CROSS-REFERENCE TO RELATED APPLICATION This application is related to U.S. application Ser. No. [Docket No. DP-312388] entitled “METHOD OF MAKING MICROSENSOR,” filed on the same date as the present application, the entire disclosure of which is hereby incorporated herein by reference.
TECHNICAL FIELD The present invention generally relates to acceleration sensors (i.e. accelerometers) and, more particularly, relates to a micro-machined capacitively coupled linear accelerometer for sensing magnitude and direction of linear acceleration.
BACKGROUND OF THE INVENTION Accelerometers are commonly employed to measure the second derivative of displacement with respect to time. In particular, linear accelerometers measure linear acceleration along a particular sensing axis. Linear accelerometers are frequently employed to generate an output signal (e.g., voltage) proportional to linear acceleration for use in any of a number of vehicle control systems. For example, the sensed output from a linear accelerometer may be used to control safety-related devices on an automotive vehicle, such as front and side impact air bags. According to other examples, accelerometers may be used in automotive vehicles for vehicle dynamics control and suspension control applications.
Conventional linear accelerometers often employ an inertial mass suspended from a support frame by multiple support beams. The mass, support beams and frame generally act as a spring mass system, such that the displacement of the mass is proportional to the linear acceleration applied to the frame. The displacement of the mass generates a voltage proportional to linear acceleration which, in turn, is used as a measure of the linear acceleration.
One type of an accelerometer is a micro-electromechanical structure (MEMS) sensor that employs a capacitive coupling between interdigitated fixed and movable capacitive plates that are movable relative to each other in response to linear acceleration. An example of a capacitive type single-axis linear accelerometer is disclosed in U.S. Pat. No. 6,761,070, entitled “MICROFABRICATED LINEAR ACCELEROMETER,” the entire disclosure of which is hereby incorporated herein by reference. An example of a capacitive type dual-axis accelerometer is disclosed in U.S. application Ser. No. 10/832,666, filed on Apr. 27, 2004, entitled “DUAL-AXIS ACCELEROMETER,” the entire disclosure of which is also hereby incorporated herein by reference.
Some conventional capacitive type accelerometers employ a vertical stacked structure to sense linear acceleration in the vertical direction. The stacked vertical structure typically has an inertial proof mass suspended between upper and lower fixed capacitive plates. The inertial proof mass moves upward or downward responsive to vertical acceleration. The measured change in capacitance between the proof mass and the fixed capacitive plates is indicative of the sensed acceleration. The vertical stacked structure employed in the aforementioned conventional linear accelerometer generally requires significant process complexities in the fabrication of the device using bulk and surface micro-machining techniques. As a consequence, conventional vertical sensing accelerometers typically suffer from high cost and undesired packaging sensitivity.
Additionally, the manufacturing process for fabricating conventional linear accelerometers typically involves a two-sided etch fabrication process which processes both the bottom and top of the patterned wafer. Conventional two-sided process fabrication typically uses a trench etching process, such as deep reactive ion etching (DRIE) and bond-etch back process. The etching process typically includes etching a pattern from a doped material suspended over a cavity to form a conductive pattern that is partially suspended over a cavity. The conventional etching processes typically require etching the patterned wafer from both the top and bottom sides. One example of a conventional etching approach is disclosed in U.S. Pat. No. 6,428,713, issued on Aug. 6, 2002, entitled “MEMS SENSOR STRUCTURE AND MICROFABRICATION PROCESS THEREFOR,” which is hereby incorporated herein by reference. Another example of an accelerometer fabrication process is disclosed in U.S. Pat. No. 5,006,487, entitled “METHOD OF MAKING AN ELECTROSTATIC SILICON ACCELEROMETER,” the entire disclosure of which is also hereby incorporated herein by reference.
The conventional two-sided fabrication process generally requires additional equipment to pattern and etch the top and bottom sides of two wafers and to achieve proper alignment and bonding of the two wafers. This equipment adds to the costs of the device. Additionally, since the patterned top and bottom wafers are aligned and bonded together, the device may suffer from misalignment and bond degradation.
