WO2001075455A2 - Three axis accelerometer - Google Patents
Three axis accelerometer Download PDFInfo
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- WO2001075455A2 WO2001075455A2 PCT/US2001/010681 US0110681W WO0175455A2 WO 2001075455 A2 WO2001075455 A2 WO 2001075455A2 US 0110681 W US0110681 W US 0110681W WO 0175455 A2 WO0175455 A2 WO 0175455A2
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- WIPO (PCT)
- Prior art keywords
- response mass
- mass
- accelerometer
- etching
- response
- Prior art date
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/08—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
- G01P15/125—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by capacitive pick-up
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/08—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
- G01P15/0802—Details
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/18—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration in two or more dimensions
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/08—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
- G01P2015/0805—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration
- G01P2015/0822—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass
- G01P2015/084—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass the mass being suspended at more than one of its sides, e.g. membrane-type suspension, so as to permit multi-axis movement of the mass
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/08—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
- G01P2015/0805—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration
- G01P2015/0822—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass
- G01P2015/084—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass the mass being suspended at more than one of its sides, e.g. membrane-type suspension, so as to permit multi-axis movement of the mass
- G01P2015/0842—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass the mass being suspended at more than one of its sides, e.g. membrane-type suspension, so as to permit multi-axis movement of the mass the mass being of clover leaf shape
Definitions
- the present invention is directed to a three axis accelerometer and a method for making a three axis accelerometer, and more particularly, to an accelerometer having generally uniform sensitivity along three axes, as well as a method for making an accelerometer having generally uniform sensitivity along three axes.
- Accelerometers are used in a wide variety of mechanisms, including vehicles, aircraft, machinery and the like, to sense the acceleration experienced by the mechanism or to sense acceleration experienced by certain components ofthe mechanism.
- the accelerometers must be quite small (i.e. on the order of a few square millimeters) to be mounted onto the desired component.
- These small-scale accelerometers are often formed by etching a silicon wafer, using surface micromachining techniques, to form a number of accelerometers on the wafer. Each accelerometer may then be removed from the wafer and mounted to the desired component.
- accelerometers produced by surface micromachining can typically sense acceleration accurately only along two axes (i.e. the axes lying in the plane ofthe surface ofthe accelerometer).
- An additional, separate accelerometer is typically required if it is desired to accurately sense acceleration along a third, orthogonal axis. Accordingly, there is a need for a small scale accelerometer formed out of a silicon wafer that can accurately sense acceleration along three axes, as well as a method for forming such an accelerometer.
- the present invention is an accelerometer formed from a silicon wafer that can accurately sense acceleration along three axes, as well as a method for making such an accelerometer.
- the bulk ofthe wafer is etched using deep reactive ion etching to form a response mass ofthe accelerometer, which provides a response mass having a large thickness.
- the accelerometer ofthe present invention can measure acceleration along all three axes, and can measure acceleration with generally equal sensitivity along all three axes.
- the invention is a method for forming an accelerometer including the steps of providing a wafer of doped silicon, growing an oxide layer on the wafer, and forming an aperture in the oxide layer.
- the method further includes the steps of forming a layer of polysilicon on the wafer such that a portion ofthe polysilicon passes through the aperture and contacts the wafer, and etching the layer of polysilicon to form a beam and a capacitor plate.
- the wafer is then etched to form a response mass and a support, at least part ofthe response mass being located below the capacitor plate.
- the oxide layer is etched to separate the response mass from the support and from the capacitor plate, the response mass being coupled to the beam by polysilicon received through the aperture.
- the invention is an accelerometer including a conductive response mass, a support, a beam coupled to the support and to the response mass such that the response mass is supported by the beam, and a displacement sensor coupled to the support, the displacement sensor including at least three capacitor plates, each capacitor plate being located adjacent to the response mass to form a capacitor with the response mass, wherein acceleration ofthe accelerometer causes the response mass to be displaced relative the support, the displacement ofthe response mass relative the support causing a change in capacitance in at least two ofthe capacitors that is sensed by the displacement sensor.
- Fig. 1 is a top view of a one embodiment ofthe accelerometer ofthe present invention
- Fig. 2 is section view ofthe accelerometer of Fig. 1 taken along line 2-2 of Fig. 1;
- Fig. 3 is a section view ofthe accelerometer of Fig. 1 taken along line 3-3 of Fig. 1;
- Fig. 4 is a schematic representation ofthe accelerometer ofthe present invention experiencing acceleration in the Z direction;
- Fig. 5 is a schematic representation ofthe accelerometer of the present invention experiencing acceleration in the X direction;
- Fig. 6A is a top view ofthe support and response mass ofthe accelerometer of Fig. i;
- Fig. 6B is a detail view of a capacitor plate ofthe accelerometer of Fig. 1;
- Fig. 6C is a top view ofthe support and an alternate embodiment ofthe response mass
- Figs. 7-13 are a series of section views showing a method for manufacturing the accelerometer of Fig. 1;
- Figs. 14-20 are a series of section views showing a method for manufacturing an alternate embodiment ofthe accelerometer of Fig. 1;
- Fig. 21 is a circuit configuration for monitoring the acceleration of an accelerometer
- Fig. 22 is a timing diagram for achieving desired outputs from the circuit of Fig. 21;
- Fig. 23 is an amplifier output table corresponding to the amplifiers ofthe circuit configuration of Fig. 21;
- Figs. 24-30 are a series of section views showing an alternate method for manufacturing the accelerometer of Figs. 1-3.
