm
conducting
pressure
bridge circuit
silicon
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Timothy A Nunn
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Leland Stanford Junior University
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L9/00Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means
    • G01L9/0041Transmitting or indicating the displacement of flexible diaphragms
    • G01L9/0051Transmitting or indicating the displacement of flexible diaphragms using variations in ohmic resistance
    • G01L9/0052Transmitting or indicating the displacement of flexible diaphragms using variations in ohmic resistance of piezoresistive elements
    • G01L9/0054Transmitting or indicating the displacement of flexible diaphragms using variations in ohmic resistance of piezoresistive elements integral with a semiconducting diaphragm

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  • the glass substrate has a circular well formed therein having a diameter at least as large as the diameter of the diaphragm.
  • Conducting leads are deposited on the glass substrate in a pattern matching that of the bonding pads on the silicon.
  • the silicon is bonded to the glass substrate with the silicon diaphragm overlying the well in the glass and the bonding pads overlying the conducting leads deposited on the glass.
  • the bond provides a hermetic seal around the well, trapping a prdetermined pressure therein which serves as a reference pressure. Ambient pressure variations cause stress variation in the diaphragm, resulting in unbalance of the bridge which can be sensed with associated circuits to give an indication of the ambient pressure.
  • FIG-6 MINIATURE AissoLUTE PRESSURE TRANSDUCER ASSEMBLY AND METHOD BACKGROUND OF' THE INVENTION
  • This invention relates generally to a transducer assembly for measuring absolute pressure and more particularly to a miniature pressure transducer assembly and method using a diaphragm as a stress magnifying device which acts as one wall of a sealed pressure
  • the need to obtain reliable pressure measurements in biological systems have been increasingly felt because of rapid advances in the biomedical field.
  • the cardiovascular system, the cerebro-spinal system, the gastrointestinal system, and the bladder are but a few of the places in the human body where pressure readings are often required.
  • Detailed pressure recordings from the cardiovascular system are the most important, since, in combination with an ECG, they provide accurate diagnosis of the condition of the heart.
  • the most common techniques for measuring intra-arterial blood pressure utilizes a flexible stainless steel guide wire about 1 mm in diameter which is inserted into the artery. This guide wire is pushed to the location where pressure is to be measured, while its "progress is monitored using a fluoroscope. A hollow catheter which envelopes the guide wire is then inserted and pushed to follow the guide wire to the desired location. After next removing the guide wire and filling the catheter with a suitable fluid, the in vivo pressure can be measured by placing a pressure transducer at the end of the liquid-filled catheter, outside the biological system. This method has inherent limitations due to the long path that the pressure wave has to travel to reach the pressure sensor. The recorded pressure wave is a function of the propagation characteristics of the hollow catheter and can depart appreciably from the true in vivo pressure.
  • a pressure sensor could be inserted into the ca theter to replace'the guide wire; however, due tothe scarcity of pressure sensors with an outer diameter equal to or less than that of conventional guide .wires, this method is rarely followed.
  • a bridge circuit is provided on the diaphragm which is electrically connected to externally accessible conducting leads on the substrate.
  • a predetermined reference pressure is trapped in the chamber during bonding, and the stress, imposed in the diaphragm by ambient pressure as indicated by the state of the bridge balance is indicative of the ambient pressure.
  • Another object of the present invention is to provide an absolute pressure transducer assembly providing external connections which do not impose physical stress on the pressure sensitive member.
  • Another object of the present invention is to provide an absolute pressure transducer assembly which may have any desired reference pressure.
  • Another object of the present invention is to provide an absolute pressure transducer assembly using simple easily controlled steps in the fabrication of the component parts, and in which the number of component parts are maintained at a minimum.
  • Another object of the present invention is to provide an absolute pressure transducer which is miniaturized using integrated circuit techniques.
  • FIG. 1 is a side elevational view of a semiconductor diaphragm assembly having a predetermined diaphragm thickness.
  • FIG. 2 is a bottom plan view of the semiconductor diaphragm assembly of FIG. 1.
  • FIG. 3. is a top plan view showing an integrated bridge circuit formed on the semiconductor diaphragm assembly of FIG. 1.
  • FIG. 4 is a plan view of an insulator substrate.
  • FIG. 5 is an assembly plan view of an absolute pressure transducer assembly.
  • FIG. 6 is a sectional view along the 5.
  • a practical structure for a miniature pressure transducer which could be used for converting blood pressure of a biological system into an electrical signal is obtained by combining a silicon diaphragm, which serves as a stress magnifying device, with diffused piezoresistors for sensing the pressure-induced stresses in line 66 of FIG.
  • the diaphragm the diaphragm.
  • the piezoresistive effect is observable at low stress levels and is the result of the change in carrier mobility with stress. Combined with the advanced state of silicon processing technology developed for making integratec circuits, this effect makes silicon a desirable material for miniature pressure transducers.
  • FIGS. 1, 2 and 3 show one form of a semiconductor V Diaphragm 16 is an essential silicon wafer having faces 12 and 13 as. shown in FIG. I
  • Faces l2 and 13 are oriented in the (100) crystallographic'pl'ane.
  • An anisotropic etching technique is used for the formation of the diaphragms.
  • This technique makes possi-' ble a novel thickness monitoring scheme which acts also as a chip separation etch.
  • Sensors with diaphragm diameters of 0.5 mm and thicknesses of only u m, sur-- rounded by' a 0.15 mm wide ring 'of thick silicon, have been batch fabricated using this technique.
  • An intrinsic sensitivity of 14 #volt per volt supply per mml-lg has been achieved.
  • the slot has apredet'ermined width and when the silicon body is exposed to the anisotropic etchant the etch proceeds through theslot in the etch resistant layer until a V shaped groove is formed:';
  • the sides of the V shaped groove correspond to the (111) crystallographic plane.
  • the slot width is approximately the square root of 2 times the depth of the groove. By appropriately selecting the slot width, the depth of the V groove is selected.
  • One side of the V groove is seen at 14 in FIG. 1 and the surface 14 correspondsto. the (111) crystallographic plane as mentioned above.
  • anyconvena tional process such as photolithography
  • etching continues from face 13 toward the bottom of the V groove, one side of which is formed by surface 14.