Accordingly, it is therefore desirable to provide for a linear accelerometer and method of manufacturing a micro-machine microsensor that does not suffer undesired packaging sensitivity and other drawbacks of prior known sensors. In particular, it is desirable to provide for a cost-effective linear accelerometer that may sense vertical acceleration including both magnitude and direction of acceleration. It is further desirable to provide for a method of manufacturing a microsensor, such as a vertical linear accelerometer, that does not suffer from the above-described drawbacks of the prior known microsensor fabrication techniques.
SUMMARY OF THE INVENTION In accordance with the teachings of the present invention, a linear accelerometer is provided. The accelerometer includes a support substrate, a first fixed electrode having one or more first fixed capacitive plates having a first height, and a second fixed electrode having one or more second fixed capacitive plates having a second height. The accelerometer also has a movable inertial mass including one or more first movable capacitive plates capacitively coupled to the first fixed capacitive plates and one or more second movable capacitive plates capacitively coupled to the second fixed capacitive plates. The first movable capacitive plates have a third height greater than the first height of the first fixed capacitive plates, and the second movable capacitive plates have a fourth height less than the second height of the second fixed capacitive plates. The accelerometer further includes a support structure for supporting the movable inertial mass and allowing linear movement of the inertial mass upon experiencing a linear acceleration along a sensing axis. The accelerometer has an input for providing input signals to one of the fixed and movable capacitive plates, and an output for providing an output signal from the other of the fixed and movable capacitive plates which varies as a function of the capacitive coupling and is indicative of magnitude and direction of linear acceleration along the sensing axis.
By employing fixed and movable capacitive plates arranged to provide capacitive coupling with a height variation between opposing fixed and movable capacitive plates, the linear accelerometer measures a signal indicative of both the magnitude and the direction of acceleration. The accelerometer is particularly well-suited to measure vertical acceleration, according to one embodiment.
These and other features, advantages and objects of the present invention will be further understood and appreciated by those skilled in the art by reference to the following specification, claims and appended drawings.
BRIEF DESCRIPTION OF THE DRAWINGS The present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
FIG. 1 is a top view of a linear accelerometer shown with the overlying cover removed according to one embodiment of the present invention;
FIG. 2 is a partial cut away sectional view of the accelerometer taken through lines II-II ofFIG. 1;
FIG. 3 is a partial cut away sectional view of the accelerometer taken through lines III-III ofFIG. 1;
FIG. 4 is an enlarged view of section IV ofFIG. 1;
FIGS. 5A-5C are cross-sectional views taken through lines V-V ofFIG. 4 illustrating the fixed and movable capacitive plates subjected to no vertical acceleration inFIG. 5A, downward acceleration inFIG. 5B, and upward acceleration inFIG. 5C;
FIGS. 6A-6C are cross-sectional views taken through lines VI-VI ofFIG. 4 illustrating the fixed and movable capacitive plates subjected to no acceleration inFIG. 6A, downward acceleration inFIG. 6B, and upward acceleration inFIG. 6C;
FIG. 7 is a exemplary block/circuit diagram illustrating processing of the sensed capacitance output;
FIG. 8 is a block/circuit diagram further illustrating processing self-test circuitry coupled to the accelerometer;
FIG. 9 is a flow diagram illustrating process steps for fabricating the accelerometer according to the present invention;
FIGS. 10A-10H are cross-sectional views further illustrating the process steps for fabricating the accelerometer according to the present invention; and
FIG. 11 is a top view of a portion of the accelerometer illustrating a mask and etch module for forming the capacitive plates of different heights.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Linear Accelerometer
Referring toFIGS. 1-4, anaccelerometer10 is illustrated according to one embodiment of the present invention for sensing magnitude and direction of acceleration along at least one sensing axis, which is shown as the vertical Z-axis. Theaccelerometer10 is shown and described herein as a single-axis linear bi-directional accelerometer for sensing linear acceleration in both upward and downward directions of the vertical Z-axis, according to one embodiment. The Z-axis extends perpendicular to the plane defined by the X- and Y-axes. Alternately, theaccelerometer10 may be employed as a multi-axis accelerometer for sensing acceleration in multiple axes. For example, theaccelerometer10 may be employed as a three-axis accelerometer for sensing linear acceleration in any of the X-, Y- and Z-axes. Further, it should be appreciated that theaccelerometer10 could be employed to sense angular acceleration or angular velocity, such as angular acceleration or angular velocity about the Z-axis, as well as linear acceleration along the vertical Z-axis.