- the sensor or accelerometer 10 ofthe present invention can be coupled to a component 12 to measure the acceleration experienced by the component 12.
- the accelerometer 10 includes a support 14, a set of capacitors Cl, C2, C3 and C4, a response mass 16, and a set of beams 18, 20, 22, 24 extending from the support to the response mass.
- the support 14 extends around the perimeter ofthe response mass 16, and is generally square in top view. Each side ofthe support 14 preferably has a length ranging from between about 1.5 mm and about 2.5 mm.
- the support 14 also includes a set of inwardly extending arms 26, 28, 30, 32, 34, 36, 38, 40. Adjacent arm pairs form a set of four cavities 42, 44, 46, 48 in the support 14, each cavity being located adjacent a corner ofthe support.
- the response mass 16 is located within the support 14, and includes a central portion 50 and four corner protrusions 52, 54, 56, 58. Each protrusion 52, 54, 56, 58 is closely received within a cavity 42, 44, 46, 48. As shown in Figs. 1 and 2, each beam 18, 20, 22, 24 is connected at one end to the support 14, and at the other end to the center of the response mass 16. A nonconductive layer, such as an oxide layer 61, is located between each beam 18, 20, 22, 24 and the support 14 (Figs. 2 and 3). The beams 18, 20, 22, 24 are located at the top ofthe support 14 and coupled to the top ofthe response mass 16 by an anchor 60 such that the response mass is suspended from the beams. The beams 18, 20, 22, 24 may also be located below the response mass 16.
- the beams 18, 20, 22, 24 support the response mass 16.
- the lower edge 15 ofthe response mass 16 is spaced above the lower edge 17 ofthe support 14 such that the response mass 16 is suspended from, and supported by, the beams 18, 20, 22, 24.
- the anchor 60 also provides an electrical contact between the suspension beams 18, 20, 22, 24 and the response mass 16.
- the accelerometer 10 includes four capacitor plates 66, 68, 70, 72, each capacitor plate having an end portion 74 and an overhang portion 76.
- Each capacitor plate 66, 68, 70, 72 is located over a cavity 42, 44, 46, 48 ofthe support 14 and the associated protrusion 52, 54, 56, 58 ofthe response mass 16.
- a non-conductive layer such as an oxide layer 61, is located between each capacitor plate 66, 68, 70, 72 and the support 14 (see Fig. 3).
- Parts ofthe overhang portions 76 of each capacitor plate are coupled to the arms 26, 28, 30, 32, 34, 36, 38, 40 of the support 14 to further attach the capacitor plates to the support.
- the arms help to support the capacitor plates 66, 68, 70, 72 to limit the deflection ofthe plates.
- parts ofthe overhang portion 76 of capacitor plate 66 are attached to the arms 26, 28, parts ofthe overhang portion 76 of capacitor plate 68 are attached to the arms 30, 32, parts ofthe overhang portion 76 of capacitor plate 70 are attached to the arms 34, 36, and parts ofthe overhang portion 76 of capacitor plate 72 are attached to the arms 38, 40.
- the capacitor plates may be located below the response mass 16.
- each capacitor plate/protrusion pairing forms a capacitor, shown as capacitors Cl, C2, C3 and C4 in Fig. 1.
- the materials and size ofthe capacitors Cl, C2, C3 and C4 are preferably matched such that the nominal capacitance value of each capacitor is equal.
- the change in capacitance in the capacitors is inversely proportional to the applied acceleration.
- the change in capacitance can be sensed in a manner well known in the art, and the acceleration can then be calculated.
- the response mass 16 moves downwardly (in the -Z direction) to its position shown in solid lines in Fig. 4 (the position ofthe response mass at rest being shown in hidden lines).
- the acceleration force is balanced by a spring force in the suspension beams 18, 20, 22, 24. Because the response mass 16 is moved further away from the capacitor plates 66, 68, 70, 72, the capacitance of the capacitors Cl, C2, C3 and C4 changes accordingly.
- the deflection ofthe response mass 16 can be measured. The measured displacement ofthe response mass 16 can then be converted into an acceleration.
- the response mass 16 tilts from its rest position (shown in hidden lines) to a displaced position (shown in solid lines).
