US20160154019A1

US20160154019A1 - Mems gyroscope

Info

Publication number: US20160154019A1
Application number: US14/518,621
Authority: US
Inventors: Biao Zhang; Tao Ju
Original assignee: INSIGHTECH LLC
Current assignee: INSIGHTECH LLC
Priority date: 2012-07-27
Filing date: 2014-10-20
Publication date: 2016-06-02
Also published as: US20140190257A1; US10012670B2; US20160153780A1; US20150034620A1; US20150226555A1; US20140026658A1; US20140026660A1; US20160154070A1; US20160154020A1; US20150033856A1; US20150033855A1; US20150033854A1; US20140026659A1; US20140026661A1

Abstract

A MEMS gyroscope is disclosed herein, wherein the MEMS gyroscope comprises a movable portion capable of moving in response to angular velocity, a conducting wire attached to the movable portion for generating magnetic field, and a spintronic device for measuring the magnetic field. The conducting wire is disposed such that the current it carries is substantially perpendicular to the sensing direction of the sensing mode of the proof-mass.

Description

CROSS-REFERENCE

This U.S. utility patent application claims priority from co-pending U.S. utility patent application “A HYBRID MEMS DEVICE,” Ser. No. 13/559,625 filed Jul. 27, 2012, which claims priority from U.S. provisional patent application “A HYBRID MEMS DEVICE,” tiled May 31, 2012, Ser. No. 61/653,408 to Biao Zhang and Tao Ju. This US utility patent application also claims priority from co-pending U.S. utility patent application “A MEMS DEVICE,” Ser. No. 13/854,972 tiled Apr. 2, 2013 to the same inventor of this U.S. utility patent application, the subject matter of each of which is incorporated herein by reference in its entirety.

TECHNICAL FIELD OF THE DISCLOSURE

The technical field of the examples to be disclosed in the following sections is related generally to the art of operation of microstructures, and, more particularly, to operation of MEMS devices comprising MEMS magnetic sensing structures.

BACKGROUND OF THE DISCLOSURE

Microstructures, such as microelectromechanical (hereafter MEMS) devices (e.g. accelerometers, DC relay and RF switches, optical cross connects and optical switches, microlenses, reflectors and beam splitters, filters, oscillators and antenna system components, variable capacitors and inductors, switched banks of filters, resonant comb-drives and resonant beams, and micromirror arrays for direct view and projection displays) have many applications in basic signal transduction. For example, a MEMS gyroscope measures angular rate.
A gyroscope (hereafter “gyro” or “gyroscope”) is based on the Coriolis effect as diagrammatically illustrated in FIG. it. Proof-mass 100 is moving with velocity V_d. Under external angular velocity Ω, the Coriolis effect causes movement of the poof-mass (100) with velocity V_s. With fixed V_d, the external angular velocity can be measured from V_d. A typical example based on the theory shown in FIG. 1 is capacitive MEMS gyroscope, as diagrammatically illustrated in FIG. 2,
The MEMS gyro is a typical capacitive MEMS gyro, which has been widely studied. Regardless of various structural variations, the capacitive MEMS gyro in FIG. 2 includes the very basic theory based on which all other variations are built. In this typical structure, capacitive MEMS gyro 102 is comprised of proof-mass 100, driving mode 104, and sensing mode 102. The driving mode (104) causes the proof-mass (100) to move in a predefined direction, and such movement is often in a form of resonance vibration. Under external angular rotation, the proof-rnass (100) also moves along the V_sdirection with velocity V_s. Such movement of V_sis detected by the capacitor structure of the sensing mode (102). Both of the driving and sensing modes use capacitive structures, whereas the capacitive structure of the driving mode changes the overlaps of the capacitors, and the capacitive structure of the sensing mode changes the gaps of the capacitors.
Current capacitive MEMS gyros, however, are hard to achieve submicro-g/rtHz because the capacitance between sensing electrodes decreases with the miniaturization of the movable structure of the sensing element and the impact of the stray and parasitic capacitance increase at the same time, even with large and high aspect ratio proof-masses.
Therefore, what is desired is a MEMS device capable of sensing angular velocities and methods of operating the same.

SUMMARY OF THE DISCLOSURE

In view of the foregoing, a MEMS gyroscope is disclosed herein, wherein the gyroscope comprises: a first substrate, comprising: a movable portion that is capable of moving in response to an angular velocity; a driving mechanism associated with said movable portion for moving the movable portion along a driving direction in a driving mode; a conducting wire of a magnetic source on the movable portion for generating magnetic field; and a second substrate, comprising: a magnetic sensor that is a spintronic device for measuring the magnetic field from the conducting wire, wherein the magnetic sensor has an easy axis and hard axis; wherein the hard axis is substantially parallel to a sensing direction of a sensing mode of the movable portion; and wherein the conducting wire is disposed such that the current it carries is substantially perpendicular to the sensing direction of the sensing mode of the (proof-mass,

BRIEF DESCRIPTION OF DRAWINGS

FIG. 1 diagrammatically illustrates the Coriolis effect in a MEMS structure;

FIG. 2 is a top view of a typical existing capacitive MEMS gyroscope having a driving mode and a sensing mode, wherein both of the driving and sensing mode utilize capacitance structures;

FIG. 3 illustrates an exemplary MEMS gyroscope having a magnetic sensing mechanism;

FIG. 4 illustrates a top view of a portion of an exemplary implementation of the MEMS gyroscope illustrated in FIG. 3, wherein the MEMS gyroscope illustrated in FIG. 4 having a capacitive driving mode and a magnetic sensing mechanism;