The bi-directionallinear accelerometer10 is a micro-machined MEMS accelerometer formed with a top-side etching process described herein according to one embodiment. Thelinear accelerometer10 is fabricated on a supportingsubstrate14, which may include a silicon substrate, according to one embodiment. Thesubstrate14 may be formed from a handle wafer having abond oxide layer52 formed on the top surface. Various electrical and mechanical components of the device are formed in an epitaxial (EPI) device layer above thesubstrate14. Anoverlying cover54 is shown inFIGS. 2 and 3 positioned on top to enclose theaccelerometer10 to prevent contamination and damage, such as that caused by moisture and particles.
Formed on top of the supportingsubstrate14 is aninertial proof mass12 which extends over acavity50. Theinertial mass12 is shown inFIG. 1 having a central portion extending to each of four corner quadrants. However, theinertial mass12 may be formed in any of a number of shapes and sizes.Inertial mass12 is suspended from thesupport substrate14 via a support structure shown, which, according to the embodiment includes four bent generally L-shapedtethers16A-16D, such that theinertial mass12 is movable at least upward and downward relative tosubstrate14 at least in a direction along the Z-axis when subjected to vertical acceleration.Tethers16A-16D may have any appropriate shape.
The four generally L-shapedtethers16A-16D extend between theinertial mass12 at one end and support anchoredcantilevers18A-18D, respectively, at the other end. Support anchored cantilevers18A-18D are rigidly fixed to and cantilevered from thesubstrate14 byrespective anchors19A-19D which are shown by hidden lines. Thetethers16A-16D have a length, width, depth and shape selected to achieve a desired resilient spring structure that flexes to allowinertial mass12 to move a distance within a desired range when subjected to vertical acceleration. Together, theinertial mass12 and tethers16A-16D act as a spring mass system. It should be appreciated any one or more supporting structures may be employed to support themass12 according to other embodiments. For example, four folded beam tethers could be employed.
The movableinertial mass12 has a plurality of rigid comb-likeconductive fingers20A and20B that form movable capacitive plates. The movableinertial mass12 includes first and thirdmovable capacitive plates20A and20C each extending lengthwise in a direction along the Y-axis, and second and fourthmovable capacitive plates20B and20D each extending lengthwise in a direction along the X-axis. Theinertial mass12 with the comb-like conductive fingers (plates)20A-20D forms a movable electrode that moves at least linearly in the sensing Z-axis when subjected to a vertical acceleration along the sensing Z-axis. For purposes of discussion herein, the X-axis and Y-axis are defined as shown oriented inFIG. 1, and the vertical Z-axis is defined as shown inFIGS. 2 and 3.
Thelinear accelerometer10 also includes four fixedelectrodes22A-22D shown generally located at ninety degree (90°) increments. The fixedelectrodes22A-22D generally extend from and are fixed to thesupport substrate14, and thus do not move relative to thesupport substrate14. Each of the fixedelectrodes22A-22D includes a plurality of fixedcapacitive plates30A-30D, respectively, which are generally formed as a plurality of rigid comb-like conductive fingers. The fixedcapacitive plates30A-30D are formed to be interdigitated with themovable capacitive plates20A-20D, respectively, to form four banks of variable capacitors. That is, themovable capacitive plates20A-20D are oriented parallel to and interdigitated with the plurality of fixedcapacitive plates30A-30D, respectively, so that adjacent capacitive plates face each other in a juxtaposition such that a capacitive coupling is provided.