- the response mass 16 tilts in the same manner (although around a different axis) as shown in Fig. 5.
- acceleration in the Y direction is governed by the same equations that are used when the accelerometer 10 experiences acceleration along the X axis.
- the lower edge 15 ofthe response mass 16 is spaced above the lower edge 17 ofthe support 14 sufficiently to enable the response mass 16 to move downwardly without engaging (i.e. "bottoming out on") the component 12.
- the deflection and acceleration ofthe response mass is directly proportional to (1/C2 - 1/C3), where C2 is the capacitance ofthe capacitor C2 and C3 is the capacitance ofthe capacitor C3.
- the capacitors C2 and C3 form a line or axis that extends along the X axis.
- the capacitance of any two capacitors that are spaced along the X axis may be used to measure X acceleration.
- the value of (1/C2 - 1/C3) changes only under X acceleration, and does not change under any other accelerations.
- the deflection and acceleration ofthe response mass is directly proportional to (1/Cl - 1/C2), where Cl is the capacitance ofthe capacitor Cl.
- the capacitors Cl and C2 form a line or axis that extends along the Y axis. Again, the capacitance of any two capacitors spaced along the Y axis may be used, and the value of (1/Cl - 1/C2) is only responsive to Y acceleration.
- the displacement and acceleration ofthe response mass is directly proportional to 1/Cl, 1/C2 or 1/C3.
- the displacement in the Z direction is calculated based upon (1/Cl + 1/C3).
- the value of (1/C1+ 1/C3) is responsive to Z acceleration only.
- a preferred circuit configuration 200 for monitoring the accelerometer is shown in Fig. 21, which depicts a switched-capacitor circuit approach.
- Three switched capacitor amplification stages 202, 204 and 206 with respective op-amps 203, 205 and 207 are provided in the circuit 200.
- a final stage 208 of the circuit 200 is made up of four track and hold circuit modules T/Hl, T/H2, T/H3 and T/H4.
- Each track and hold circuit module includes a respective sampling trigger input 210-1, 210-2, 210-3 and 210-4 for controlling when the respective module samples the voltage output level of amplification stage 206, and also includes a respective output 212- 1, 212-2, 212-3 and 212-4.
- Capacitors Cl, C2 and C3 ofthe accelerometer are connected in parallel in the feedback path of amplification stage 202, and are designated as capacitors Cxi, Cx2 and Cx3 respectively.
- Each capacitor Cxi, Cx2 and Cx3 is connected in series with a respective electronic switch S3, S4 or S5 for switching the capacitors into and out ofthe circuit.
- An electronic switch S12 is connected in series between the capacitors and a reference voltage NO.
- Electronic switch S6 is also provided in the feedback path of amplification stage 202. Accordingly, there are four potential feedback paths for amplification stage 202 which are selected to achieve desired circuit outputs.
- An input to amplification stage 202 is provided through switching circuit 214 which may be a 2 to 2 multiplexer.
- a reference voltage Nref such as 1.25 volts
- Switches SI and S2 are controlled to switch the input to amplification stage 202 between the upper and lower outputs ofthe switching circuit 214.
- a control input P to the switching circuit 214 controls which output ofthe switching circuit is high (1.25 volts) and which output is low (GND).
- the second and third amplification stages 204 and 206 each include selectable feedback paths.
- One ofthe selectable paths mcludes a capacitor C6 in series with an electronic switch S 8 or SI 1 and the other of which is formed by a straight connection through an electronic switch S7 or S10.
- Reference voltage NO is also selectively applicable to the capacitive feedback paths through electronic switches S9 and S12.
- Timing circuitry for achieving desired outputs from circuit 200 is shown.
- Timing circuitry (not shown) for generating the illustrated clock signals can be easily developed by those of skill in the art.
- Signal Chi controls switch S5; signal Ch2 controls switch S4; signal Ch3 controls switch S3; signal P controls the output state of switching circuit 214; signal ⁇ T2 controls switch S13; signal 613 controls switch SI; signal ⁇ T4 controls switch S2; signal Comp is provided as an input to second stage 204; signal 621 controls switches S7 and S9; signal ⁇ ->22 controls switch S8; signal 63 controls switches S10 and S12; signal 632 controls switch Sl l; signal Trackl is applied to T/Hl input 210-1; signal Track2 is applied to T/H2 input 210-2; signal Track3 is applied to T/H3 input 210-3; and signal Track4 is applied to T/H4 input 210-4.
- the X, Y and Z acceleration components can be determined.
- the voltage output of each amplification stage resulting from the sequential switching of capacitors Cxi and Cx2 into the feedback path of amplification stage 202 is shown at table segment 230.
- the resulting third stage output includes the desired (1/Cl - 1/C2) component.