  • a visual indication of the interception of the V groove bottom by theletchant proceeding from face 13 is provided when the silicon body separates from the surrounding portions of the silicon wafer following which the etch is quenched.
  • the thickness of the silicon from areas: 16 and 16 to face '12 is therefore at the predetermined thickness rep ⁇ resented by the height of the V groove.
  • the reinforcing raphy, the gold andchromium layers are selectively:
  • the piezoresistive bridge circuit shown generally at 17 is formed on surface 12 opposite area 16 as seen in FIGS. 3 and 5.
  • the starting material used for the fabri cation of the silicon diaphragm assembly 11 is n-type, 50 to ,um thick, -oriented silicon wafers. Generally the starting material has one side of the wafer polished and both sides covered with silicon dioxide.
  • The. first processing step involves the stripping of the original oxide of the wafers and regrowing it at a temperature of 1100C. to a thickness of 7000A.
  • This oxide is used as a mask for the resistor and substrate contactdiffusions and also as a mask during the diaphragm etching step.
  • alignment marks are photoengraved on both sides of the wafer using a special jig, and succeeding masks are then aligned with respect'to these marks.
  • the alignment marks are aligned with flats on the wafer derived by cleaving the wafer along the crystallographic directions.
  • the p-r'esistors :15 are diffused according to a standard base diffusion schedule, resulting in a sheet resistivity of close to l00ohms per square.
  • This schedule yields resistors 1'5 with a high piezoresistive coefficient and should also make possible the incorporation of on-chip signal processing at a later state in sensor development.
  • Conducting paths 18 are formed using a starid f emitter diffusion schedule.
  • chromium isthen evaporated over the entire wafer to a thickness of approximately 50A.
  • a layer of gold approximately 1500A thick is then evaporated on top. of the chromium layer. Again using photolithogetched away leaving] the contact or bonding pads 19.
  • the wafers, are now ready for the diaphragm etching step previously described.
  • an insulating substrate 21 is shown having formed therein a well 22 with a diameter equal to or larger than the diameter of diaphragm 16.
  • Circular area 16' thus provides structural support for circular area l6' a'nd defines the boundaries of circular area 16'.
  • Circular area 16' will hereinafter be referred to as diaphragm l6.
  • v part of the' pressure transducer.
  • Thestress magnification" properties of 'a clamped circular diaphragm are proportionabto the square of the ratio of the diaphragm radius to its thickness. Diaphragm thickness'of. about 5pm are required for obtaining reasonable sensivities with pressure sea sors having diaphragm diameters of about 0.5..mm..-.
  • One method of obtaining the finished insulating substrate 21 involves depositby evaporation of a thin layer of chromium, approximately 50 arigstroms, onto a glass substrate A top layer of goldiis' evaporateddirectly ontofthe chromium. Aphotolitho'graphy is then per formedfor removing a small .circle of the chromium 22. The exposed glass substrate is then etched to a depth of approximately 100 pm. A subsequent photolithograph'y, removes all of the remaining chromium-gold layer except. that providing the conducting leads23.
  • Diaphragm assembly 11 is then placed adjacent to the surface on the insulating substrate 21 upon which the conducting leads 23 1 are formed.
  • Diaphragm assembly '11 is oriented so that the center of diaphragm 16' overlies the center of well-22, andthe b'ondingpads 19 each overlie a portion of one of the spacedconducting leads 23.
  • FIG, 6 shows the diaphragm assembly 11'and the insulator substrate 21 in position as described above. I
  • the final step is the bonding of the silicon diaphragm assembly 11' containing the integrated circuit to the insulator substrate 21.
  • Diaphragm assembly 11 maybe bonded to the insulator substrate 21 using ananodic bonding process.
  • the insulator substrate 21 is a glass materialand is referred to as a glass cap in this embodiment.
  • the insulating subatra'te 21 may be a thin silicon wafer with glass sputtered onto one surface so that" the anodic bonding processmay 'be utilized.
  • the bonding process involves placing the surface of glass cap 21, in which well 22 is formed, in intimate layer contact with surface 12 of silicon diaphragm assembly while properly oriented as shown FIG. 6.
  • the diaphragm assemblyll and glass cap '21 are heated to about 300C.
  • a heater 24 This temperature is well below the softening point of the glass cap 21 and the melting point of the silicon diaphragm assembly 1 1.
  • the heated glass cap 21 is slightly conductive.
  • An electrical potential of several hundred volts, sufficient to cause a low density current to flow, is applied across the diaphragm assembly 11 and the glass cap 2l with the silicon diaphragm assembly 11 attached to the anode or positive side of the potential source.
  • An anodically grown bond forming a hermetic seal is created between the diaphragm assembly 11 and the glass cap 21.
  • the method of bonding disclosed in U.S. Pat. No. 3,397,278 has been used for obtaining the bond and seal between diaphragm 11 and glass cap 21.
  • the gold pads 19 connected to the integrated circuit 17 are also bonded to the conducting paths 23 on glass cap 21 during the process in the fashion of a thermocompression bond.
  • diaphragm 11 and glass 21 r to urge them together to effect the bond.
  • the electrical potential provides an attracting force creating high pressure at the surface interface.
  • FIG. 5 is a view looking through the glass insulating substrate 21.
  • a hermetically sealed chamber 26 is formed defined by the silicon diaphragm 16' and the well 22 in substrate 21. Pressure may be adjusted in chamber 26 during the sealing process to provide any desired reference pressure therein. In this fashion a versatile absolute pressure transducer is provided having any desired predetermined pressure reference. External attachment of leads is easily accomplished by connection to the accessible areas of conducting leads 23 on substrate 21. This protects the delicate silicon diaphragm assembly 11 from breakage during external lead attachment.
  • the method for forming an absolute pressure transducer includes etching a well 22 in a glass substrate 21 and forming conducting leads 23 on the surface containing the well 22.
  • the method also includes forming a thin silicon diaphragm assembly 11 with a piezoresistive bridge circuit 17 formed thereon including conducting paths 18 and bonding pads 19.
  • Diaphragm assembly 11 is placed overlying the well 22 and bonded in place with the bonding pads 19 in electrical contact with conducting paths 23.
  • Hermetic sealing is obtained in the bonding process which may be anodic bonding. Adjusting a desired reference pressure in a hermetically sealed chamber 26 is obtained during the bonding step in the method.