The first plurality of fixedcapacitive plates30A of the firstfixed electrode22A are interdisposed between adjacent firstmovable capacitive plates20A of inertial mass (movable electrode)12 generally in a first quadrant of theinertial mass12. The firstfixed electrode22A has asignal input line24A for receiving an input clocked signal CLK applied to inputpad26. The input signal CLK is a clocked signal, such as a square wave signal according to one embodiment. Thecapacitive plates20A and30A thereby form a first bank of variable capacitors.
The thirdfixed electrode22C likewise includes a third plurality of fixedcapacitive plates30C interdisposed between adjacent thirdmovable capacitive plates20C ofinertial mass12 generally in the third quadrant ofinertial mass12 to provide a third bank of variable capacitors. The thirdfixed electrode22C has asignal input line24C for also receiving the input clocked signal CLK applied to inputpad26. The bank of variable capacitors formed bycapacitive plates20C and30C is generally symmetric with the first bank of variable capacitors formed bycapacitive plates20A and30A.
The secondfixed electrode22B includes a second plurality of fixedcapacitive plates30B interdisposed between adjacent secondmovable capacitive plates20B generally in the second quadrant ofinertial mass12 to provide a second bank of variable capacitors. The secondfixed electrode22B has a signal input line24B for receiving an input clocked signal CLKB applied to inputpad28. Clocked signal CLKB is one hundred eighty degrees (180°) out-of-phase, i.e., inverse, as compared to clocked signal CLK, according to one embodiment.
The fourth fixed electrode22D includes fourth fixedcapacitive plates30D interdisposed between adjacent fourthmovable capacitive plates20D generally in the fourth quadrant ofinertial mass12 to provide a fourth bank of variable capacitors. The fourth fixed electrode22D has asignal input line24D for also receiving the input clocked signal CLKB applied to inputpad28. The fourth bank of variable capacitors is generally symmetric with the second bank of variable capacitors.
Fixed electrodes22A-22D are electrically conductive and are electrically energized with out-of-phase input clocked signals CLK and CLKB. Clocked signals CLK and CLKB may include other out-of-phase signal waveforms, such as triangular or sine waveforms. Adjacentfixed electrodes22A-22D are dielectrically isolated from each other viaisolation trenches40 within the structure.
The sensedsignal output line32 is electrically coupled to inertial mass (movable electrode)12 via the secondbent tether16B. Theoutput line32 is further connected tooutput pad34 for supplying thereto the sensed output voltage (charge). The sensed output signal is the sensed voltage generated oninertial mass12 due to changes in capacitance in any of the four banks of variable capacitors caused by acceleration. The sensed output signal is further processed to determine the magnitude and direction of the sensed vertical acceleration.
The electrical components formed in the EPI device layer oversubstrate14 are formed by an etching process which removes material in the EPI layer, such as to form trenches. The input lines24A-24D,input pads26 and28,output line32,output pad34, tethers16A-16D, isolators36, and gaps between adjacent capacitive plates are formed astrenches40 as shown inFIG. 4.Trenches40 provide both physical separation and electrical isolation. The reduced height for certain capacitive plates is formed by partially etching the capacitive plates on the EPI layer from the top side with a vertical mask and etch module to achieve the desired height.
With particular reference toFIG. 4, the adjacent fixed andmovable capacitive plates30A-30B and20A-20B are shown spaced from each other by etchedtrenches40 which provide dielectric air gaps. The gaps allow themovable capacitive plates20A-20B to move relative to the fixedcapacitive plates30A-30B. The adjacent fixed andmovable capacitive plates30A-30B and20A-20B are separated by a greater distance on one side only inregion45, which enables the capacitors formed thereby to serve as self-test capacitors that enable testing of theaccelerometer10 with self-test processing circuitry. The remaining adjacent fixed andmovable capacitive plates30A-30B and20A-20B inregion43, which is outside ofregion45, are spaced from each other on each side by equal distances, according to one embodiment.Capacitive plates30C-30D and20C-20D are similarly spaced from each other.
Thelinear accelerometer10 according to the present invention employs fixed and movable capacitive plates interdisposed between adjacent opposing plates to form multiple banks of variable capacitors that sense both magnitude and direction of acceleration in the sensing Z-axis. Adjacent fixed and movable capacitive plates are configured having different heights to enable both the magnitude and direction of acceleration to be sensed. That is, thelinear accelerometer10 is able to sense not only magnitude of acceleration, but also the direction of the acceleration, e.g., upward or downward direction of vertical acceleration.
