US20220349712A9 - Sensing device - Google Patents
Sensing device Download PDFInfo
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- US20220349712A9 US20220349712A9 US17/420,790 US201917420790A US2022349712A9 US 20220349712 A9 US20220349712 A9 US 20220349712A9 US 201917420790 A US201917420790 A US 201917420790A US 2022349712 A9 US2022349712 A9 US 2022349712A9
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- main body
- radial direction
- sensing device
- resonant member
- electrode
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
- G01C19/5719—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using planar vibrating masses driven in a translation vibration along an axis
- G01C19/5733—Structural details or topology
- G01C19/5755—Structural details or topology the devices having a single sensing mass
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
- G01C19/5705—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using masses driven in reciprocating rotary motion about an axis
- G01C19/5712—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using masses driven in reciprocating rotary motion about an axis the devices involving a micromechanical structure
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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
- G01P1/00—Details of instruments
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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
Definitions
- This application relates generally to a sensing device and more particularly, a sensing device such as a MEMS gyroscope or MEMS accelerometer.
- Inertial measurement devices such as gyroscopes and accelerometers, provide high-precision sensing.
- gyroscopes and accelerometers provide high-precision sensing.
- historically their cost, size, and power requirements have prevented their widespread use in industries such as consumer products, gaming devices, automobiles, and handheld positioning systems.
- MEMS micro-electro-mechanical systems
- State-of-the-art MEMS devices such as those disclosed in PTLs 1-7, are able to sense rotational (i.e. angle or angular velocity of rotation around an axis) or translational motion (i.e. linear acceleration along an axis) around and along axes.
- These devices typically include a resonant member surrounded by a plurality of electrodes that are spaced from the resonator by a capacitive gap.
- a sensing device 110 is illustrated in FIG. 6 that corresponds to a MEMS gyroscope, and includes a resonant member 112 , an anchor 114 that supports the resonant member 112 relative to a substrate 116 , and a plurality of electrodes 118 that are spaced from the resonant member 112 .
- Each electrode 118 is capacitively coupled to the resonant member 112 .
- the resonant member 112 has a plurality of capacitive surface portions 122 that each face and are capacitively coupled to an associated capacitive surface portion 128 of an electrode 118 .
- a capacitive channel 130 is thereby defined between the resonant member 112 and each electrode 118 .
- the resonant member 112 is movable in two resonant modes—a drive mode and a sense mode.
- two of the electrodes 118 a , 118 c are drive electrodes that are operable to apply a driving force to the resonant member 112 in an X direction so as to excite the resonant member 112 and vibrate the resonant member 112 in the drive mode at its natural frequency. If the resonant member 112 is rotated, the Coriolis Effect will transfer energy from the drive mode to the sense mode and cause the resonant member 112 to vibrate in the sense mode.
- two of the electrodes 118 b , 118 d are sense electrodes that are configured to generate a current in response to sense-mode movement of the resonant member 112 in a Y direction that is perpendicular to the X direction. This current can thus be analyzed to determine the rotation rate of the resonant member 112 .
- Each electrode 118 is aligned with a node axis of the resonant member 112 (for the purposes of this disclosure, a “node axis” of a resonant member is an axis that passes through two or more node points of the resonant member, and a “node point” refers to either an antinode or node of the resonant member when vibrating in the drive mode or sense mode).
- the drive electrodes 118 a , 118 c are aligned with a first node axis N 1 that passes through two node points 134 a , 134 c of the resonant member 112
- the sense electrodes 118 b , 118 d are aligned with a second node axis N 2 that passes through two other node points 134 b , 134 d of the resonant member 112 .
- the two node points 134 a , 134 c correspond to nodes of the resonant member 112 in sense mode and antipodes of the resonant member 112 in drive mode, while the other two node points 134 b , 134 d correspond to antinodes of the resonant member 112 in sense mode and nodes of the resonant member 112 in drive mode.
- the capacitive surface portions 122 , 128 of the resonant member 112 and electrodes 118 are preferably shaped and arranged such that their capacitive channels 130 are symmetrical about their associated node points 134 and node axes.
- the sense mode will not be excited when the resonant member 112 is under zero rate (i.e., no rotation), such that sense-mode movement of the resonant member 112 in the Y direction is zero and no current output is generated at the sense electrodes 118 b , 118 d that would falsely indicate rotation.
- some excitation of the sense electrodes 118 b , 118 d can occur even when the resonant member 112 is under zero rate.
- the sensing device 110 in FIG. 6 is typically manufactured using an etching process that divides a single body of material into the resonant member 112 and electrodes 118 .
- the capacitive channels 130 are formed at the locations of the single body that are etched, along with the capacitive surface portions 122 , 128 of the resonant member 112 and electrodes 118 .
- the capacitive surface portions 122 , 128 of the resonant member 112 and electrodes 118 are preferably shaped and arranged such that their capacitive channels 130 are symmetrical about their associated node axes.
- the capacitive surface portions 122 , 128 can have imperfections at the ends of each channel 130 that result in asymmetries of the channel 130 about its associated node axe.
- FIG. 7 shows an example wherein an imperfection 142 is formed in the capacitive surface portion 128 b of the sense electrode 118 b such that its capacitive channel 130 b is not symmetrical about the second node axis N 2 .
- the drive electrodes 118 a , 118 c are operated to excite the resonant member 112 in drive mode, some drive mode movement will be experienced at the capacitive surface portion 122 b of the resonant member 112 (see e.g., broken line 146 in FIG. 7 indicating drive-mode movement of the resonant member 112 ).
- the capacitive channel 130 b for the sense electrode 118 b was symmetrical about the second node axis N 2 , the effective capacitive displacement of the capacitive surface portion 122 b would be zero, thereby resulting in a zero current at the sense electrode 118 b .
- effective capacitive displacement of the capacitive surface portion 122 b will be non-zero, thereby producing a zero-rate output (ZRO) at the sense electrode 118 b that falsely indicates rotation of the resonant member 112 and can change over time and temperature.
- ZRO zero-rate output
- this asymmetry can cause the drive electrodes 118 a , 118 c to also excite sense-mode movement of the resonant member 112 under zero rate, which can further produce a ZRO at the sense electrodes 118 b , 118 d (even if the capacitive channels 130 b , 130 d for the sense electrodes 118 b , 118 d are perfectly symmetrical).
- the resonant member 112 includes a main body 136 that can be made of a single-crystal solid (e.g., silicon).
- the single-crystal structure of this base material causes the resonant member 112 to have material and component stiffnesses that are direction dependent (for the purposes of this disclosure, it is to be appreciated that “component stiffness” of an object refers to the overall stiffness of the object, while “material stiffness” of an object refers to the stiffness/Young's modulus of the object's underlying material).
- the main body 136 in FIG. 6 has a material stiffness that varies radially about a central axis M of the anchor 114 such that the main body 136 has a first material stiffness in a first radial direction D 1 and a second material stiffness in a second radial direction D 2 that is less than the first material stiffness.
- the angle between the first and second radial directions D 1 , D 2 is about 45 degrees, and material stiffnesses of the main body 136 along intermediate radial directions will gradually transition from the first material stiffness in the first radial direction D 1 to the second material stiffness in the second radial direction D 2 .