  • Anextremely small absolute pressure transducer assembly which in one embodiment utilized a glass substrate of sufficient thickness to accept a 100p.m deep well, and which had a length of 2mm and a width of 1.5mm.
  • the silicon diaphragm assembly 11 was formed of a silicon chiphaving a thickness of from 50 to lOOum and the etching process produced a diaphragm thickness as low as 5pm. 7
  • the piezoresistor-bridge 17 when excited with a voltage provides an unbalance voltage which is a function of applied pressure on the diaphragm 16.
  • Silicon diaphragm assemblies having a 0.5 mm disphragm diameter have been made.
  • the diaphragm thickness was 7,um.
  • a pressure transducer haVing 'OLSmm diaphragm diameter and 7pm diaphragm thickness has provided pressure sensivity of 14p. volts per volt supply per -mm Hg. Higher sensitivities are gained with either thinner diaphragms or larger diameter diaphragms.-
  • the high sensitivity realized permits pressure variations as small as 1 mmHg to be resolved with the 0.5mm diameter. Even'with thesethin diaphragms, the pressure sensitivities of ,all sensors relized from a processing run are usually within l5 percent of the average value, with the variations attributed to small differences in diaphragm thickness from sensor to sensor. No changes in sensitivity due to repeated diaphragm flexing have been observed.
  • the piezoresistive coeficient of the diffused p-type resistors for known value of sheet resistivity may be calculated. Substituting the known values into the following equation:
  • the frequency response to these transducers is more than adequate for biomedical applications. Although detailed frequency measurements have not been made above 10 kHz, the first calculated diaphragm resonance is at about 60 kHz for the 1.2mm diaphragm and is considerably higher for the smaller sensor.
  • sensors after being mounted on the tip of a small catheter, may be inserted into the biological system through the inner bore of a larger catheter which was formerly occupied by a guide wire.
  • the sensor disclosed herein having its own contained reference pressure cavity, does not require a clear passage to ambient pressure to make in vivo measurements.
  • An absolute pressure transducer comprising a semiconductor diaphragm, an integral reinforcing area surrounding and defining the boundaries of said diaphragm, means forming a bridge circuit on said diaphragm, said last named means having electrical characteristics related to stress in said diaphragm, conducting pads formed on said reinforcing area in a predetermined pattern, conducting paths connected between oul 1 uumlu said means forming a bridge circuit and said conducting pads, an insulator substrate having a well formed therein with a diametral dimension at least as great as said diaphragm diametral dimension, and conducting leads formed on said insulator substrate spaced thereon to match said predetermined pattern of conducting pads, said substrate and reinforcing area being bonded together with the center of said diaphragm substantially overlying the center of said well for providing a hermetically sealed chamber therebetween, whereby said means forming a bridge circuit is enclosed in said hermetically sealed chamber for protection from ambient environments, said predetermined pattern of conducting pads substantially overlying and
  • a transducer for absolute pressure measurement comprising a semiconductor integrated circuit pressure transducer having a diaphragm section with a piezoresistive bridge circuit formed thereon, an insulator substrate having a well formed therein, conducting leads deposited on said insulator substrate having externally accessible portions, said semiconductor integrated circuit pressure transducer being bonded to said insulator substrate with said diaphragm section overlying said well thereby forming a hermetically sealed chamber therebetween, said piezoresistive bridge circuit being enclosed in said sealed chamber for protection from ambient environment and being in electrical contact with said conductive leads on said insulating substrate, whereby said piezoresistive bridge circuit may be unbalanced by stress imposed in said diaphragm by pressure differential across said diaphragm.

Abstract

A transducer assembly for measuring absolute pressure utilizing a glass substrate and a thin silicon diaphragm upon which is diffused a piezoresistive bridge circuit. Bridge circuit components are properly oriented and connected to bonding pads formed on the silicon. The glass substrate has a circular well formed therein having a diameter at least as large as the diameter of the diaphragm. Conducting leads are deposited on the glass substrate in a pattern matching that of the bonding pads on the silicon. The silicon is bonded to the glass substrate with the silicon diaphragm overlying the well in the glass and the bonding pads overlying the conducting leads deposited on the glass. The bond provides a hermetic seal around the well, trapping a prdetermined pressure therein which serves as a reference pressure. Ambient pressure variations cause stress variation in the diaphragm, resulting in unbalance of the bridge which can be sensed with associated circuits to give an indication of the ambient pressure.

Description

United States Patent [191 Nunn Nov. 4, 1975 [75] Inventor: Timothy A. Nunn, Stanford, Calif.
[73] Assignee: The Board of Trustees of the Leland Stanford Junior University, Stanford, Calif.
22 Filed: Mar. 11, 1974 [21] Appl. No.: 449,900
52 US. Cl. 338/42; 73/885 so; 338/2; 338/36 [51] Int. Cl. H01C 13/00 {58] Field of Search 338/2-5, 36, 338/42; 73/885 SD, 88.5 R, 398 AR; 29/626, 628
[56] References Cited UNITED STATES PATENTS 3,417,361 12/1968 Heller et a1. I 3,697,918 10/1972 Orth 3,774,834 ll/1973 Holler... 3,800,264 3/1974 Kurtz 338/3 X 3,820,401 6/1974 Lewis 73/398 AR Primary ExaminerC. L. Albritton Attorney, Agent, or FirmFlehr, Hohbach, Test, Albritton & Herbert [57] ABSTRACT A transducer assembly for measuring absolute pressure utilizing a glass substrate and a thin silicon diaphragm upon which is diffused a piezoresistive bridge circuit. Bridge circuit components are properly oriented and connected to bonding pads formed on the silicon. The glass substrate has a circular well formed therein having a diameter at least as large as the diameter of the diaphragm. Conducting leads are deposited on the glass substrate in a pattern matching that of the bonding pads on the silicon. The silicon is bonded to the glass substrate with the silicon diaphragm overlying the well in the glass and the bonding pads overlying the conducting leads deposited on the glass. The bond provides a hermetic seal around the well, trapping a prdetermined pressure therein which serves as a reference pressure. Ambient pressure variations cause stress variation in the diaphragm, resulting in unbalance of the bridge which can be sensed with associated circuits to give an indication of the ambient pressure.