With particular reference toFIG. 2, the first and thirdmovable capacitive plates20A and20C are shown formed having a height that is less than the height of the first and thirdfixed capacitive plates30A and30C. The reduced height ofmovable capacitive plates20A and20C is realized by etching the EPI layer on the top surface of thecapacitive plates20A and20C to a reduced height. This height variance is further illustrated withcapacitive plates20A and30A inFIGS. 5A-5C.Capacitive plates20C and30C are formed similar tocapacitive plates20A and30A.
As seen inFIG. 5A,capacitive plates20A and30A are formed so that the bottom edge of each adjacent plate is substantially at the same elevation when there is no vertical acceleration present. The fixedcapacitive plates30A have a height that is higher than the reduced heightmovable capacitive plates20A by a predetermined distance Dr. Thecapacitive plates20A-20D and30A-30D may have a uniform doping (e.g., P+ or N+) or two different dopings (e.g., P+/N+ or P+(P++)/N+(N++)), according to one embodiment.
Capacitive plates20A and30A have an effective overlapping area that determines the amount of capacitance generated by that bank of capacitors. The maximum area of the resulting capacitors is functionally the area of the smallest plate. The capacitance therefore is a function of the overlapping height DCof adjacent opposing capacitor plates. When theinertial mass12 moves upward by distance D due to downward acceleration, as seen inFIG. 5B, the overlapping height DCand area of thecapacitor plates20A and30A remains the same (i.e., unchanged). When this happens there is no change in capacitance generated by these capacitive plates. When theinertial mass12 moves downward by distance D due to upward acceleration, as seen inFIG. 5C, the overlapping height DCand area of thecapacitor plates20A and30A is reduced. This causes a reduction in the capacitance generated by these capacitive plates. Thus, a change in capacitance ofcapacitive plates20A and30A is indicative of the direction as well as magnitude of the sensed acceleration.
With reference toFIG. 3, the second and fourthmovable capacitive plates20B and20D are shown having a height that is greater than the height of the second and fourth fixedcapacitive plates30B and30D. The reduced height of the fixedcapacitive plates30B and30D is realized by etching the EPI layer on the top surface of the capacitive plates connected to the second and fourthfixed electrodes22B and22D to a reduced height. This height variance is further illustrated withcapacitive plates20B and30B inFIGS. 6A-6C.Capacitive plates20D and30D are formed similar tocapacitive plates20A and30A.
As seen inFIG. 6A,capacitive plates20B and30B are formed so that the bottom edge of each adjacent plate is substantially at the same elevation when there is no vertical acceleration present. Themovable capacitive plates20B have a height that extends higher than the reduced height fixedcapacitive plates30B by a predetermined distance Dr.
Capacitive plates20B and30B have an effective overlapping area that determines the amount of capacitance generated by that bank of capacitors. The maximum area of the resulting capacitors is functionally the area of the smallest plate and, therefore, the capacitance is a function of the overlapping height DCof adjacent opposing capacitor plates. When theinertial mass12 moves upward by distance D due to downward acceleration, as seen inFIG. 6B, the overlapping height DCand area of thecapacitor plates20B and30B is reduced. This causes a reduction in the capacitance generated by these capacitive plates. Thus, a change in capacitance ofcapacitive plates20B and30B is indicative of the direction as well as magnitude of the sensed acceleration. When theinertial mass12 moves downward by distance D due to upward acceleration, as seen inFIG. 6C, the overlapping height DCand area of thecapacitor plates20B and30B remains the same (i.e., unchanged). When this happens there is no change in capacitance generated by these capacitive plates. Thus, no signal contribution to direction or magnitude is provided by this set of capacitors.