- the material stiffness of the main body 136 will periodically alternate between the first and second material stiffnesses every further 45 degrees about the central axis M
- the main body 136 has a component stiffness that will similarly vary periodically about the central axis M, such that the main body 136 has a first component stiffness in the first radial direction D 1 and a second component stiffness in the second radial direction D 2 that is less than the first component stiffness.
- This anisotropic component stiffness of the main body 136 about the central axis M of the anchor 114 will cause stiffer regions of the main body 136 to displace shorter distances during vibration than regions of the main body 136 that are more flexible, which in turn can create an imbalance of momentum forces at the anchor 114 that generate stress and lead to energy losses from the resonant member 112 .
- a sensing device includes an anchor having a central axis that defines a first radial direction and a second radial direction, and a resonant member flexibly supported by the anchor that includes a main body made of a single-crystal solid.
- the main body has a first material stiffness in the first radial direction and a second material stiffness in the second radial direction that is less than the first material stiffness.
- the main body has a first component stiffness in the first radial direction and a second component stiffness in the second radial direction that is substantially similar to the first component stiffness.
- the resonant member is movable in a resonant mode and the main body of the resonant member is shaped such that a net momentum force applied to the anchor from the resonant member from vibration in the resonant mode is 0.1 pN or less.
- a first distance between the central axis and an outer perimeter of the main body in the first radial direction is greater than a second distance between the central axis and the outer perimeter of the main body in the second radial direction.
- the main body defines an aperture located along the first radial direction that extends through the main body. In one example, the main body has no aperture located along the second radial direction between an inner perimeter and outer perimeter of the main body.
- the sensing device includes an electrode capacitively coupled to the resonant member, wherein the electrode is located in the aperture such that a capacitive channel is defined between the electrode and the main body that circumscribes the electrode. In one example, the electrode is capacitively coupled to the main body about an entire outer perimeter of the electrode. In one example, the capacitive channel has a line of symmetry that is substantially parallel to a drive direction of the resonant member.
- the single-crystal solid is silicon. In one example, the single-crystal solid is (100) oriented silicon.
- an angle between the first radial direction and second radial direction is about 45 degrees.
- a gyroscope includes the sensing device.
- a sensing device includes an anchor having a central axis that defines a first radial direction and a second radial direction, and a resonant member flexibly supported by the anchor that includes a main body made of a single-crystal solid.
- the resonant member is movable in a resonant mode and the main body of the resonant member is shaped such that a net momentum force applied to the anchor from the resonant member from vibration in the resonant mode is 0.1 pN or less.
- a sensing device includes a resonant member having a main body that defines an aperture extending through the main body, and an electrode capacitively coupled to the resonant member.
- the electrode is located in the aperture such that a capacitive channel is defined between the electrode and the main body that circumscribes the electrode.
- the electrode is capacitively coupled to the main body about an entire outer perimeter of the electrode.
- the capacitive channel follows a continuous path and has a width that is substantially constant along the continuous path.
- the capacitive channel has a line of symmetry that is substantially parallel to a drive direction of the resonant member.
- the sensing device includes an anchor having a central axis that defines a first radial direction and a second radial direction.
- the resonant member is flexibly supported by the anchor, the main body of the resonant member is made of a single-crystal solid and has a first material stiffness in the first radial direction and a second material stiffness in the second radial direction that is less than the first stiffness, and the aperture is located along the first direction.
- a first distance between the central axis and an outer perimeter of the main body in the first radial direction is greater than a second distance between the central axis and the outer perimeter of the main body in the second radial direction.
- a gyroscope includes the sensing device.
- a sensing device includes a resonant member having a main body that defines a pair of first apertures and a pair of second apertures extending through the main body; a pair of first electrodes capacitively coupled to the resonant member that are arranged respectively in the pair of first apertures; and a pair of second electrodes capacitively coupled to the resonant member that are arranged respectively in the pair of second apertures.
- the pair of first electrodes are aligned on a first axis that extends through a center of each first electrode
- the pair of second electrodes are aligned on a second axis that extends through a center of each second electrode
- the first axis is substantially perpendicular to the second axis.
- FIG. 1 is a schematic plan view of an example sensing device
- FIG. 2 is an enlarged view of the sensing device in FIG. 1 ;
- FIG. 3 is an enlarged, schematic plan view of an example decoupling mechanism of the sensing device
- FIG. 4 is a schematic plan view of another embodiment of the sensing device.
- FIG. 5 is a schematic plan view of yet another embodiment of the sensing device.
- FIG. 6 is an example sensing device in the prior art.
- FIG. 7 is an enlarged view of the sensing device in FIG. 6 .
- Example embodiments are described and illustrated in the drawings. These examples are not intended to be a limitation on the present invention. For example, one or more aspects can be utilized in other embodiments and even other types of devices. Moreover, certain terminology is used herein for convenience only and is not to be taken as a limitation.
- an example sensing device 10 includes a resonant member 12 , an anchor 14 that is fixed to a substrate 16 and flexibly supports the resonant member 12 , and a plurality of electrodes 18 that are capacitively coupled to the resonant member 12 .
- the sensing device 10 in the present embodiment corresponds to a MEMS gyroscope. However, the sensing device 10 can correspond to other sensing devices in other examples such as a MEM accelerometer.
- the resonant member 12 is flexibly supported by the anchor 14 such that the resonant member 12 is movable in two resonant modes a drive mode and a sense mode.
- two of the electrodes 18 a , 18 c are drive electrodes that are operable to capacitively induce a driving force to the resonant member 12 in an X direction so as to excite the resonant member 12 and vibrate the resonant member 12 in the drive mode at a particular frequency (e.g., the resonant member's natural frequency). If the resonant member 12 is rotated, the Coriolis Effect will transfer energy from the drive mode to the sense mode and cause the resonant member 12 to vibrate in the sense mode.
- two of the electrodes 18 b , 18 d are sense electrodes that are configured to capacitively generate a current in response to sense-mode movement of the resonant member 12 in a Y direction that is perpendicular to the X direction. This current can thus be analyzed to determine the rotation rate of the resonant member 12 .
- Each electrode 18 is preferably aligned with a node axis of the resonant member 12 .
- the centers of the drive electrodes 18 a , 18 c in the present embodiment are aligned with a first node axis ⁇ that passes through two node points 34 a , 34 c of the resonant member 12
- the centers of the sense electrodes 18 b , 18 d are aligned with a second node axis ⁇ that passes through two other node points 34 b , 34 d of the resonant member 12 and is substantially perpendicular to the first node axis ⁇
- substantially perpendicular means 1 degrees or less from perpendicular, and preferably 0.5 degrees or less from perpendicular, and more preferably 0.1 degrees or less from perpendicular).
- the two node points 34 a , 34 c correspond to nodes of the resonant member 112 in sense mode and antinodes of the resonant member 12 in drive mode, while the other two node points 34 b , 34 d correspond to antinodes of the resonant member 12 in sense mode and nodes of the resonant member 12 in drive mode.
- the electrodes 18 can be arranged differently and/or provide different capacitive functions in other examples.
- one or more electrodes 18 can correspond to a tuning or alignment electrode.
- one or more electrodes 18 can be aligned along or offset from different node axes that are substantially oblique to each other.