5 Claims, 6 Drawing Figures US. Patent N0v.4,1975 sheet 1 on 3,918,019
U.S. Patent No\ /.4, 1975 Sheet2 0f2 3,918,019
F l G.-4
FIG-6 MINIATURE AissoLUTE PRESSURE TRANSDUCER ASSEMBLY AND METHOD BACKGROUND OF' THE INVENTION This invention relates generally to a transducer assembly for measuring absolute pressure and more particularly to a miniature pressure transducer assembly and method using a diaphragm as a stress magnifying device which acts as one wall of a sealed pressure The need to obtain reliable pressure measurements in biological systems have been increasingly felt because of rapid advances in the biomedical field. The cardiovascular system, the cerebro-spinal system, the gastrointestinal system, and the bladder are but a few of the places in the human body where pressure readings are often required. Detailed pressure recordings from the cardiovascular system are the most important, since, in combination with an ECG, they provide accurate diagnosis of the condition of the heart.
v At present, the most common techniques for measuring intra-arterial blood pressure utilizes a flexible stainless steel guide wire about 1 mm in diameter which is inserted into the artery. This guide wire is pushed to the location where pressure is to be measured, while its "progress is monitored using a fluoroscope. A hollow catheter which envelopes the guide wire is then inserted and pushed to follow the guide wire to the desired location. After next removing the guide wire and filling the catheter with a suitable fluid, the in vivo pressure can be measured by placing a pressure transducer at the end of the liquid-filled catheter, outside the biological system. This method has inherent limitations due to the long path that the pressure wave has to travel to reach the pressure sensor. The recorded pressure wave is a function of the propagation characteristics of the hollow catheter and can depart appreciably from the true in vivo pressure.
Ideally, to avoid this propagation distortion, a pressure sensor could be inserted into the ca theter to replace'the guide wire; however, due tothe scarcity of pressure sensors with an outer diameter equal to or less than that of conventional guide .wires, this method is rarely followed. I
A need exists for pressure transducers having selfcontained reference pressure and very small physical size, which may be obtained through the use of semi- 2 sealed chamber is formed with the diaphragm serving as'one wall of the chamber. A bridge circuit is provided on the diaphragm which is electrically connected to externally accessible conducting leads on the substrate. A predetermined reference pressure is trapped in the chamber during bonding, and the stress, imposed in the diaphragm by ambient pressure as indicated by the state of the bridge balance is indicative of the ambient pressure.
In general, it is an object of the present invention to provide an absolute pressure transducer assembly using assembly structure and methods affording extremely small physical size.
Another object of the present invention is to provide an absolute pressure transducer assembly providing external connections which do not impose physical stress on the pressure sensitive member.
Another object of the present invention is to provide an absolute pressure transducer assembly which may have any desired reference pressure.
Another object of the present invention is to provide an absolute pressure transducer assembly using simple easily controlled steps in the fabrication of the component parts, and in which the number of component parts are maintained at a minimum.
Another object of the present invention is to provide an absolute pressure transducer which is miniaturized using integrated circuit techniques.
Additional objects and features of the invention will appear from the following description in which the preferred embodiment has been set forth in detail in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a side elevational view of a semiconductor diaphragm assembly having a predetermined diaphragm thickness.
FIG. 2 is a bottom plan view of the semiconductor diaphragm assembly of FIG. 1.
conductor materials and integrated circuit processes for providing greater efficiency in the use of available volumes for a-p'ressure transducer.
SUMMARY AND OBJECTS or TIA-IE I ENTIO An absolute pressure transducer has a semiconductor diaphragm which is bonded to an insulator substrate overlying a well formed in the substrate. A hermetically FIG. 3.is a top plan view showing an integrated bridge circuit formed on the semiconductor diaphragm assembly of FIG. 1.
FIG. 4 is a plan view of an insulator substrate.
FIG. 5 is an assembly plan view of an absolute pressure transducer assembly.
FIG. 6 is a sectional view along the 5.
I BRIEF DESCRIPTION OF THE PREFERRED EMBODIMENT A practical structure for a miniature pressure transducerwhich could be used for converting blood pressure of a biological system into an electrical signal is obtained by combining a silicon diaphragm, which serves as a stress magnifying device, with diffused piezoresistors for sensing the pressure-induced stresses in line 66 of FIG.
,the diaphragm. The piezoresistive effect is observable at low stress levels and is the result of the change in carrier mobility with stress. Combined with the advanced state of silicon processing technology developed for making integratec circuits, this effect makes silicon a desirable material for miniature pressure transducers.
FIGS. 1, 2 and 3 show one form of a semiconductor V Diaphragm 16 is an essential silicon wafer having faces 12 and 13 as. shown in FIG. I
1. Faces l2 and 13 are oriented in the (100) crystallographic'pl'ane. I
An anisotropic etching technique is used for the formation of the diaphragms. This technique makes possi-' ble a novel thickness monitoring scheme which acts also asa chip separation etch. Sensors with diaphragm diameters of 0.5 mm and thicknesses of only u m, sur-- rounded by' a 0.15 mm wide ring 'of thick silicon, have been batch fabricated using this technique. An intrinsic sensitivity of 14 #volt per volt supply per mml-lg, has been achieved. I In the method for forming the silicon diaphragm as; sembly 11 a slot is formed in an etch resistantlayer applied to face 12. The slot has apredet'ermined width and when the silicon body is exposed to the anisotropic etchant the etch proceeds through theslot in the etch resistant layer until a V shaped groove is formed:'; The sides of the V shaped groove correspond to the (111) crystallographic plane. When the V groove is completed no (100) crystallographic surface is left ex posed 'to the anisotropic etchant, and the etching effectively stops from the side of the silicon bodyhaving face 12. Thus, the slot width'deterr'nines thefi'nal depth of the V groove. The slot width is approximately the square root of 2 times the depth of the groove. By appropriately selecting the slot width, the depth of the V groove is selected. One side of the V groove is seen at 14 in FIG. 1 and the surface 14 correspondsto. the (111) crystallographic plane as mentioned above.