Thecapacitive plates20A-20D and30A-30D may be configured in various shapes and sizes. According to one embodiment,capacitive plates20A-20D and30A-30D are generally rectangular. The reduced height capacitive plates may be reduced in height up to one-half the height of the extended height capacitive plates, according to one embodiment. In one example, the reduced height capacitive plates have a height of twenty-eight micrometers (28 μm) as compared to a height of thirty micrometers (30 μm) for the extended height capacitive plates.
Referring toFIG. 7, a simplified representation of theaccelerometer10 is shown electrically coupled to signal processing circuitry, according to one embodiment. Theaccelerometer10 is generally represented as an electrical equivalent circuit having four electromechanical capacitors C1-C4 representing the four banks of variable capacitors. Capacitor C1 is formed bycapacitive plates20A and30A, capacitor C2 is formed bycapacitive plates20C and30C, capacitor C3 is formed bycapacitive plates20B and30B, and capacitor C4 is formed bycapacitive plates20D and30D. Thus, capacitors C1 and C2 receive input clocked signal CLK and capacitors C2 and C3 receive input clocked signal CLKB.
The sensed output signal received atoutput pad34 is input to acharge amplifier72 and is further processed by ademodulator75 shown receiving clocked signal CLK. The feedback path, CFin thecharge amplifier72, serves to prevent overloads in the high frequency front-end amplifier section and to minimize signal distortions due to high frequency signal components. Thecharge amplifier72 output voltage VOis inputted to thedemodulation circuit75 to generate the output voltage denoted by VOUT. The amplitude and sign of voltage VOUTrepresent the amplitude and direction of the vertical acceleration applied to theaccelerometer10.
The output voltage VOmay be represented by the following equation: VO=[(C3+C4)−(C1+C2)]/CF. When theinertial mass12 moves downward, output voltage VOmay be represented by the following simplified equation: VO=—(2*ΔC)*CLK/CF, where A C represents the change in capacitance of capacitors C3 and C4. When theinertial mass12 moves upward, then the output voltage VOmay be represented by the following simplified equation: VO=+(2*ΔC)*CLK/CF, where ΔC represents the change in capacitance of capacitors C1 and C2.
Accordingly, theaccelerometer10 of the present invention advantageously measures acceleration applied in either direction along the vertical sensing axis. By employing movable capacitive plates having a height different than the adjacent fixed capacitive plates, theaccelerometer10 senses magnitude of acceleration as well as the direction of the acceleration along the sensing axis. This is achieved by applying clocked signals CLK and CLKB, which are one hundred eighty degrees (180°) out-of-phase with each other, as inputs to the variable capacitors. Theaccelerometer10 advantageously provides high gain to linear acceleration sensed along the sensing Z-axis, while maintaining very low other linear and rotational cross-axis sensitivities.
While theaccelerometer10 is shown and described herein as a single-axis linear accelerometer, it should be appreciated thataccelerometer10 may be configured to sense acceleration in other sensing axes, such as the X- and Y-axes. Thus, theaccelerometer10 could be configured as a three-axis accelerometer. It should further be appreciated that theaccelerometer10 may be configured to sense angular acceleration or angular velocity.
Theaccelerometer10 may be tested following its fabrication by employing a self-test circuit as shown inFIG. 8, according to one embodiment. Theaccelerometer10 is generally illustrated having normal operation capacitive plates forming variable capacitors inregion43 and normal operation plus self-test capacitive plates forming variable capacitors inregion45. As mentioned above, the variable capacitors inregion43 are formed of capacitive plates that are linear and have equal gap spacings between each of the adjacent movable capacitive plates and the fixed capacitive plates. This gap spacing arrangement results in no response from motion along the X- and Y-axes, and allows for a change in capacitance when subjected to the vertical acceleration along the Z-axis. The normal plus self-test capacitive plates in conjunction with the input clock arrangement maximizes the main axis response while minimizing off axis responses.
The self-test operation can be performed by applying a clocked signal CLK to variable capacitor C1 and applying its clock compliment CLKB (one hundred eighty degrees (180°) out-of-phase) to variable capacitor C2. The average value of the clocked signal CLK and its compliment signal CLKB is designed to be different just as the self-test initiated and these average values are chosen for a desired electrostatically induced inertial mass displacement in the X-axis or Y-axis direction. Therefore, the X- and Y-mode shape may be designed in relation to the Z-mode shape such that an optimum trade-off is realized between the main sensing axis and cross-axis responses. Similarly, clocked signals CLK and CLKB are applied across variable capacitors C3 and C4. The sensed output voltage is further processed as explained in connection withFIG. 7 to generate an output voltage output VOUT.