- one or more electrodes 18 can each comprise a plurality of electrodes that are electrically connected to each other.
- the associated node points 34 of each electrode 18 may correspond to other nodes or antinodes of one or more resonant modes.
- the electrodes 18 can be configured in a variety of different manners without departing from the scope of this disclosure.
- the resonant member 12 comprises a main body 36 having a center of mass cm that is aligned with a central axis ⁇ of the anchor 14 .
- the shape of the main body 36 can vary by embodiment.
- the main body 36 is a planar body that extends along the X-Y plane and circumscribes the anchor 14 .
- the main body 36 has an inner perimeter 38 that defines an opening 40 extending through the main body 36 for the anchor 14 to reside in.
- the main body 36 further has an outer perimeter 42 .
- the main body 36 can be made of a single-crystal or polycrystalline solid.
- the main body 36 in the present embodiment comprises a single-crystal solid and more specifically, (100)-oriented single-crystal silicon.
- the main body 36 can comprise other orientations of single-crystal silicon such as, for example, (111) and (110).
- the main body can comprise other single-crystal solids such as beryllium.
- the sensing device 10 relates to embodiments in which the main body 36 comprises a single-crystal solid.
- the main body 36 will have a material stiffness that is direction dependent.
- the main body 36 in the present example has a material stiffness that varies radially about the central axis ⁇ of the anchor 14 such that the main body 36 has a first material stiffness in a first radial direction R 1 and a second material stiffness in a second radial direction R 2 that is less than the first material stiffness.
- the first radial direction R 1 is aligned with the first node axis a of the resonant member 12 , and the angle between the first and second radial directions R 1 , R 2 is about 45 degrees such that the first and second radial directions R 1 , R 2 are non-orthogonal to each other.
- the material stiffness of the main body 36 along radial directions between the first and second radial directions R 1 , R 2 will gradually transition from the first material stiffness in the first radial direction R 1 to the second material stiffness in the second radial direction R 2 .
- the material stiffness of the main body 36 will periodically alternate between the first and second material stiffnesses every 45 degrees about the central axis ⁇ .
- first and second radial directions R 1 , R 2 can be located at other angles about the central axis w.
- the period in which material stiffness changes about the central axis ⁇ can be different in other embodiments.
- the geometry of the main body 36 can be optimized to mimic the behavior of an isotropic material and achieve low instantaneous momentum flow along any arbitrary in-plane direction.
- the geometry of the main body 36 can be varied about the central axis ⁇ such that the component stiffness of the main body 36 is substantially isotropic.
- a radial distance r between the central axis ⁇ and the outer perimeter 42 of the main body 36 can vary about the central axis ⁇ so that radial segments with greater material stiffness have a greater radial distance r than radial segments with lower material stiffness.
- the main body 36 can be formed such that radial segments with greater material stiffness define one or more apertures 44 that extend through the main body 36 , while radial segments with lower material stiffness define no apertures or define apertures that are fewer in number and/or smaller in size.
- the present embodiment employs both approaches, such that a radial distance r 1 in the first radial direction R 1 is greater than a radial distance r 2 in the second radial direction R 2 , and an aperture 44 b is located along the first radial direction R 1 while no aperture is located along the second radial direction R 2 between the inner and outer perimeters 40 , 42 of the main body 36 .
- the radial distance r between the central axis ⁇ and outer perimeter 42 varies continuously around the central axis ⁇ such that the outer perimeter 42 has four convex portions 42 a that are interconnected by four concave portions 42 b.
- the component stiffness of the main body 36 can be made substantially isotropic such that component stiffnesses in different radial directions of the main body 36 are substantially similar to each other (for the purposes of this disclosure, two component stiffnesses in different radial directions are “substantially similar” if their ratio is from 0.9 to 1.1, and preferably from 0.95 to 1.05, and more preferably from 0.98 to 1.02).
- the main body 36 in the present embodiment has a first component stiffness in the first radial direction R 1 and a second component stiffness in the second radial direction R 2 that is substantially similar to the first component stiffness.
- a net momentum force applied to the anchor 14 from vibration in one or both of sense mode and drive mode is preferably 0.1 pN or less, and more preferably 0.01 pN or less, and still more preferably 0.0001 or less.
- the configuration of the main body 36 can be varied about the central axis ⁇ of the anchor 14 in a variety of different ways to compensate for anisotropic material stiffness and result in a component stiffness for the main body 36 that is substantially isotropic.
- the radial distance r between the central axis ⁇ and the outer perimeter 42 of the main body 36 can be relatively constant about the central axis ⁇ while one or more apertures 44 are provided in stiffer radial segments of the main body 36 to compensate for anisotropic material stiffness.
- main body 36 can be apertureless while the radial distance r between the central axis ⁇ End the outer perimeter 42 of the main body 36 is varied about the central axis ⁇ to compensate for anisotropic material stiffness.
- the main body 36 may comprise a polycrystalline solid having isotropic material stiffness in some examples such that the configuration of the main body 36 can be relatively constant about the central axis ⁇ while having isotropic component stiffness. Still further, the main body 36 can be configured in some examples such that its component stiffness is anisotropic or partially isotropic about the central axis ⁇ regardless of its material.
- Another aspect of the sensing device 10 relates to an arrangement of its electrodes 18 . More specifically, as shown in FIG. 1 , one or more electrodes 18 of the sensing device 10 can be arranged within associated apertures defined by the main body 36 of the resonator 12 . In the present embodiment, the electrodes 18 are arranged within the apertures 44 described above that compensate for the main body's anisotropic material stiffness. However, the electrodes 18 can be arranged in other apertures that do not serve to compensate for anisotropic material stiffness, such as in embodiments wherein the main body 36 has isotropic material stiffness.
- the electrodes 18 can be arranged in their associated apertures 42 such that for each electrode 18 , a capacitive channel 50 is defined between the electrode 18 and main body 36 that circumscribes (i.e., completely surrounds) the electrode 18 .
- each electrode 18 and associated aperture 44 can be located a long an associated node axis of the resonant member 12 .
- the electrodes 18 a , 18 c and apertures 44 a , 44 c in the present embodiment are located along the first node axis ⁇ such that the electrodes 18 a , 18 c and apertures 44 a , 44 c are respectively concentric with the node points 34 a , 34 c .
- the electrodes 18 b , 18 d and apertures 44 b , 44 d in the present embodiment are located along the second node axis ⁇ such that the electrodes 18 b , 18 d and apertures 44 b , 44 d are respectively concentric with the node points 34 b , 34 d .
- the electrodes 18 and apertures 44 can be arranged at other locations in other embodiments.
- FIG. 2 An enlarged view of the sense electrode 18 b and its associated aperture 44 b and capacitive channel 50 b is shown in FIG. 2 in a stationary state of the main body 36 , which will now be described in further detail.
- the structure described with respect to the sense electrode 18 b can be similarly applied to the other electrodes 18 of the sensing device 10 .
- the main body 36 has a capacitive surface 52 b that defines the aperture 44 b and circumscribes the electrode 18 b .
- the electrode 18 b has a capacitive surface 54 b that extends completely about the electrode 18 b and is spaced from the capacitive surface 52 b of the main body 36 by the capacitive channel 50 b .