Continuing the method disclosed in the referenced application an etch resistant layer-is alsoapplied tothe face 13 of the silicon diaphram assembly 11. Portions of the etch resistant layer are removed by anyconvena tional process, such as photolithography, exposing face 13 in areas 16 and 16'. When the silicon body is placed in an anisotropic etchant etching continues from face 13 toward the bottom of the V groove, one side of which is formed by surface 14. A visual indication of the interception of the V groove bottom by theletchant proceeding from face 13 is provided when the silicon body separates from the surrounding portions of the silicon wafer following which the etch is quenched. The thickness of the silicon from areas: 16 and 16 to face '12 is therefore at the predetermined thickness rep} resented by the height of the V groove.
The. remaining silicon material below surface 13 which was protected by the etch =resistant layer provides a reinforcing area surrounding the area l6 "which in this embodiment is circular in shape. The reinforcing raphy, the gold andchromium layers are selectively:
' I 4 cally opposite resistors'l5 inthe bridge 17 have the same sign of piezoresistivity, which is opposite to that of the remaining two resistors. After analyzing the stress patterns of the diaphragm and the orientation dependenceof the piezoresistivity, the change in bridge unbalancedue'to an applied pressure can be maximized. a l
The piezoresistive bridge circuit shown generally at 17 is formed on surface 12 opposite area 16 as seen in FIGS. 3 and 5. The starting material used for the fabri cation of the silicon diaphragm assembly 11 is n-type, 50 to ,um thick, -oriented silicon wafers. Generally the starting material has one side of the wafer polished and both sides covered with silicon dioxide.
The. first processing step involves the stripping of the original oxide of the wafers and regrowing it at a temperature of 1100C. to a thickness of 7000A. This oxide is used as a mask for the resistor and substrate contactdiffusions and also as a mask during the diaphragm etching step.
To facilitate the photolithography of related patterns on the front and backside 'of the wafer, alignment marks are photoengraved on both sides of the wafer using a special jig, and succeeding masks are then aligned with respect'to these marks. The alignment marks are aligned with flats on the wafer derived by cleaving the wafer along the crystallographic directions. a
To'make the fabrication as compatible as possible with standard bipolarint'egrated circuit processing,the p-r'esistors :15 are diffused according to a standard base diffusion schedule, resulting in a sheet resistivity of close to l00ohms per square. This schedule yields resistors 1'5 with a high piezoresistive coefficient and should also make possible the incorporation of on-chip signal processing at a later state in sensor development. Conducting paths 18 (doped P+) are formed using a starid f emitter diffusion schedule.
After opening the contact holes and removing the photor' esist, chromium isthen evaporated over the entire wafer to a thickness of approximately 50A. A layer of gold approximately 1500A thick is then evaporated on top. of the chromium layer. Again using photolithogetched away leaving] the contact or bonding pads 19. The wafers, are now ready for the diaphragm etching step previously described. a,
Referring to FIG. 4 an insulating substrate 21 is shown having formed therein a well 22 with a diameter equal to or larger than the diameter of diaphragm 16.
1 Also formed on the surface of insulating s bs'trate' 21,
area 13 thus provides structural support for circular area l6' a'nd defines the boundaries of circular area 16'. Circular area 16' will hereinafter be referred to as diaphragm l6. v part of the' pressure transducer. Thestress magnification" properties of 'a clamped circular diaphragm are proportionabto the square of the ratio of the diaphragm radius to its thickness. Diaphragm thickness'of. about 5pm are required for obtaining reasonable sensivities with pressure sea sors having diaphragm diameters of about 0.5..mm..-. The
5 gold layer corresponding in size to the diameterrof well supporting rim 13 of thick silicon 'is then necessary to facilitate the handling tures. a
The pressure-induced stresses on diaphragm 16" are and mounting of these strucf .r I I 65 sensed by four properly-oriented piezoresistors 15 interconnect ed to form a bridge circuit 17. Two diametrion the sarne surfaceas that in .which well 22 is formed, area plurality of conducting leads 23 having a spacing -matching the pattermof the bonding pads 19 ondiaphra g'rn assembly 11.
One method of obtaining the finished insulating substrate 21 involves depositby evaporation of a thin layer of chromium, approximately 50 arigstroms, onto a glass substrate A top layer of goldiis' evaporateddirectly ontofthe chromium. Aphotolitho'graphy is then per formedfor removing a small .circle of the chromium 22. The exposed glass substrate is then etched to a depth of approximately 100 pm. A subsequent photolithograph'y, removes all of the remaining chromium-gold layer except. that providing the conducting leads23.
Surface 12 on silicon diaphragm assembly 11 is then placed adjacent to the surface on the insulating substrate 21 upon which the conducting leads 23 1 are formed. Diaphragm assembly '11 is oriented so that the center of diaphragm 16' overlies the center of well-22, andthe b'ondingpads 19 each overlie a portion of one of the spacedconducting leads 23. FIG, 6 shows the diaphragm assembly 11'and the insulator substrate 21 in position as described above. I
The final step is the bonding of the silicon diaphragm assembly 11' containing the integrated circuit to the insulator substrate 21. Diaphragm assembly 11 maybe bonded to the insulator substrate 21 using ananodic bonding process. The insulator substrate 21 is a glass materialand is referred to as a glass cap in this embodiment. The insulating subatra'te 21 may be a thin silicon wafer with glass sputtered onto one surface so that" the anodic bonding processmay 'be utilized. The bonding process involves placing the surface of glass cap 21, in which well 22 is formed, in intimate layer contact with surface 12 of silicon diaphragm assembly while properly oriented as shown FIG. 6. The diaphragm assemblyll and glass cap '21 are heated to about 300C. by a heater 24. This temperature is well below the softening point of the glass cap 21 and the melting point of the silicon diaphragm assembly 1 1..The heated glass cap 21 is slightly conductive. An electrical potential of several hundred volts, sufficient to cause a low density current to flow, is applied across the diaphragm assembly 11 and the glass cap 2l with the silicon diaphragm assembly 11 attached to the anode or positive side of the potential source. An anodically grown bond forming a hermetic seal is created between the diaphragm assembly 11 and the glass cap 21. The method of bonding disclosed in U.S. Pat. No. 3,397,278 has been used for obtaining the bond and seal between diaphragm 11 and glass cap 21. The gold pads 19 connected to the integrated circuit 17 are also bonded to the conducting paths 23 on glass cap 21 during the process in the fashion of a thermocompression bond. No
external force is exerted on diaphragm 11 and glass 21 r to urge them together to effect the bond. The electrical potential provides an attracting force creating high pressure at the surface interface.