Theaccelerometer10 shown provides four variable capacitors arranged in four symmetric quarters. However, it should be appreciated that two or more variable capacitors may be provided in other symmetries, such as one-half symmetries. It should also be appreciated that additional signal pads may be formed on theaccelerometer10. This may include a low impedance electrical ground connection to minimize electrical feedthrough components, an isolation pad, and a pad to create pseudo-differential electrical connection(s) between thesensor10 and readout electronic circuitry of the signal of signal processing integrated circuitry (IC).
Process of Manufacturing Microsensor
Referring now toFIG. 9 andFIGS. 10A-10H, aprocess100 is illustrated for fabricating a microsensor, such as thelinear accelerometer10 described above. The microsensor is a micro-electromechanical system (MEMS) sensor that is fabricated on thecrystal silicon substrate14. While thefabrication process100 is described herein according to one example to form thelinear accelerometer10, it should be appreciated the fabrication process may be used to form other microsensors.
Thefabrication process100 employs a trench etching process, such as deep reactive ion etching (DRIE) and bond-etch back process. The etching process generally includes etching out a pattern from a doped material inEPI device layer56 suspended oversubsurface cavity50 formed insubstrate14. Thefabrication process100 according to the embodiment shown provides for a top side etching process which employs a vertical mask and etch module for performing a top side mask and etch to remove material from the top side surface of epitaxial (EPI)device layer56 to achieve a reduced height dimension.
The sequence of the steps for fabricating the microsensor according to thefabrication process100 are illustrated inFIG. 9, according to one embodiment.FIGS. 10A-10H further illustrate the fabrication process ofFIG. 9 for forming a specific microsensor, particularly thelinear accelerometer10.Process100 is shown beginning withstep110 of formingsubsurface cavity50 in the top surface ofhandle wafer substrate14, and mating thehandle wafer substrate14 with the deviceEPI layer wafer56. This step is generally shown inFIG. 10A. Thehandle wafer substrate14 may include silicon or any other suitable support substrate. Grown on top surface ofsubstrate14 is anoxide bond layer52.Oxide bond layer52 may include silicon dioxide or any other suitable dielectric material for forming a silicon bond.
TheEPI device layer56 is shown having anupper wafer substrate58 formed on the top surface thereof.EPI device layer56 may include a single crystal EPI layer of silicon, according to one embodiment. In one example,EPI layer56 is thirty (30) micrometers thick. Theupper wafer substrate58 allows for ease in handling theEPI device layer56 during the fabrication process.
Fabrication process100 includesstep112 of bonding thehandle wafer substrate14 to theEPI layer56 and etching back theupper wafer substrate58 to leave theEPI layer56 formed over the cavity substrate. Thisstep112 is illustrated inFIG. 10B. Any appropriate silicon bonding method may be employed as is well-known in the art. Presumably, theEPI layer wafer56 is etched back to form a requisite device thickness. Etch stops for chemical etch back of bonded silicon layers are known in the art. Dopent concentration-dependent silicon etches are also known in the art. Concentration-dependent selective removal of a layer of one doping type material from the top of the second doping typing material (i.e., P+ removed selectively from N-type material or N-type material selectively removed from on top of P-type material) is further known in the art.
The fabricated microsensor, particularly thelinear accelerometer10, may employ a P-typedevice EPI layer56, according to one embodiment. The etch stop material may be a counter-doped P++ layer, according to one embodiment. Process steps of removing the P++ layer from the underlying P-type EPI layer are well-known in the art.
Once theEPI layer wafer56 is etched back to the desired device layer thickness (e.g., thirty (30) micrometers),fabrication process100 forms adielectric oxide layer60 on the top surface of theEPI device layer56 instep114. This step is seen inFIG. 10C.Layer60 may include silicon dioxide or any other suitable dielectric medium.