- the capacitive surfaces 52 b , 54 b of the main body 36 and electrode 18 b are capacitively coupled such that the electrode 18 b is capacitively coupled to the main body 36 about an entire outer perimeter of the electrode 18 b .
- the electrode 18 b and aperture 44 b in FIG. 2 are substantially circular in shape such that their capacitive surfaces 52 b , 54 b are cylindrical.
- the shapes of these features can vary in other embodiments.
- the electrode 18 b and aperture 44 b can be substantially square in shape such that their capacitive surfaces 52 b , 54 b each comprise four, substantially planar surface portions.
- the capacitive channel 50 b follows a continuous path 60 b around the electrode 18 b and preferably has a line of symmetry 64 b that is substantially parallel with the drive direction (i.e., X direction) of the resonant member 12 (For the purposes of this disclosure, a line of symmetry for a capacitive channel is “substantially parallel” to the drive direction if the line of symmetry and drive direction are 1 degrees or less from parallel, and preferably 0.1 degrees or less from parallel, and more preferably 0.01 degrees or less from parallel. In some examples, the capacitive channel 50 b can have additional lines of symmetry that are, for example, perpendicular to the line of symmetry 64 b.
- the continuous path 60 b of the capacitive channel 50 b is preferably symmetric in shape, and the capacitive channel 50 b preferably has a width w (measured as the distance between capacitive surfaces 52 b , 54 b ) that is substantially constant along the continuous path 60 b of the capacitive channel 50 b .
- a width of a capacitive channel is substantially constant along a given path if a maximum variance of the width is 7% or less, and preferably 1% or less, and more preferably 0.5% or less.
- a maximum variance of the width in some examples can be 20 nm or less, and preferably 5 nm or less, and more preferably 1 nm or less.
- a cross-sectional area 70 b ′ of the capacitive channel 50 b on one side of the line of symmetry 64 b will be substantially equal to a cross-sectional area 70 b ′′ of the capacitive channel 50 b on an opposite side of the line of symmetry 64 b (the cross-sectional areas 70 b ′, 70 b “being taken along the X-Y plane).
- these cross-sectional areas 70 b ”, 70 b ′′ will remain substantially equal to each other as the resonant member 12 moves in the drive direction X in drive mode.
- the fabrication process that is commonly used to form capacitive channels between electrodes and a resonant member in a sensor device can form imperfections in the capacitive surface portions at the ends of the channel.
- the capacitive channel 50 b in the present embodiment is a continuous channel that circumscribes the electrode 18 b , there are no end portions of the capacitive channel 50 b that are likely to cause imperfections in the capacitive surfaces 52 b , 54 b of the main body 36 and electrode 18 b , thereby further preventing the ZRO effect that is caused by asymmetries in a capacitive channel.
- the resonant member 12 is flexibly supported by the anchor 14 such that the resonant member 12 is movable in two resonant modes—the drive mode and sense mode.
- U.S. Patent Application Publication No. 2016/0327390 which is incorporated herein by reference in its entirety, discloses various example structures (referred to as “decoupling mechanisms”) for flexibly supporting a resonant member relative to a substrate that can be applied to the sensing device 10 of the present disclosure.
- These structures are referred to as “decoupling mechanisms” because they attach the resonant member to a support structure (e.g., anchor) such that the resonant Member is flexibly supported while mitigating energy transfer (i.e., energy loss) of the resonant member to the anchor.
- energy transfer can get coupled to another mode (e.g., sense mode) from the resonant member and further cause the ZRO effect described above.
- FIG. 3 of the present disclosure includes a flange 82 that circumscribes and is directly connected to the anchor 14 of the sensing device 10 described above.
- the decoupling mechanism 80 further includes a plurality ring portions 84 including a first ring portion 84 a that circumscribes and is radially spaced from the flange 82 , a second ring portion 84 b that circumscribes and is radially spaced from the first ring portion 84 a , and a third ring portion 84 c that circumscribes and is radially spaced from the second ring portion 84 b .
- the third ring portion 84 c is circumscribed by the main body 36 of the resonant member 12 such that the main body 36 is radially spaced from the third ring portion 84 c.
- the decoupling mechanism 80 includes a plurality of connecting portions 86 including a plurality of first connecting portions 86 a that connect the first ring portion 84 a to the flange 82 , a plurality of second connecting portions 86 b that connect the second ring portion 84 b to the first ring portion 84 a , a plurality of third connecting portions 86 c that connect the third ring portion 84 c to the second ring portion 84 b , and a plurality of fourth connecting portions 86 d that connect the third ring portion 84 c to the main body 36 .
- connection portions 86 are located about the central axis w of the anchor 14 such that the first connecting portions 86 a are circumferentially aligned with each other and circumferentially spaced by an angle ⁇ 1 , the second connecting portions 86 b are circumferentially aligned with each other and circumferentially spaced by the angle ⁇ 1 , the third connecting portions 86 c are circumferentially aligned with each other and circumferentially spaced by the angle ⁇ 1 , and the fourth connecting portions 86 d are circumferentially aligned with each other and circumferentially spaced by the angle ⁇ 1 , wherein the angle ⁇ 1 is 22.5 degrees.
- each first connecting portion 86 a is radially aligned with an associated third connecting portion 86 c
- each second connecting portion 86 b is radially aligned with an associated fourth connecting portion 86 d
- the first and third connecting portions 86 a , 86 c are radially offset from the second and fourth connecting portions 86 b , 86 d by an angle ⁇ 2 that is 12.25 degrees.
- the ring portions 84 of the decoupling mechanism 80 above act as buffer that reduce anchor loss to the anchor 14 . It is possible to further reduce energy loss by implementing additional rings 84 and connecting portions 86 that connect the additional rings 84 to the three rings 84 a , 84 b , 84 c above. However, implementing extra rings may lower the resonant frequency of some modes and adversely impact the vibration immunity of the sensing device 10 . It has been found that a four-ring design can substantially reduce energy loss while also ensuring that the lowest mode frequency is not too low.
- FIG. 4 illustrates an embodiment of the sensing device 10 wherein the outer periphery 42 of the main body 36 is a circle.
- the drive mode executes negligible normal displacement at the sense electrodes 18 b , 18 d . Capacitive transduction of this mode is negligible as electrostatic forces are approximately perpendicular to the resonator boundary.
- FIG. 5 illustrates an embodiment of the sensing device 10 wherein a plurality of release holes 92 are arranged so as to form an equilateral triangle when connecting specific three release holes 92 .
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Abstract
Description
- This application relates generally to a sensing device and more particularly, a sensing device such as a MEMS gyroscope or MEMS accelerometer.
- Inertial measurement devices, such as gyroscopes and accelerometers, provide high-precision sensing. However, historically their cost, size, and power requirements have prevented their widespread use in industries such as consumer products, gaming devices, automobiles, and handheld positioning systems.