A finished assembly is shown in FIG. 5, which is a view looking through the glass insulating substrate 21. A hermetically sealed chamber 26 is formed defined by the silicon diaphragm 16' and the well 22 in substrate 21. Pressure may be adjusted in chamber 26 during the sealing process to provide any desired reference pressure therein. In this fashion a versatile absolute pressure transducer is provided having any desired predetermined pressure reference. External attachment of leads is easily accomplished by connection to the accessible areas of conducting leads 23 on substrate 21. This protects the delicate silicon diaphragm assembly 11 from breakage during external lead attachment.
The method for forming an absolute pressure transducer includes etching a well 22 in a glass substrate 21 and forming conducting leads 23 on the surface containing the well 22. The method also includes forming a thin silicon diaphragm assembly 11 with a piezoresistive bridge circuit 17 formed thereon including conducting paths 18 and bonding pads 19. Diaphragm assembly 11 is placed overlying the well 22 and bonded in place with the bonding pads 19 in electrical contact with conducting paths 23. Hermetic sealing is obtained in the bonding process which may be anodic bonding. Adjusting a desired reference pressure in a hermetically sealed chamber 26 is obtained during the bonding step in the method. t
. Anextremely small absolute pressure transducer assembly is provided which in one embodiment utilized a glass substrate of sufficient thickness to accept a 100p.m deep well, and which had a length of 2mm and a width of 1.5mm. The silicon diaphragm assembly 11 was formed of a silicon chiphaving a thickness of from 50 to lOOum and the etching process produced a diaphragm thickness as low as 5pm. 7
The piezoresistor-bridge 17 when excited with a voltage provides an unbalance voltage which is a function of applied pressure on the diaphragm 16. Silicon diaphragm assemblies having a 0.5 mm disphragm diameter have been made. The diaphragm thickness was 7,um. A pressure transducer haVing 'OLSmm diaphragm diameter and 7pm diaphragm thickness has provided pressure sensivity of 14p. volts per volt supply per -mm Hg. Higher sensitivities are gained with either thinner diaphragms or larger diameter diaphragms.-
The high sensitivity realized permits pressure variations as small as 1 mmHg to be resolved with the 0.5mm diameter. Even'with thesethin diaphragms, the pressure sensitivities of ,all sensors relized from a processing run are usually within l5 percent of the average value, with the variations attributed to small differences in diaphragm thickness from sensor to sensor. No changes in sensitivity due to repeated diaphragm flexing have been observed.
From the pressure sensitivity and the known values of diaphragm diameter and thickness, the piezoresistive coeficient of the diffused p-type resistors for known value of sheet resistivity may be calculated. Substituting the known values into the following equation:
and equating it with the measured sensitivities, we find the value of 11- X l0 cm dyne This value of 11- is in agreement with the published value for the resistivity used.
The frequency response to these transducers is more than adequate for biomedical applications. Although detailed frequency measurements have not been made above 10 kHz, the first calculated diaphragm resonance is at about 60 kHz for the 1.2mm diaphragm and is considerably higher for the smaller sensor.
These sensors, after being mounted on the tip of a small catheter, may be inserted into the biological system through the inner bore of a larger catheter which was formerly occupied by a guide wire. The sensor disclosed herein, having its own contained reference pressure cavity, does not require a clear passage to ambient pressure to make in vivo measurements.
I claim:
1. An absolute pressure transducer comprising a semiconductor diaphragm, an integral reinforcing area surrounding and defining the boundaries of said diaphragm, means forming a bridge circuit on said diaphragm, said last named means having electrical characteristics related to stress in said diaphragm, conducting pads formed on said reinforcing area in a predetermined pattern, conducting paths connected between oul 1 uumlu said means forming a bridge circuit and said conducting pads, an insulator substrate having a well formed therein with a diametral dimension at least as great as said diaphragm diametral dimension, and conducting leads formed on said insulator substrate spaced thereon to match said predetermined pattern of conducting pads, said substrate and reinforcing area being bonded together with the center of said diaphragm substantially overlying the center of said well for providing a hermetically sealed chamber therebetween, whereby said means forming a bridge circuit is enclosed in said hermetically sealed chamber for protection from ambient environments, said predetermined pattern of conducting pads substantially overlying and electrically conducting portions of said conducting leads, whereby pressure trapped in said sealed chamber provides a reference pressureand stress may be imposed in said diaphragm by ambient pressure.
2. An absolute pressure transducer as in claim 1 wherein said diaphragm is a thin silicon member, said means forming a bridge circuit is a piezoresistive integrated circuit bridge formed thereon, and said conducting paths are P+ diffusion areas.
3. An absolute pressure transducer as in claim 1 wherein said insulator substrate is glass and said conducting leads are electrically conductive strips deposited on the side of said glass in which said well is formed.
4. An absolute pressure transducer as in claim 1 wherein said insulator substrate has alarger area than said reinforcing area and said'conducting leads extend beyond the area overlain by said reinforcing, area, whereby said conducting paths are accessible formaking connection to said means forming a bridge,
5. A transducer for absolute pressure measurement comprising a semiconductor integrated circuit pressure transducer having a diaphragm section with a piezoresistive bridge circuit formed thereon, an insulator substrate having a well formed therein, conducting leads deposited on said insulator substrate having externally accessible portions, said semiconductor integrated circuit pressure transducer being bonded to said insulator substrate with said diaphragm section overlying said well thereby forming a hermetically sealed chamber therebetween, said piezoresistive bridge circuit being enclosed in said sealed chamber for protection from ambient environment and being in electrical contact with said conductive leads on said insulating substrate, whereby said piezoresistive bridge circuit may be unbalanced by stress imposed in said diaphragm by pressure differential across said diaphragm.

Claims (5)

1. An absolute pressure transducer comprising a semiconductor diaphragm, an integral reinforcing area surrounding and defining the boundaries of said diaphragm, means forming a bridge circuit on said diaphragm, said last named means having electrical characteristics related to stress in said diaphragm, conducting pads formed on said reinforcing area in a predetermined pattern, conducting paths connected between said means forming a bridge circuit and said conducting pads, an insulator substrate having a well formed therein with a diametral dimension at least as great as said diaphragm diametral dimension, and conducting leads formed on said insulator substrate spaced thereon to match said predetermined pattern of conducting pads, said substrate and reinforcing area being bonded together with the center of said diaphragm substantially overlying the center of said well for providing a hermetically sealed chamber therebetween, whereby said means forming a bridge circuit is enclosed in said hermetically sealed chamber for protection from ambient environments, said predetermined pattern of conducting pads substantially overlying and electrically conducting portions of said conducting leads, whereby pressure trapped in said sealed chamber provides a reference pressure and stress may be imposed in said diaphragm by ambient pressure.