- table segment 232 shows the amplification stage outputs when capacitors Cx3 and Cxi are sequentially switched into the feedback path of amplification stage 202.
- the third stage output includes the desired (1/C3 + 1/Cl) component.
- timing signal P goes high as capacitor Cxi is switched into the feedback path to assure that the critical third stage output component is additive rather than subtractive.
- Table segment 234 shows the amplification stage outputs when capacitors Cx2 and Cx3 are sequentially switched into the feedback path of amplification stage 202.
- the third stage output includes the desired component (1/Cl - 1/C3).
- Table segment 236 shows the circuit output when none ofthe capacitors are in the feedback path of amplification stage 202.
- Gl and G2 represent the gain constants of stages 204 and 206 respectively and are known per the electronic components used.
- each amplifier stage during clock phase 1 the amplifier is reset and the output is set to NO.
- the amplifier amplifies the voltage change in the input compared to the voltage value right at the moment the reset switch is open.
- the clock frequencies for first stage 202, second stage 204 and third stage 206 are f,f/2 an ⁇ f/4 as shown in the timing diagram 220.
- the frequency / is preferably in the range of tens of KHz. For clock signals "high” means a switch is closed and "low” means a switch is open.
- the operation repeats every two cycles.
- a stimulation signal is applied to the input and therefore the first stage output is the sum of (NrefCo)/Cx and some circuit offset errors.
- no stimulation signal is applied to the input and the first stage output is simply the offset error.
- the op-amp amplifies the output difference between the two cycles of the first stage.
- the output ofthe second stage 204 is a signal that represents one ofthe sense capacitors without offset errors.
- the unwanted sensor offset is canceled by intentionally applying negative offset by applying signal "Comp" to C4.
- the gain ofthe second stage is about 5.
- the circuit calculates and amplifies the difference between the outputs produced in the two cycles ofthe second stage 204.
- the output ofthe second stage corresponds to 1/Cx without any offset error.
- the switched-capacitor circuit itself can only perform subtraction.
- the polarity ofthe stimulus applied to the first stage is changed using switching circuit 214 when Cl is selected.
- Each ofthe track and hold modules (column 6 of Fig. 23) is controlled to sample the third stage output when the voltage at the output corresponds to the value shown in adjacent column 5 ofthe illustrated table.
- each track and hold module stores a respective acceleration indicative output.
- Module T/Hl stores the Y-direction acceleration indicative value
- module T/H2 stores the Z-direction acceleration indicative value
- module T/H3 stores the X-direction acceleration indicative value.
- the acceleration indicative third stage outputs all include a component "offset 2".
- Module T/H4 stores the value "offset 2" allowing it to be subtracted from each ofthe acceleration indicative outputs to provide final outputs which are directly proportional to acceleration.
- the value in module T/H4 can be subtracted from the value in module T/Hl and the resulting final value can be used to reference a stored acceleration map to determine the Y-direction acceleration.
- the resulting final value could be used to directly calculate the Y-direction acceleration.
- suitable processing circuitry 240 is provided to perform these functions as is l ⁇ iown in the art. Similar operations are performed to deteraiine X-direction acceleration and Z-direction acceleration.
- each capacitor Cl, C2, C3 is preferably located at a corner ofthe accelerometer 10. In this manner, capacitors Cl and C2 form a line that is perpendicular to a line formed by capacitors C2 and C3. This enables the accelerometer 10 to sense acceleration along all three axes.
- the accelerometer 10 may include a fourth capacitor plate 72 that forms a capacitor C4 with the response mass 16.
- the capacitor C4 is preferably used as an actuator that is used to implement a self-test mechanism.
- a DC voltage is applied to the capacitor plate 72, which causes the response mass 16 to be deflected (i.e. upwardly in the +Z direction).
- the deflection ofthe response mass 16 can then be sensed by the sense capacitors Cl, C2 and C3, and the measured deflection can be analyzed to check whether the sensed displacement ofthe response mass correlates with the expected displacement.
- E is the Young's modulus ofthe beams 18, 20, 22, 24; ⁇ is Poisson's ratio of the beams; b, h, andE are the width, thickness and length ofthe beams, respectively; m is the mass ofthe response mass 16; and a z is the acceleration in the Z direction.
- Equation (3) In order to achieve uniform triaxial sensitivity, the conditions of Equation (3) must be met in the design ofthe accelerometer.
- e is very small (on the order of microns), such that the condition of Equation (3) cannot be practically achieved. That is, L cannot be made small enough and d cannot be made large enough to compensate for the small value of e.
- DRIE deep reactive ion etching
- e can be on the same order of magnitude as L, such that uniform sensitivity over three axes is achievable.
- L 2 Ade
- the constant A is preferably about 6, but the value may deviate, up to an integer or more from 6 (i.e., from about 4 to about 8), while still providing acceptable sensitivities.