- More recently, micro-electro-mechanical systems (MEMS) sensor devices have been gaining increased attention from multiple industries since micro-machining technologies have made fabrication of miniature gyroscopes and accelerometers possible. Miniaturization also enables integration of MEMS devices with readout electronics on the same die, resulting in reduced size, cost, and power consumption as well as improved resolution by reducing noise. Consumer products such as digital cameras, 3D gaming equipment, and automotive sensors are employing MEMS devices because of their numerous advantages. The demand for low cost, more sophisticated, and user-friendly devices by the consumers has caused a steep rise in the demand of MEMS sensors, as they offer adequate reliability and performance at very low prices. State-of-the-art MEMS devices, such as those disclosed in PTLs 1-7, are able to sense rotational (i.e. angle or angular velocity of rotation around an axis) or translational motion (i.e. linear acceleration along an axis) around and along axes. These devices typically include a resonant member surrounded by a plurality of electrodes that are spaced from the resonator by a capacitive gap.
- For instance, a
sensing device 110 is illustrated inFIG. 6 that corresponds to a MEMS gyroscope, and includes aresonant member 112, ananchor 114 that supports theresonant member 112 relative to asubstrate 116, and a plurality of electrodes 118 that are spaced from theresonant member 112. Each electrode 118 is capacitively coupled to theresonant member 112. - More specifically, the
resonant member 112 has a plurality of capacitive surface portions 122 that each face and are capacitively coupled to an associated capacitive surface portion 128 of an electrode 118. A capacitive channel 130 is thereby defined between theresonant member 112 and each electrode 118. - The
resonant member 112 is movable in two resonant modes—a drive mode and a sense mode. In particular, two of theelectrodes resonant member 112 in an X direction so as to excite theresonant member 112 and vibrate theresonant member 112 in the drive mode at its natural frequency. If theresonant member 112 is rotated, the Coriolis Effect will transfer energy from the drive mode to the sense mode and cause theresonant member 112 to vibrate in the sense mode. Moreover, two of theelectrodes resonant member 112 in a Y direction that is perpendicular to the X direction. This current can thus be analyzed to determine the rotation rate of theresonant member 112. - Each electrode 118 is aligned with a node axis of the resonant member 112 (for the purposes of this disclosure, a “node axis” of a resonant member is an axis that passes through two or more node points of the resonant member, and a “node point” refers to either an antinode or node of the resonant member when vibrating in the drive mode or sense mode). More specifically, the
drive electrodes node points resonant member 112, and thesense electrodes other node points 134 b, 134 d of theresonant member 112. The twonode points resonant member 112 in sense mode and antipodes of theresonant member 112 in drive mode, while the other twonode points 134 b, 134 d correspond to antinodes of theresonant member 112 in sense mode and nodes of theresonant member 112 in drive mode. Moreover, the capacitive surface portions 122, 128 of theresonant member 112 and electrodes 118 are preferably shaped and arranged such that their capacitive channels 130 are symmetrical about their associated node points 134 and node axes. - Ideally, the sense mode will not be excited when the
resonant member 112 is under zero rate (i.e., no rotation), such that sense-mode movement of theresonant member 112 in the Y direction is zero and no current output is generated at thesense electrodes sense electrodes resonant member 112 is under zero rate. For example, thesensing device 110 inFIG. 6 is typically manufactured using an etching process that divides a single body of material into theresonant member 112 and electrodes 118. The capacitive channels 130 are formed at the locations of the single body that are etched, along with the capacitive surface portions 122, 128 of theresonant member 112 and electrodes 118. As noted above, the capacitive surface portions 122, 128 of theresonant member 112 and electrodes 118 are preferably shaped and arranged such that their capacitive channels 130 are symmetrical about their associated node axes. However, due to imperfections that arise in the fabrication process when forming the ends of each channel 130, the capacitive surface portions 122, 128 can have imperfections at the ends of each channel 130 that result in asymmetries of the channel 130 about its associated node axe. -
FIG. 7 shows an example wherein animperfection 142 is formed in thecapacitive surface portion 128 b of thesense electrode 118 b such that its capacitive channel 130 b is not symmetrical about the second node axis N2. When thedrive electrodes resonant member 112 in drive mode, some drive mode movement will be experienced at the capacitive surface portion 122 b of the resonant member 112 (see e.g.,broken line 146 inFIG. 7 indicating drive-mode movement of the resonant member 112). If the capacitive channel 130 b for thesense electrode 118 b was symmetrical about the second node axis N2, the effective capacitive displacement of the capacitive surface portion 122 b would be zero, thereby resulting in a zero current at thesense electrode 118 b. However, because the capacitive channel 130 b is not symmetrical, effective capacitive displacement of the capacitive surface portion 122 b will be non-zero, thereby producing a zero-rate output (ZRO) at thesense electrode 118 b that falsely indicates rotation of theresonant member 112 and can change over time and temperature. Additionally, if there is asymmetry in one or both of thecapacitive channels 130 a, 130 c for thedrive electrodes drive electrodes resonant member 112 under zero rate, which can further produce a ZRO at thesense electrodes capacitive channels 130 b, 130 d for thesense electrodes - Another potential problem with the
sensing device 110 inFIG. 6 relates to anisotropic stiffness of itsresonant member 112. More specifically, theresonant member 112 includes amain body 136 that can be made of a single-crystal solid (e.g., silicon). The single-crystal structure of this base material causes theresonant member 112 to have material and component stiffnesses that are direction dependent (for the purposes of this disclosure, it is to be appreciated that “component stiffness” of an object refers to the overall stiffness of the object, while “material stiffness” of an object refers to the stiffness/Young's modulus of the object's underlying material). - For instance, the
main body 136 inFIG. 6 has a material stiffness that varies radially about a central axis M of theanchor 114 such that themain body 136 has a first material stiffness in a first radial direction D1 and a second material stiffness in a second radial direction D2 that is less than the first material stiffness. The angle between the first and second radial directions D1, D2 is about 45 degrees, and material stiffnesses of themain body 136 along intermediate radial directions will gradually transition from the first material stiffness in the first radial direction D1 to the second material stiffness in the second radial direction D2. Moreover, the material stiffness of themain body 136 will periodically alternate between the first and second material stiffnesses every further 45 degrees about the central axis M - Consequently, the
main body 136 has a component stiffness that will similarly vary periodically about the central axis M, such that themain body 136 has a first component stiffness in the first radial direction D1 and a second component stiffness in the second radial direction D2 that is less than the first component stiffness. This anisotropic component stiffness of themain body 136 about the central axis M of theanchor 114 will cause stiffer regions of themain body 136 to displace shorter distances during vibration than regions of themain body 136 that are more flexible, which in turn can create an imbalance of momentum forces at theanchor 114 that generate stress and lead to energy losses from theresonant member 112. - [PTL 1]
- U.S. Pat. No. 7,543,496
- [PTL 2]
- U.S. Pat. No. 7,578,189
- [PTL 3]
- U.S. Pat. No. 7,892,876
- [PTL 4]
- U.S. Pat. No. 8,173,470
- [PTL 5]
- U.S. Pat. No. 8,372,677
- [PTL 6]
- U.S. Pat. No. 8,528,404
- [PTL 7]
- U.S. Pat. No. 8,166,816
- The following presents a simplified summary of example embodiments of the invention. This summary is not intended to identify critical elements of the invention or to delineate the scope of the invention. The sole purpose of the summary is to present some example embodiments in simplified form as a prelude to the more detailed description that is presented later.