2. An absolute pressure transducer as in claim 1 wherein said diaphragm is a thin silicon member, said means forming a bridge circuit is a piezoresistive integrated circuit bridge formed thereon, and said conducting paths are P+ diffusion areas.
3. An absolute pressure transducer as in claim 1 wherein said insulator substrate is glass and said conducting leads are electrically conductive strips deposited on the side of said glass in which said well is formed.
4. An absolute pressure transducer as in claim 1 wherein said insulator substrate has a larger area than said reinforcing area and said conducting leads extend beyond the area overlain by said reinforcing area, whereby saiD conducting paths are accessible for making connection to said means forming a bridge.
5. A transducer for absolute pressure measurement comprising a semiconductor integrated circuit pressure transducer having a diaphragm section with a piezoresistive bridge circuit formed thereon, an insulator substrate having a well formed therein, conducting leads deposited on said insulator substrate having externally accessible portions, said semiconductor integrated circuit pressure transducer being bonded to said insulator substrate with said diaphragm section overlying said well thereby forming a hermetically sealed chamber therebetween, said piezoresistive bridge circuit being enclosed in said sealed chamber for protection from ambient environment and being in electrical contact with said conductive leads on said insulating substrate, whereby said piezoresistive bridge circuit may be unbalanced by stress imposed in said diaphragm by pressure differential across said diaphragm.
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DE2913772A1 (en) * 1978-04-05 1979-10-18 Hitachi Ltd SEMI-CONDUCTOR PRESSURE CONVERTER
EP0010204A1 (en) * 1978-09-27 1980-04-30 Hitachi, Ltd. Semiconductor absolute pressure transducer assembly
US4203128A (en) * 1976-11-08 1980-05-13 Wisconsin Alumni Research Foundation Electrostatically deformable thin silicon membranes
US4234361A (en) * 1979-07-05 1980-11-18 Wisconsin Alumni Research Foundation Process for producing an electrostatically deformable thin silicon membranes utilizing a two-stage diffusion step to form an etchant resistant layer
US4246908A (en) * 1976-10-19 1981-01-27 Kabushiki Kaisha Toyota Kenkyusho Intracranial pressure transducer
WO1981003086A1 (en) * 1980-04-14 1981-10-29 Motorola Inc Silicon pressure sensor
US4303903A (en) * 1978-09-22 1981-12-01 Hitachi, Ltd. Pressure sensitive apparatus
US4322980A (en) * 1979-11-08 1982-04-06 Hitachi, Ltd. Semiconductor pressure sensor having plural pressure sensitive diaphragms and method
US4411158A (en) * 1981-04-14 1983-10-25 Ametek, Inc. Apparatus for sensing the condition of a fluid
US4416156A (en) * 1981-12-23 1983-11-22 Honeywell Inc. High pressure electrical feedthru
US4445385A (en) * 1982-04-30 1984-05-01 International Telephone & Telegraph Corporation Static pressure sensor with glass bonded strain gauge transducers
US4498070A (en) * 1983-06-30 1985-02-05 Lirman Irving R Semi-conductor transducer and method of making the same
US4522072A (en) * 1983-04-22 1985-06-11 Insouth Microsystems, Inc. Electromechanical transducer strain sensor arrangement and construction
US4545255A (en) * 1984-01-17 1985-10-08 Environmental Control Technology, Inc. Low pressure transducer
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US4685469A (en) * 1984-03-09 1987-08-11 Keller Hans W Piezoresistive pressure measuring cell
EP0250948A2 (en) * 1986-06-26 1988-01-07 Fraunhofer-Gesellschaft Zur Förderung Der Angewandten Forschung E.V. Microvalve
US4802952A (en) * 1987-03-06 1989-02-07 Hitachi, Ltd. Method for manufacturing semiconductor absolute pressure sensor units
US5012316A (en) * 1989-03-28 1991-04-30 Cardiac Pacemakers, Inc. Multiaxial transducer interconnection apparatus
DE4409068A1 (en) * 1994-03-14 1996-01-25 Mannesmann Ag Oxidised silicon layer to boron-silicate glass bonding method
US5507090A (en) * 1994-07-20 1996-04-16 Thiokol Corporation Method for making stress sensors
US5563634A (en) * 1993-07-14 1996-10-08 Seiko Epson Corporation Ink jet head drive apparatus and drive method, and a printer using these
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US5668579A (en) * 1993-06-16 1997-09-16 Seiko Epson Corporation Apparatus for and a method of driving an ink jet head having an electrostatic actuator
US5675310A (en) * 1994-12-05 1997-10-07 General Electric Company Thin film resistors on organic surfaces
US5818473A (en) * 1993-07-14 1998-10-06 Seiko Epson Corporation Drive method for an electrostatic ink jet head for eliminating residual charge in the diaphragm
US5821951A (en) * 1993-06-16 1998-10-13 Seiko Epson Corporation Ink jet printer having an electrostatic activator and its control method
US6198379B1 (en) * 1997-06-19 2001-03-06 Robert Bosch Gmbh Semiconductor component with piezoresistive measuring shunts
US20110193363A1 (en) * 2010-02-10 2011-08-11 Seiko Epson Corporation Stress sensing device, tactile sensor, and grasping apparatus
US20120234112A1 (en) * 2009-12-25 2012-09-20 Alps Electric Co., Ltd. Force sensor and method of manufacturing the same
RU2474007C1 (en) * 2011-09-08 2013-01-27 Федеральное Государственное Бюджетное Учреждение "Научно-Производственный Комплекс "Технологический Центр" Миэт" Design of sensitive element of pressure converter based on silicon-on-insulator structure
US9597480B2 (en) 2009-10-07 2017-03-21 Endophys Holding, LLC Intraluminal devices and systems