- good linearity ofthe accelerometer can be achieved when the full range of deflection ofthe response mass is less than 30% ofthe thickness ofthe beams.
- the full range of deflection of the response mass can be 4% or less ofthe thickness ofthe beams.
- FIG. 7-13 A preferred process for forming the accelerometer shown in Figs. 1-6 is shown in Figs. 7-13 and discussed below.
- the process begins with a silicon wafer 100 that is preferably heavily doped, the wafer typically being about 400 to 600 microns thick.
- the wafer may be made of other materials besides silicon such as glass, silicon carbide, polysilicon, or any number of ceramics.
- the wafer 100 can etched to simultaneously form a plurality of accelerometers on the wafer using batch processing techniques well l ⁇ iown in the art. For example, up to 1000 or more accelerometers may be fabricated on a four inch diameter wafer. However, for ease of illustration Figs. 7-20 and 24-30 show the forming of only a single accelerometer on a wafer 100.
- a top 102 and a bottom 104 oxide layer (such as silicon dioxide) are then grown onto the silicon wafer 100. Although the thickness ofthe oxide layers 102, 104 may vary, the oxide layers are typically about one micron thick.
- the top oxide layer 102 is then patterned by forming an aperture 106 in the center ofthe oxide. Either dry or wet etching techniques may be used to pattern the top oxide layer 102.
- the aperature 106 will ultimately be the location ofthe anchor 60 where the beams 18, 20, 22, 24 are attached to the response mass 16.
- a top layer 110 and a bottom layer 111 of polysilicon are deposited on top ofthe oxide layers 102, 104.
- the deposition ofthe bottom layer of polysilicon 111 is not necessary to the manufacturing process, but is a byproduct of depositing the top layer of polysilicon 110 and will subsequently be removed.
- the top polysilicon layer 110 is preferably heavily doped (such as n-type) to improve its conductivity, and may be from about 5-10 microns thick.
- Other materials besides polysilicon such as amorphous silicon, heavily doped silicon, glass, silicon carbide, polysilicon, ceramics, sapphire, single crystal silicon, metal, polyimid, silicon-on-insulator and the like may also be used.
- the top layer of polysilicon 110 is then patterned to form the desired shape ofthe suspension beams 18, 20, 22, 24 and capacitor plates 66, 68, 70, 72 (i.e. the shape of the suspension beams and capacitor plates shown in Figs. 1-3 and 6B).
- a series of release holes 114 are formed in the suspension beams 18, 20, 22, 24 (as shown in Fig. 10) and in the capacitor plates 66, 68, 70, 72 (not shown in Fig. 10) during this step.
- the release holes 114 can be seen in Fig. 1 and will be used as a conduit for a wet etching materials, as will be discussed in greater detail below.
- the suspension beams 18, 20, 22, 24, capacitor plates 66, 68, 70, 72 and release holes 114 may be varied to change the size and shape ofthe suspension beams 18, 20, 22, 24, capacitor plates 66, 68, 70, 72 and release holes 114.
- Various techniques of etching the top layer of polysilicon 110 may be used, although dry etching, such as reactive ion etching, is preferred.
- the bottom layer 111 of polysilicon is removed.
- the bottom oxide layer 104 is then removed, and the back side ofthe wafer 100 is etched (preferably using DRIE) to define the shape ofthe support 14 and the response mass 16, including the protrusions 52, 54, 56, 58 and cavities 42, 44, 46, 48, as shown in Figs. 6A or 6C.
- the size and shape ofthe support 14 and response mass 16 can be controlled during this step to produce desired qualities in the accelerometer 10.
- the response mass 16 may be shaped as the response mass shown in Fig. 6A or 6C, which provides differing values of J and b.
- the device is released by removing the upper oxide layer 102 between the response mass 16 and the suspension beams 18, 20, 22 and 24, and between the response mass 16 and the capacitor plates 66, 68, 70, 72 , as shown in Fig. 13.
- the portions ofthe upper oxide layer 102 are preferably removed with a wet etch material, such as hydrofluoric acid (HF).
- HF hydrofluoric acid
- the wet etch material is passed through the release holes 114 and the gaps 120 shown in Fig. 12 to etch away the oxide 102 connecting the suspension beams 18, 20, 22, 24 and the support 12, and the capacitor plates 66, 68, 70, 72 and the response mass 16.
- the etch release time during this step must be carefully controlled to ensure that contact remains between the response mass 16 and the beams 18, 20, 22, 24 (i.e.
- the anchor 60 is preferably at least about 50 microns, and the distance between the release holes is preferable about 25 microns.
- the process described above is a preferred method for forming the accelerometer 10 shown in Figs. 1-3, although different steps may be used to form the accelerometer without departing from the scope ofthe invention.