- According to a first aspect, a sensing device includes an anchor having a central axis that defines a first radial direction and a second radial direction, and a resonant member flexibly supported by the anchor that includes a main body made of a single-crystal solid. The main body has a first material stiffness in the first radial direction and a second material stiffness in the second radial direction that is less than the first material stiffness. Moreover, the main body has a first component stiffness in the first radial direction and a second component stiffness in the second radial direction that is substantially similar to the first component stiffness.
- In one example of the first aspect, the resonant member is movable in a resonant mode and the main body of the resonant member is shaped such that a net momentum force applied to the anchor from the resonant member from vibration in the resonant mode is 0.1 pN or less.
- In one example of the first aspect, a first distance between the central axis and an outer perimeter of the main body in the first radial direction is greater than a second distance between the central axis and the outer perimeter of the main body in the second radial direction.
- In another example of the first aspect, the main body defines an aperture located along the first radial direction that extends through the main body. In one example, the main body has no aperture located along the second radial direction between an inner perimeter and outer perimeter of the main body. In one example, the sensing device includes an electrode capacitively coupled to the resonant member, wherein the electrode is located in the aperture such that a capacitive channel is defined between the electrode and the main body that circumscribes the electrode. In one example, the electrode is capacitively coupled to the main body about an entire outer perimeter of the electrode. In one example, the capacitive channel has a line of symmetry that is substantially parallel to a drive direction of the resonant member.
- In yet another example of the first aspect, the single-crystal solid is silicon. In one example, the single-crystal solid is (100) oriented silicon.
- In still yet another example of the first aspect, an angle between the first radial direction and second radial direction is about 45 degrees.
- In another example of the first aspect, a gyroscope includes the sensing device.
- According to a second aspect, a sensing device includes an anchor having a central axis that defines a first radial direction and a second radial direction, and a resonant member flexibly supported by the anchor that includes a main body made of a single-crystal solid. The resonant member is movable in a resonant mode and the main body of the resonant member is shaped such that a net momentum force applied to the anchor from the resonant member from vibration in the resonant mode is 0.1 pN or less.
- According to a third aspect, a sensing device includes a resonant member having a main body that defines an aperture extending through the main body, and an electrode capacitively coupled to the resonant member. The electrode is located in the aperture such that a capacitive channel is defined between the electrode and the main body that circumscribes the electrode.
- In one example of the third aspect, the electrode is capacitively coupled to the main body about an entire outer perimeter of the electrode.
- In another example of the third aspect, the capacitive channel follows a continuous path and has a width that is substantially constant along the continuous path.
- In yet another example of the third aspect, the capacitive channel has a line of symmetry that is substantially parallel to a drive direction of the resonant member.
- In still yet another example of the third aspect, the sensing device includes an anchor having a central axis that defines a first radial direction and a second radial direction. The resonant member is flexibly supported by the anchor, the main body of the resonant member is made of a single-crystal solid and has a first material stiffness in the first radial direction and a second material stiffness in the second radial direction that is less than the first stiffness, and the aperture is located along the first direction. In one example, a first distance between the central axis and an outer perimeter of the main body in the first radial direction is greater than a second distance between the central axis and the outer perimeter of the main body in the second radial direction. In another example of the third aspect, a gyroscope includes the sensing device.
- According to a fourth aspect, a sensing device includes a resonant member having a main body that defines a pair of first apertures and a pair of second apertures extending through the main body; a pair of first electrodes capacitively coupled to the resonant member that are arranged respectively in the pair of first apertures; and a pair of second electrodes capacitively coupled to the resonant member that are arranged respectively in the pair of second apertures.
- In one example of the fourth aspect, the pair of first electrodes are aligned on a first axis that extends through a center of each first electrode, the pair of second electrodes are aligned on a second axis that extends through a center of each second electrode, and the first axis is substantially perpendicular to the second axis.
- It is to be understood that both the foregoing general description and the following detailed description present example and explanatory embodiments. The accompanying drawings are included to provide a further understanding of the described embodiments and are incorporated into and constitute a part of this specification. The drawings illustrate various example embodiments.
- The foregoing and other aspects of the present invention will become apparent to those skilled in the art to which the present invention relates upon reading the following description with reference to the accompanying drawings, in which:
-
FIG. 1 is a schematic plan view of an example sensing device; -
FIG. 2 is an enlarged view of the sensing device inFIG. 1 ; -
FIG. 3 is an enlarged, schematic plan view of an example decoupling mechanism of the sensing device; -
FIG. 4 is a schematic plan view of another embodiment of the sensing device; -
FIG. 5 is a schematic plan view of yet another embodiment of the sensing device; -
FIG. 6 is an example sensing device in the prior art; and -
FIG. 7 is an enlarged view of the sensing device inFIG. 6 . - Example embodiments are described and illustrated in the drawings. These examples are not intended to be a limitation on the present invention. For example, one or more aspects can be utilized in other embodiments and even other types of devices. Moreover, certain terminology is used herein for convenience only and is not to be taken as a limitation.
- Turning to
FIG. 1 , anexample sensing device 10 includes aresonant member 12, ananchor 14 that is fixed to asubstrate 16 and flexibly supports theresonant member 12, and a plurality of electrodes 18 that are capacitively coupled to theresonant member 12. Thesensing device 10 in the present embodiment corresponds to a MEMS gyroscope. However, thesensing device 10 can correspond to other sensing devices in other examples such as a MEM accelerometer. - The
resonant member 12 is flexibly supported by theanchor 14 such that theresonant member 12 is movable in two resonant modes a drive mode and a sense mode. In the present embodiment, two of theelectrodes resonant member 12 in an X direction so as to excite theresonant member 12 and vibrate theresonant member 12 in the drive mode at a particular frequency (e.g., the resonant member's natural frequency). If theresonant member 12 is rotated, the Coriolis Effect will transfer energy from the drive mode to the sense mode and cause theresonant member 12 to vibrate in the sense mode. Moreover, two of theelectrodes 18 b, 18 d are sense electrodes that are configured to capacitively generate a current in response to sense-mode movement of theresonant member 12 in a Y direction that is perpendicular to the X direction. This current can thus be analyzed to determine the rotation rate of theresonant member 12. Each electrode 18 is preferably aligned with a node axis of theresonant member 12. For example, the centers of thedrive electrodes node points resonant member 12, and the centers of thesense electrodes 18 b, 18 d are aligned with a second node axis β that passes through two other node points 34 b, 34 d of theresonant member 12 and is substantially perpendicular to the first node axis α (for the purposes of this disclosure, “substantially perpendicular” means 1 degrees or less from perpendicular, and preferably 0.5 degrees or less from perpendicular, and more preferably 0.1 degrees or less from perpendicular). The twonode points resonant member 112 in sense mode and antinodes of theresonant member 12 in drive mode, while the other twonode points 34 b, 34 d correspond to antinodes of theresonant member 12 in sense mode and nodes of theresonant member 12 in drive mode. - However, it is to be appreciated that the electrodes 18 can be arranged differently and/or provide different capacitive functions in other examples. For example, one or more electrodes 18 can correspond to a tuning or alignment electrode. As another example, one or more electrodes 18 can be aligned along or offset from different node axes that are substantially oblique to each other. Furthermore, one or more electrodes 18 can each comprise a plurality of electrodes that are electrically connected to each other. Still further, the associated node points 34 of each electrode 18 may correspond to other nodes or antinodes of one or more resonant modes. The electrodes 18 can be configured in a variety of different manners without departing from the scope of this disclosure.