Next, as seen inFIG. 10D,contacts62 in the form of openings are formed in the oxide layer according to step116. Thecontacts62 may be formed by etching. Instep118, ametal conductor64 is deposited and patterned in thecontacts62 formed onoxide layer60, as seen inFIG. 10E. Additionally, the patternedmetal64 may further be passivated instep120. The patternedmetal64 may be aluminium or alloys of aluminium and silicon and other advantageous materials deposited by known sputtering or evaporation techniques. Accordingly,metal conductors64 are appropriately routed on top of theEPI device layer56.
Instep122,microsensor fabrication process100 patterns theoxide layer60 to expose portions of the top surface of devicesilicon EPI layer56. This exposesregions66 on the top side ofEPI layer60 as seen inFIG. 10F. The exposedregions66 include the overlying region where device components, such as capacitive plates and isolation trenches, are to be formed.
Referring toFIG. 10G and step124 of thefabrication process100 shown inFIG. 9, the silicon EPI device layer is masked and etched using a vertical mask and etch module on the top side to form areas of reducedheight EPI layer56. The reducedheight EPI layer56 is formed in regions where reduced height capacitive fingers or plates are desired, according to the embodiment shown. The reduced height regions are shown by etchedportions68. The step of masking and etchingEPI layer56 to form reducedheight regions68 is achieved by employing a mask andetch module70 seen inFIG. 11. In the embodiment shown, the vertical etch andmask module70 is placed on top of theregion68 that is to be etched to form the reduced height region(s). In this particular example, the vertical mask andetch module70 is placed on top of themovable capacitive plates20A to etch and remove material from the EPI layer to form reduced height capacitive plates. It should be appreciated that the verticaletching mask module70 likewise is placed on top ofmovable capacitive plates20C and fixedcapacitive plates30B and30D, to form the reduced height capacitive plates described in connection with thelinear accelerometer10.
The vertical mask andetch module70 is a top side processed module that may employ a photoresist mask applied to theEPI layer56, followed by a shallow silicon etch. The vertical mask andetch module70 creates a step in the silicon on the top side. The silicon etch step may include any of dry, wet or vapor phase etches, as is known in the art. The etch may be isotropic or anisotropic. If an isotropic etch is employed, the trenches that separate capacitive plates on theaccelerometer10, as well as the air gap distance between adjacentcapacitive plates40, should be sized appropriately. Once the etch is performed, the photoresist mask may be stripped from the surface, as is known in the art.
According to one example, the vertical mask and etch step may include spinning a photoresist, and masking areas to expose areas to be etched. This may include rinsing the photoresist material away from the areas to be etched. An etchant, such hydrofluoric (HF) acid according to a wet etching embodiment, is then applied to the areas to be etched. A desired depth etch may be achieved based on the etch rate of the etchant acid by controlling the time that the etchant acid is applied to the non-masked surface. Any appropriate silicon etch, such as a wet, dry or vapor etch, may be used as is known in the art.
Thefabrication process100 further includesstep126 of masking and etching the silicon EPI device layer to simultaneously form theisolation trenches40, and delineate the various features of the micro-machined device instep126. These features may include forming theinertial proof mass12, tether springs16A-16D, fixed electrodes and capacitive plates and the movable electrode and capacitive plates. These various features may be formed by masking and etching and is known in the art. According to one embodiment, this process step uses DRIE etching to do this etch due to its anisotropic characteristic and high aspect ratio (depth-to-surface width) ability. Following completion offabrication process100, the fabricated microsensor may be capped with an overlying cover to prevent contamination and moisture intrusion.
Accordingly, theprocess100 of the present invention advantageously provides for a top side microsensor fabrication technique. The process advantageously allows for the formation of different height structures on the device layer, without requiring added bottom side processing steps and equipment.
It will be understood by those who practice the invention and those skilled in the art, that various modifications and improvements may be made to the invention without departing from the spirit of the disclosed concept. The scope of protection afforded is to be determined by the claims and by the breadth of interpretation allowed by law.