- a number of accelerometers 10 may be simultaneously etched onto a single, larger wafer (not shown). If this is the case, each accelerometer must then be released from the large wafer in a manner commonly known to those skilled in the art, for example through dicing. After the accelerometer 10 is released, it is packaged within a housing or packaging (not shown).
- a set of wires are then electrically coupled to the accelerometer 10 to couple the accelerometer to a signal conditioning circuit or a microprocessor, and the ends ofthe wire extend outside ofthe packaging.
- Each beam 18, 20, 22, 24 also includes a bonding pad 91 upon which a wire may be soldered, bonded, or otherwise attached.
- a wire that is coupled to one ofthe bonding pads 91 of one ofthe beams is electrically coupled to the response mass 16, because the beams are electrically coupled to the response mass by the anchor 60 (Fig. 2).
- the beams 18, 20, 22, 24 are electrically isolated from the support 14 due to the oxide layer 61 between the beams and the support 14 (Fig. 3).
- the mass ofthe response mass 16 may be selected during the manufacturing process to adjust the characteristics ofthe accelerometer 10 to the expected operating conditions. That is, the size, shape and mass ofthe response mass 16 may be adjusted to adapt the accelerometer to the expected range of acceleration. For example, a larger, more massive response mass 16 is desired when relatively low acceleration is expected. In contrast, when larger accelerations are expected, a smaller, lighter response mass 16 is desired.
- One advantage provided by the present invention is that the shape and mass ofthe response mass is not deteraiined until relatively late in the manufacturing process. This provides flexible manufacturing benefits.
- the desired size ofthe response mass 16 is not known in advance, a number of accelerometers may be partially formed and stored.
- the stored, partially completed accelerometers may be pulled from storage and quickly processed to completion.
- a manufacturer may process a number of wafers up through the processing step shown in Fig. 11, and then store the partially completed wafers.
- the desired shape and size ofthe response mass 16 may be calculated based upon the accelerometer specifications supplied by the customer.
- the partially completed wafers may then be pulled from storage, and processed according to the customer specifications. This provides flexibility and quick response time to the manufacturer.
- the size, shape, thickness and materials of various components of the accelerometer 10 may be varied to adapt the accelerometer to the expected operating characteristics.
- the size and shape ofthe response mass 16 may be varied to adapt the response mass to the expected range of accelerations.
- Fig. 6C illustrates a response mass 16 that is small compared to the response mass 16 of Fig. 6A. However, in some cases it may be desired to reduce mass ofthe response mass 16 even beyond that shown in Fig. 6C, and this is accomplished by etching the back side ofthe response mass 16, including those sections ofthe response mass forming the arms 19 (Fig. 6C) and the protrusions 52, 54, 56, 58.
- Fig. 20 illustrates an alternate embodiment 10' ofthe accelerometer 10 wherein the back side ofthe response mass 16 is etched to reduce the mass ofthe response mass.
- This embodiment is used when an accelerometer is needed to measure high accelerations, and where the response mass 16 needs to be decreased beyond the size ofthe response mass that can be made according to the process shown in Figs. 7-13.
- an additional DRIE etch may be applied to the response mass 16 to etch away the back side ofthe response mass under the protrusions 52, 54, 56, 58.
- the etching ofthe back side ofthe protrusions 52, 54, 56, 58 must be carefully controlled to ensure that the top parts ofthe protrusions 52, 54, 56, 58 remain to form the capacitors Cl, C2, C3, C4.
- Figs. 14-20 illustrate one manner in which the mass ofthe response mass 16 may be additionally reduced.
- the wafer 100 of Fig. 7 has the configuration shown in Fig. 11, as also shown in Fig. 14 (Figs. 14-20 illustrate a "diagonal" cross section ofthe wafer 100 , for example, taken along lines 3-3 of Fig. 1, whereas Figs. 7-13 illustrate a side cross section taken along lines 2-2 of Fig. 1).
- the bottom oxide layer 104 is then patterned with a first wet or dry etch, as shown in Fig. 15.
- a photoresist 126 is coated on the top ofthe bottom oxide 104 and patterned as shown in Fig. 16. It is advantageous to add the photoresist 126 on top ofthe bottom oxide 104 at this point as will be explained below.
- the extra mass that is desired to be etched from the under side ofthe wafer 100 is not covered by the photoresist 126.
- the wafer 110 is then time etched using DRIE and the areas ofthe wafer 110 that are not covered by the bottom oxide 104 and not covered by the photoresist 126 are etched away to a predetermined depth (about 50 microns in one embodiment) (Fig. 17).
- the photoresist 126 was placed onto the wafer 100 before the bulk ofthe wafer 100 was etched, the photoresist need not be placed onto the wafer after this etching step. This is advantageous because the newly etched areas 113 (Fig. 17) ofthe wafer would be coated by a photoresist if it were added after the wafer 100 were etched.
- the wafer 110 is then put into a liquid etch material to etch the exposed oxide 104 (i.e. the oxide not covered by the photoresist, Fig. 18).