- The
resonant member 12 comprises amain body 36 having a center of mass cm that is aligned with a central axis ω of theanchor 14. The shape of themain body 36 can vary by embodiment. In the present example, themain body 36 is a planar body that extends along the X-Y plane and circumscribes theanchor 14. In particular, themain body 36 has aninner perimeter 38 that defines anopening 40 extending through themain body 36 for theanchor 14 to reside in. Themain body 36 further has anouter perimeter 42. - The
main body 36 can be made of a single-crystal or polycrystalline solid. For instance, themain body 36 in the present embodiment comprises a single-crystal solid and more specifically, (100)-oriented single-crystal silicon. However, themain body 36 can comprise other orientations of single-crystal silicon such as, for example, (111) and (110). Moreover, the main body can comprise other single-crystal solids such as beryllium. - One aspect of the
sensing device 10 relates to embodiments in which themain body 36 comprises a single-crystal solid. In such embodiments, themain body 36 will have a material stiffness that is direction dependent. For instance, themain body 36 in the present example has a material stiffness that varies radially about the central axis ω of theanchor 14 such that themain body 36 has a first material stiffness in a first radial direction R1 and a second material stiffness in a second radial direction R2 that is less than the first material stiffness. The first radial direction R1 is aligned with the first node axis a of theresonant member 12, and the angle between the first and second radial directions R1, R2 is about 45 degrees such that the first and second radial directions R1, R2 are non-orthogonal to each other. The material stiffness of themain body 36 along radial directions between the first and second radial directions R1, R2 will gradually transition from the first material stiffness in the first radial direction R1 to the second material stiffness in the second radial direction R2. Moreover, the material stiffness of themain body 36 will periodically alternate between the first and second material stiffnesses every 45 degrees about the central axis ω. However, it is to be appreciated that the first and second radial directions R1, R2 can be located at other angles about the central axis w. Moreover, the period in which material stiffness changes about the central axis ω can be different in other embodiments. To compensate for anisotropic material stiffness of themain body 36, the geometry of themain body 36 can be optimized to mimic the behavior of an isotropic material and achieve low instantaneous momentum flow along any arbitrary in-plane direction. In particular, the geometry of themain body 36 can be varied about the central axis ω such that the component stiffness of themain body 36 is substantially isotropic. For example, a radial distance r between the central axis ω and theouter perimeter 42 of themain body 36 can vary about the central axis ω so that radial segments with greater material stiffness have a greater radial distance r than radial segments with lower material stiffness. In addition or alternatively, themain body 36 can be formed such that radial segments with greater material stiffness define one or more apertures 44 that extend through themain body 36, while radial segments with lower material stiffness define no apertures or define apertures that are fewer in number and/or smaller in size. - The present embodiment employs both approaches, such that a radial distance r1 in the first radial direction R1 is greater than a radial distance r2 in the second radial direction R2, and an
aperture 44 b is located along the first radial direction R1 while no aperture is located along the second radial direction R2 between the inner andouter perimeters main body 36. Indeed, the radial distance r between the central axis ω andouter perimeter 42 varies continuously around the central axis ω such that theouter perimeter 42 has fourconvex portions 42 a that are interconnected by fourconcave portions 42 b. - By varying the configuration of the
main body 36 about the central axis ω to compensate for anisotropic material stiffness, the component stiffness of themain body 36 can be made substantially isotropic such that component stiffnesses in different radial directions of themain body 36 are substantially similar to each other (for the purposes of this disclosure, two component stiffnesses in different radial directions are “substantially similar” if their ratio is from 0.9 to 1.1, and preferably from 0.95 to 1.05, and more preferably from 0.98 to 1.02). For instance, themain body 36 in the present embodiment has a first component stiffness in the first radial direction R1 and a second component stiffness in the second radial direction R2 that is substantially similar to the first component stiffness. Accordingly, an imbalance of momentum forces that results at theanchor 14 due to anisotropic component stiffness can be prevented or mitigated. For instance, in some examples, a net momentum force applied to theanchor 14 from vibration in one or both of sense mode and drive mode is preferably 0.1 pN or less, and more preferably 0.01 pN or less, and still more preferably 0.0001 or less. - It is to be appreciated that the configuration of the
main body 36 can be varied about the central axis ω of theanchor 14 in a variety of different ways to compensate for anisotropic material stiffness and result in a component stiffness for themain body 36 that is substantially isotropic. For instance, the radial distance r between the central axis ω and theouter perimeter 42 of themain body 36 can be relatively constant about the central axis ω while one or more apertures 44 are provided in stiffer radial segments of themain body 36 to compensate for anisotropic material stiffness. As another example,main body 36 can be apertureless while the radial distance r between the central axis ω End theouter perimeter 42 of themain body 36 is varied about the central axis ω to compensate for anisotropic material stiffness. - Moreover, the
main body 36 may comprise a polycrystalline solid having isotropic material stiffness in some examples such that the configuration of themain body 36 can be relatively constant about the central axis ω while having isotropic component stiffness. Still further, themain body 36 can be configured in some examples such that its component stiffness is anisotropic or partially isotropic about the central axis ω regardless of its material. - Another aspect of the
sensing device 10 relates to an arrangement of its electrodes 18. More specifically, as shown inFIG. 1 , one or more electrodes 18 of thesensing device 10 can be arranged within associated apertures defined by themain body 36 of theresonator 12. In the present embodiment, the electrodes 18 are arranged within the apertures 44 described above that compensate for the main body's anisotropic material stiffness. However, the electrodes 18 can be arranged in other apertures that do not serve to compensate for anisotropic material stiffness, such as in embodiments wherein themain body 36 has isotropic material stiffness. - The electrodes 18 can be arranged in their associated
apertures 42 such that for each electrode 18, a capacitive channel 50 is defined between the electrode 18 andmain body 36 that circumscribes (i.e., completely surrounds) the electrode 18. Moreover, each electrode 18 and associated aperture 44 can be located a long an associated node axis of theresonant member 12. For example, theelectrodes apertures electrodes apertures electrodes 18 b, 18 d andapertures electrodes 18 b, 18 d andapertures - An enlarged view of the sense electrode 18 b and its associated
aperture 44 b and capacitive channel 50 b is shown inFIG. 2 in a stationary state of themain body 36, which will now be described in further detail. However, it is to be appreciated that the structure described with respect to the sense electrode 18 b can be similarly applied to the other electrodes 18 of thesensing device 10. - As shown in