US10315013B2 (en) 2001-07-13 2019-06-11 Endophys Holdings, Llc Sheath with sensing capabilities

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Cited By (43)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4246908A (en) * 1976-10-19 1981-01-27 Kabushiki Kaisha Toyota Kenkyusho Intracranial pressure transducer
US4203128A (en) * 1976-11-08 1980-05-13 Wisconsin Alumni Research Foundation Electrostatically deformable thin silicon membranes
DE2913772A1 (en) * 1978-04-05 1979-10-18 Hitachi Ltd SEMI-CONDUCTOR PRESSURE CONVERTER
US4303903A (en) * 1978-09-22 1981-12-01 Hitachi, Ltd. Pressure sensitive apparatus
EP0010204A1 (en) * 1978-09-27 1980-04-30 Hitachi, Ltd. Semiconductor absolute pressure transducer assembly
US4291293A (en) * 1978-09-27 1981-09-22 Hitachi, Ltd. Semiconductor absolute pressure transducer assembly and method
US4234361A (en) * 1979-07-05 1980-11-18 Wisconsin Alumni Research Foundation Process for producing an electrostatically deformable thin silicon membranes utilizing a two-stage diffusion step to form an etchant resistant layer
US4322980A (en) * 1979-11-08 1982-04-06 Hitachi, Ltd. Semiconductor pressure sensor having plural pressure sensitive diaphragms and method
US4317126A (en) * 1980-04-14 1982-02-23 Motorola, Inc. Silicon pressure sensor
WO1981003086A1 (en) * 1980-04-14 1981-10-29 Motorola Inc Silicon pressure sensor
US4411158A (en) * 1981-04-14 1983-10-25 Ametek, Inc. Apparatus for sensing the condition of a fluid
US4416156A (en) * 1981-12-23 1983-11-22 Honeywell Inc. High pressure electrical feedthru
US4445385A (en) * 1982-04-30 1984-05-01 International Telephone & Telegraph Corporation Static pressure sensor with glass bonded strain gauge transducers
US4522072A (en) * 1983-04-22 1985-06-11 Insouth Microsystems, Inc. Electromechanical transducer strain sensor arrangement and construction
US4498070A (en) * 1983-06-30 1985-02-05 Lirman Irving R Semi-conductor transducer and method of making the same
US4545255A (en) * 1984-01-17 1985-10-08 Environmental Control Technology, Inc. Low pressure transducer
US4685469A (en) * 1984-03-09 1987-08-11 Keller Hans W Piezoresistive pressure measuring cell
DE3436001A1 (en) * 1984-10-01 1986-04-03 Siemens AG, 1000 Berlin und 8000 München Electrostatic glass-soldering of semiconductor components
EP0250948A3 (en) * 1986-06-26 1989-05-10 Fraunhofer-Gesellschaft Zur Forderung Der Angewandten Forschung E.V. Microvalve
EP0250948A2 (en) * 1986-06-26 1988-01-07 Fraunhofer-Gesellschaft Zur Förderung Der Angewandten Forschung E.V. Microvalve
US4802952A (en) * 1987-03-06 1989-02-07 Hitachi, Ltd. Method for manufacturing semiconductor absolute pressure sensor units
US5012316A (en) * 1989-03-28 1991-04-30 Cardiac Pacemakers, Inc. Multiaxial transducer interconnection apparatus
US5668579A (en) * 1993-06-16 1997-09-16 Seiko Epson Corporation Apparatus for and a method of driving an ink jet head having an electrostatic actuator
US5975668A (en) * 1993-06-16 1999-11-02 Seiko Epson Corporation Ink jet printer and its control method for detecting a recording condition
US5821951A (en) * 1993-06-16 1998-10-13 Seiko Epson Corporation Ink jet printer having an electrostatic activator and its control method
US5563634A (en) * 1993-07-14 1996-10-08 Seiko Epson Corporation Ink jet head drive apparatus and drive method, and a printer using these
US5644341A (en) * 1993-07-14 1997-07-01 Seiko Epson Corporation Ink jet head drive apparatus and drive method, and a printer using these
US5818473A (en) * 1993-07-14 1998-10-06 Seiko Epson Corporation Drive method for an electrostatic ink jet head for eliminating residual charge in the diaphragm
DE4409068A1 (en) * 1994-03-14 1996-01-25 Mannesmann Ag Oxidised silicon layer to boron-silicate glass bonding method
DE4409068C2 (en) * 1994-03-14 1998-05-28 Hartmann & Braun Ag Bonding process and bond connection produced therewith
US5507090A (en) * 1994-07-20 1996-04-16 Thiokol Corporation Method for making stress sensors
US5849623A (en) * 1994-12-05 1998-12-15 General Electric Company Method of forming thin film resistors on organic surfaces
US5675310A (en) * 1994-12-05 1997-10-07 General Electric Company Thin film resistors on organic surfaces
US6198379B1 (en) * 1997-06-19 2001-03-06 Robert Bosch Gmbh Semiconductor component with piezoresistive measuring shunts
US10315013B2 (en) 2001-07-13 2019-06-11 Endophys Holdings, Llc Sheath with sensing capabilities
US10716921B2 (en) 2001-07-13 2020-07-21 Endophys Holdings, Llc Methods of using a dual-lumen sheath in intraluminal procedures
US9597480B2 (en) 2009-10-07 2017-03-21 Endophys Holding, LLC Intraluminal devices and systems
US9913959B2 (en) 2009-10-07 2018-03-13 Endophys Holdings, Llc Device configured for real-time pressure sensing
US20120234112A1 (en) * 2009-12-25 2012-09-20 Alps Electric Co., Ltd. Force sensor and method of manufacturing the same
US8516906B2 (en) * 2009-12-25 2013-08-27 Alps Electric Co., Ltd. Force sensor and method of manufacturing the same
US20110193363A1 (en) * 2010-02-10 2011-08-11 Seiko Epson Corporation Stress sensing device, tactile sensor, and grasping apparatus
US8573069B2 (en) * 2010-02-10 2013-11-05 Seiko Epson Corporation Stress sensing device, tactile sensor, and grasping apparatus
RU2474007C1 (en) * 2011-09-08 2013-01-27 Федеральное Государственное Бюджетное Учреждение "Научно-Производственный Комплекс "Технологический Центр" Миэт" Design of sensitive element of pressure converter based on silicon-on-insulator structure

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