- a second DRIE timed etch is employed to etch away the extra mass in the mass 16 to a predetermined depth, as shown in Fig. 19.
- the areas etched away during this step is controlled by the photoresist layer 126. Care must be taken to ensure that the response mass 16 is not etched all the way through, to ensure that parts ofthe response mass are located below each capacitor plate to act as an electrode ofthe capacitors Cl, C2, C3 and C4.
- the top oxide layer 102, photoresist 126 and bottom oxide layer 104 are then removed to form the accelerometer 10' shown in Fig. 20.
- the resultant accelerometer 10' has a response mass 16 with removed portions 13 (portions that are removed compared to the accelerometer 10 of Figs. 1-3).
- the center section 50, arms 19 and protrusions portions 52, 54, 56, 58 can be etched to their minimum required thickness to reduce the mass ofthe response mass. This reduces the weight ofthe response mass 16, which means that the accelerometer 10' is can sense higher accelerations.
- the additional etching steps of Figs. 14-20 changes e, and an appropriate compensation in the external processor or circuit is required to achieve uniform sensitivity ofthe accelerometer.
- other methods of etching the back side ofthe wafer to reduce the response mass may be used without departing from the scope ofthe present invention.
- Figs. 24-30 illustrate a method for forming an accelerometer similar to the accelerometer 10 of Figs. 1-3.
- the process begins with a wafer 140 having a top silicon layer 142 and a middle oxide layer 144.
- the wafer 140 is preferably heavily doped silicon, and the top silicon layer 142 is preferably about 5-10 microns thick and also heavily doped.
- the middle oxide layer 144 is preferably about 1 micron thick.
- the top silicon layer 142 is patterned to form the top capacitor plates 66, 68, 70, 72, suspension beams 18, 20, 22, 24, release holes 114 and an opening 148 for the anchor 60.
- a photoresist layer 150 is coated onto the top silicon layer 142, and is patterned to open a window 152 at the anchor area and opening 148.
- the portion ofthe oxide layer 144 located below the opening 148 is removed, and the photoresist 150 is then removed.
- a conductor, such as metal is deposited into the opening 148 (Fig. 28) to form an anchor 60' that ensures electrical contact between the suspension beams 18, 20, 22, 24 and the portion ofthe wafer 140 that will be formed as the response mass. If metal is used to form the anchor 60', the metal is preferably resistant to HF.
- the back side ofthe wafer 140 is etched to form the support 14 and the response mass 16.
- the response mass 16 is then released by etching the oxide layer 144 to form the accelerometer 10" as shown in Fig. 30.
- the accelerometer 10" may then be packaged and shipped to a customer, as described above.
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Abstract
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Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
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JP2001572880A JP2004506176A (en) | 2000-04-04 | 2001-04-03 | 3-axis accelerometer |
AU2001253093A AU2001253093A1 (en) | 2000-04-04 | 2001-04-03 | Three axis accelerometer |
Applications Claiming Priority (2)
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US54236300A | 2000-04-04 | 2000-04-04 | |
US09/542,363 | 2000-04-04 |
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WO2001075455A2 true WO2001075455A2 (en) | 2001-10-11 |
WO2001075455A3 WO2001075455A3 (en) | 2002-05-16 |
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PCT/US2001/010681 WO2001075455A2 (en) | 2000-04-04 | 2001-04-03 | Three axis accelerometer |
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JP (1) | JP2004506176A (en) |
AU (1) | AU2001253093A1 (en) |
WO (1) | WO2001075455A2 (en) |
Cited By (24)
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EP1517151A1 (en) * | 2003-09-16 | 2005-03-23 | Hitachi Metals, Ltd. | Acceleration sensor |
EP2100152A2 (en) * | 2006-12-18 | 2009-09-16 | Akustica Inc. | Proof-mass with supporting structure on integrated circuit-mems platform and method of fabricating the same |
EP2237049A1 (en) * | 2009-03-31 | 2010-10-06 | Domintech Co., LTD. | Process of fabricating a capacitive tri-axial accelerometer |
CN103238075A (en) * | 2010-09-18 | 2013-08-07 | 快捷半导体公司 | Micromachined 3-axis accelerometer with a single proof-mass |
US8978475B2 (en) | 2012-02-01 | 2015-03-17 | Fairchild Semiconductor Corporation | MEMS proof mass with split z-axis portions |
US9006846B2 (en) | 2010-09-20 | 2015-04-14 | Fairchild Semiconductor Corporation | Through silicon via with reduced shunt capacitance |