FIG. 2 , themain body 36 has a capacitive surface 52 b that defines theaperture 44 b and circumscribes the electrode 18 b. Meanwhile, the electrode 18 b has a capacitive surface 54 b that extends completely about the electrode 18 b and is spaced from the capacitive surface 52 b of themain body 36 by the capacitive channel 50 b. The capacitive surfaces 52 b, 54 b of themain body 36 and electrode 18 b are capacitively coupled such that the electrode 18 b is capacitively coupled to themain body 36 about an entire outer perimeter of the electrode 18 b. The electrode 18 b andaperture 44 b inFIG. 2 are substantially circular in shape such that their capacitive surfaces 52 b, 54 b are cylindrical. However, it is to be appreciated that the shapes of these features can vary in other embodiments. For instance, the electrode 18 b andaperture 44 b can be substantially square in shape such that their capacitive surfaces 52 b, 54 b each comprise four, substantially planar surface portions. - The capacitive channel 50 b follows a
continuous path 60 b around the electrode 18 b and preferably has a line ofsymmetry 64 b that is substantially parallel with the drive direction (i.e., X direction) of the resonant member 12 (For the purposes of this disclosure, a line of symmetry for a capacitive channel is “substantially parallel” to the drive direction if the line of symmetry and drive direction are 1 degrees or less from parallel, and preferably 0.1 degrees or less from parallel, and more preferably 0.01 degrees or less from parallel. In some examples, the capacitive channel 50 b can have additional lines of symmetry that are, for example, perpendicular to the line ofsymmetry 64 b. - To enable such symmetry of the capacitive channel 50 b, the
continuous path 60 b of the capacitive channel 50 b is preferably symmetric in shape, and the capacitive channel 50 b preferably has a width w (measured as the distance between capacitive surfaces 52 b, 54 b) that is substantially constant along thecontinuous path 60 b of the capacitive channel 50 b. For the purposes of this disclosure, a width of a capacitive channel is substantially constant along a given path if a maximum variance of the width is 7% or less, and preferably 1% or less, and more preferably 0.5% or less. For instance, a maximum variance of the width in some examples can be 20 nm or less, and preferably 5 nm or less, and more preferably 1 nm or less. - Because the capacitive channel 50 b of the electrode 18 b has a line of
symmetry 64 b that is substantially parallel with the drive direction X of the electrode 18 b, across-sectional area 70 b′ of the capacitive channel 50 b on one side of the line ofsymmetry 64 b will be substantially equal to across-sectional area 70 b″ of the capacitive channel 50 b on an opposite side of the line ofsymmetry 64 b (thecross-sectional areas 70 b′, 70 b “being taken along the X-Y plane). Moreover, thesecross-sectional areas 70 b”, 70 b″ will remain substantially equal to each other as theresonant member 12 moves in the drive direction X in drive mode. Thus, capacitive transduction of sense mode current that would normally be caused by a difference incross-sectional areas 70 b′, 70 b″ is zero, and the ZRO effect described above can be prevented. - Moreover, as noted above, the fabrication process that is commonly used to form capacitive channels between electrodes and a resonant member in a sensor device can form imperfections in the capacitive surface portions at the ends of the channel. However, because the capacitive channel 50 b in the present embodiment is a continuous channel that circumscribes the electrode 18 b, there are no end portions of the capacitive channel 50 b that are likely to cause imperfections in the capacitive surfaces 52 b, 54 b of the
main body 36 and electrode 18 b, thereby further preventing the ZRO effect that is caused by asymmetries in a capacitive channel. - It is to be appreciated that the structure described above with respect to the sense electrode 18 b,
aperture 44 b, and capacitive channel 50 b shown inFIG. 2 can be similarly applied to the other electrodes 18 of thesensing device 10. Such structure can similarly prevent the ZRO effect at those electrodes 18. - As noted above with reference to
FIG. 1 , theresonant member 12 is flexibly supported by theanchor 14 such that theresonant member 12 is movable in two resonant modes—the drive mode and sense mode. U.S. Patent Application Publication No. 2016/0327390, which is incorporated herein by reference in its entirety, discloses various example structures (referred to as “decoupling mechanisms”) for flexibly supporting a resonant member relative to a substrate that can be applied to thesensing device 10 of the present disclosure. These structures are referred to as “decoupling mechanisms” because they attach the resonant member to a support structure (e.g., anchor) such that the resonant Member is flexibly supported while mitigating energy transfer (i.e., energy loss) of the resonant member to the anchor. Such energy transfer can get coupled to another mode (e.g., sense mode) from the resonant member and further cause the ZRO effect described above. - One specific example of a
decoupling mechanism 80 is illustrated inFIG. 3 of the present disclosure, which includes aflange 82 that circumscribes and is directly connected to theanchor 14 of thesensing device 10 described above. Thedecoupling mechanism 80 further includes a plurality ring portions 84 including afirst ring portion 84 a that circumscribes and is radially spaced from theflange 82, asecond ring portion 84 b that circumscribes and is radially spaced from thefirst ring portion 84 a, and athird ring portion 84 c that circumscribes and is radially spaced from thesecond ring portion 84 b. Thethird ring portion 84 c is circumscribed by themain body 36 of theresonant member 12 such that themain body 36 is radially spaced from thethird ring portion 84 c. - Moreover, the
decoupling mechanism 80 includes a plurality of connecting portions 86 including a plurality of first connectingportions 86 a that connect thefirst ring portion 84 a to theflange 82, a plurality of second connecting portions 86 b that connect thesecond ring portion 84 b to thefirst ring portion 84 a, a plurality of third connectingportions 86 c that connect thethird ring portion 84 c to thesecond ring portion 84 b, and a plurality of fourth connectingportions 86 d that connect thethird ring portion 84 c to themain body 36. - The plurality of connection portions 86 are located about the central axis w of the
anchor 14 such that the first connectingportions 86 a are circumferentially aligned with each other and circumferentially spaced by an angle θ1, the second connecting portions 86 b are circumferentially aligned with each other and circumferentially spaced by the angle θ1, the third connectingportions 86 c are circumferentially aligned with each other and circumferentially spaced by the angle θ1, and the fourth connectingportions 86 d are circumferentially aligned with each other and circumferentially spaced by the angle θ1, wherein the angle θ1 is 22.5 degrees. Additionally, each first connectingportion 86 a is radially aligned with an associated third connectingportion 86 c, and each second connecting portion 86 b is radially aligned with an associated fourth connectingportion 86 d. The first and third connectingportions portions 86 b, 86 d by an angle θ2 that is 12.25 degrees. - The ring portions 84 of the
decoupling mechanism 80 above act as buffer that reduce anchor loss to theanchor 14. It is possible to further reduce energy loss by implementing additional rings 84 and connecting portions 86 that connect the additional rings 84 to the threerings sensing device 10. It has been found that a four-ring design can substantially reduce energy loss while also ensuring that the lowest mode frequency is not too low. -
FIG. 4 illustrates an embodiment of thesensing device 10 wherein theouter periphery 42 of themain body 36 is a circle. In this case, the drive mode executes negligible normal displacement at thesense electrodes 18 b, 18 d. Capacitive transduction of this mode is negligible as electrostatic forces are approximately perpendicular to the resonator boundary. -
FIG. 5 illustrates an embodiment of thesensing device 10 wherein a plurality of release holes 92 are arranged so as to form an equilateral triangle when connecting specific three release holes 92. - This application has been described with reference to the example embodiments described above. Modifications and alterations will occur to others upon a reading and understanding of this specification. Examples embodiments incorporating one or more aspects of the invention are intended to include all such modifications and alterations insofar as they come within the scope of the appended claims.
Claims (22)
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US11614328B2 (en) | 2023-03-28 |
US20220128359A1 (en) | 2022-04-28 |
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