US9062972B2 (en) | 2012-01-31 | 2015-06-23 | Fairchild Semiconductor Corporation | MEMS multi-axis accelerometer electrode structure |
US9069006B2 (en) | 2012-04-05 | 2015-06-30 | Fairchild Semiconductor Corporation | Self test of MEMS gyroscope with ASICs integrated capacitors |
US9095072B2 (en) | 2010-09-18 | 2015-07-28 | Fairchild Semiconductor Corporation | Multi-die MEMS package |
US9094027B2 (en) | 2012-04-12 | 2015-07-28 | Fairchild Semiconductor Corporation | Micro-electro-mechanical-system (MEMS) driver |
US9156673B2 (en) | 2010-09-18 | 2015-10-13 | Fairchild Semiconductor Corporation | Packaging to reduce stress on microelectromechanical systems |
US9278845B2 (en) | 2010-09-18 | 2016-03-08 | Fairchild Semiconductor Corporation | MEMS multi-axis gyroscope Z-axis electrode structure |
US9278846B2 (en) | 2010-09-18 | 2016-03-08 | Fairchild Semiconductor Corporation | Micromachined monolithic 6-axis inertial sensor |
US9352961B2 (en) | 2010-09-18 | 2016-05-31 | Fairchild Semiconductor Corporation | Flexure bearing to reduce quadrature for resonating micromachined devices |
US9425328B2 (en) | 2012-09-12 | 2016-08-23 | Fairchild Semiconductor Corporation | Through silicon via including multi-material fill |
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US9488693B2 (en) | 2012-04-04 | 2016-11-08 | Fairchild Semiconductor Corporation | Self test of MEMS accelerometer with ASICS integrated capacitors |
US9618361B2 (en) | 2012-04-05 | 2017-04-11 | Fairchild Semiconductor Corporation | MEMS device automatic-gain control loop for mechanical amplitude drive |
US9625272B2 (en) | 2012-04-12 | 2017-04-18 | Fairchild Semiconductor Corporation | MEMS quadrature cancellation and signal demodulation |
WO2017188514A1 (en) * | 2016-04-26 | 2017-11-02 | (주)스탠딩에그 | Method for manufacturing mems device having improved offset drift characteristics, mems package including mems device, and computing system |
US10060757B2 (en) | 2012-04-05 | 2018-08-28 | Fairchild Semiconductor Corporation | MEMS device quadrature shift cancellation |
US10065851B2 (en) | 2010-09-20 | 2018-09-04 | Fairchild Semiconductor Corporation | Microelectromechanical pressure sensor including reference capacitor |
US10697994B2 (en) | 2017-02-22 | 2020-06-30 | Semiconductor Components Industries, Llc | Accelerometer techniques to compensate package stress |
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US7520170B2 (en) * | 2007-07-10 | 2009-04-21 | Freescale Semiconductor, Inc. | Output correction circuit for three-axis accelerometer |
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EP1517151A1 (en) * | 2003-09-16 | 2005-03-23 | Hitachi Metals, Ltd. | Acceleration sensor |
US7111514B2 (en) | 2003-09-16 | 2006-09-26 | Hitachi Metals, Ltd. | Acceleration sensor |
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EP2100152A4 (en) * | 2006-12-18 | 2011-06-08 | Akustica Inc | Proof-mass with supporting structure on integrated circuit-mems platform and method of fabricating the same |
US8094980B2 (en) | 2006-12-18 | 2012-01-10 | Akustica, Inc. | Proof-mass with supporting structure on integrated circuit-MEMS platform and method of fabricating the same |
EP2237049A1 (en) * | 2009-03-31 | 2010-10-06 | Domintech Co., LTD. | Process of fabricating a capacitive tri-axial accelerometer |
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US8978475B2 (en) | 2012-02-01 | 2015-03-17 | Fairchild Semiconductor Corporation | MEMS proof mass with split z-axis portions |
US9599472B2 (en) | 2012-02-01 | 2017-03-21 | Fairchild Semiconductor Corporation | MEMS proof mass with split Z-axis portions |
US9488693B2 (en) | 2012-04-04 | 2016-11-08 | Fairchild Semiconductor Corporation | Self test of MEMS accelerometer with ASICS integrated capacitors |
US10060757B2 (en) | 2012-04-05 | 2018-08-28 | Fairchild Semiconductor Corporation | MEMS device quadrature shift cancellation |
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US9444404B2 (en) | 2012-04-05 | 2016-09-13 | Fairchild Semiconductor Corporation | MEMS device front-end charge amplifier |
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US9625272B2 (en) | 2012-04-12 | 2017-04-18 | Fairchild Semiconductor Corporation | MEMS quadrature cancellation and signal demodulation |
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WO2021069071A1 (en) * | 2019-10-09 | 2021-04-15 | Gottfried Wilhelm Leibniz Universität Hannover | Electrical circuit |
Also Published As
Publication number | Publication date |
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WO2001075455A3 (en) | 2002-05-16 |
AU2001253093A1 (en) | 2001-10-15 |
JP2004506176A (en) | 2004-02-26 |
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