FIG. 5 illustrates a perspective view of a portion of another exemplary implementation of the MEMS gyroscope illustrated in FIG. 3, wherein the MEMS gyroscope illustrated in FIG. 5 having a magnetic driving mechanism for the driving mode and a magnetic sensing mechanism for the sensing mode

FIG. 6 illustrates an exemplary magnetic driving mechanism of the MEMS gyroscope in FIG. 5;

FIG. 7 illustrates an exemplary magnetic source of the MEMS gyroscope illustrated in FIG. 3;

FIG. 8 illustrates an exemplary magnetic sensing mechanism that can be used in the MEMS gyroscope illustrated in FIG. 3;

FIG. 9 shows an exemplary thin-film stack that can be configured into a CIP or CPP structure for use in the magnetic sensing mechanism illustrated in FIG. 8;

FIG. 10 illustrates an exemplary MEMS gyroscope that comprises multiple magnetic sensing structures;

FIG. 11 illustrates an exemplary MEMS gyroscope that comprises multiple proof-masses;

FIG. 12 illustrates an exemplary MEMS gyroscope that comprises multiple proof-masses having magnetic driving mechanisms;

FIG. 13a and FIG. 13b illustrate an exemplary driving scheme for use in the MEMS gyroscope illustrated in FIG. 12;

FIG. 14 illustrates an exemplary magnetic source and magnetic sensing mechanism of the MEMS gyroscope illustrated in FIG. 13;

FIG. 15 illustrates another exemplary MEMS gyroscope that comprises multiple proof-masses having capacitive driving mechanisms;

FIG. 16a to FIG. 16d illustrate yet another exemplary MEMS gyroscope comprising multiple proof-masses and multiple magnetic sources in at least one of the proof-masses; and

FIG. 17 illustrates yet another exemplary MEMS gyroscope comprising multiple proof-masses, multiple magnetic sources in at least one of the proof-masses, and a reference magnetic sensor for the multiple magnetic sensors.

DETAILED DESCRIPTION OF SELECTED EXAMPLES

Disclosed herein is a MEMS gyroscope for sensing an angular velocity, wherein the MEMS gyroscope utilizes a magnetic sensing mechanism. It will be appreciated by those skilled in the art that the following discussion is for demonstration purposes, and should not be interpreted as a limitation. Many other variations within the scope of the following disclosure are also applicable. For example, the MEMS gyroscope and the method disclosed in the following are applicable for use in accelerometers.
Referring to FIG. 3, an exemplary MEMS gyroscope is illustrated herein, In this example, MEMS gyroscope 106 comprises magnetic sensing mechanism 114 for sensing the target angular velocity through the measurement of proof-mass 112, Specifically, MEMS gyroscope 106 comprises mass-substrate 108 and sensor substrate 110. Mass-substrate 108 comprises proof-mass 112 that is capable of responding to an angular velocity, The two substrates (108 and 110) are spaced apart, for example, by a pillar (not shown herein for simplicity) such that at least the proof-mass (112) is movable in response to an angular velocity under the Coriolis effect. The movement of the proof-mass (112) and thus the target angular velocity can be measured by magnetic sensing mechanism 114.
The magnetic sensing mechanism (114) in this example comprises a magnetic source 116 and magnetic sensor 118. The magnetic source (116) generates a magnetic field, and the magnetic sensor (118) detects the magnetic field and/or the magnetic field variations that is generated by the magnetic source (116). In the example illustrated herein in RUG. 3, the magnetic source is placed on/in the proof-mass (112) and moves with the proof-mass (112), The magnetic sensor (118) is placed on/in the sensor substrate (120) and non-movable relative to the moving proof-mass (112) and the magnetic source (116). With this configuration, the movement of the proof-mass 12) can be measured from the measurement of the magnetic field from the magnetic source (116).
Other than placing the magnetic source on/in the movable proof-mass (1112), the magnetic source (116) can be placed on in the sensor substrate (120); and the magnetic sensor (118) can be placed on/ in the proof-mass (112).
It is also noted that the MEMS gyroscope illustrated in FIG. 3 can also be used as an accelerometer.
The MEMS gyroscope as discussed above with reference to FIG. 3 can be implemented in many ways, one of which is illustrated in FIG. 4. Referring to FIG. 4, the proof-mass (120) is driven by capacitive, such. as capacitive comb. The sensing mode, however, is performed using the magnetic sensing mechanism illustrated in FIG. 3. For this reason, capacitive combs can be absent from the proof-mass (120).
Alternatively, the proof-mass can be driven by magnetic force, an example of which is illustrated in FIG. 5. Referring to FIG. 5, the mass substrate (108) comprises a movable proof-mass (126) that is supported by flexible structures such as flexures 128, 129, and 130. The layout of the flexures enables the proof-mass to move in a plane substantially parallel to the major planes of mass substrate 108. In particular, the flexures enables the proof-mass to move along the length. and the width. directions, wherein the length direction can. be the driving mode direction and the width direction can be the sensing mode direction of the MEMS gyro device. The proof-mass (126) is connected to frame 132 through flexures (128, 129, and 130). The frame (132) is anchored by non-movable structures such as pillar 134. The mass-substrate (108) and sensing substrate 110 are spaced apart by the pillar (134). The proof-mass (112.) in this example is driving by a magnetic driving mechanism (136). Specifically, the proof-mass (126) can move (e.g. vibrate) in the driving mode under magnetic force applied by magnetic driving mechanism 136, which is better illustrated in FIG. 6.
Referring to FIG. 6, the magnetic driving mechanism 136 comprise a magnet core 138 surrounded by coil 140. By applying an alternating current through coil 140, an alternating magnetic field can be generated from the coil 140. The alternating magnetic field applies magnetic force to the magnet core 140 so as to move the magnet core. The magnet core thus moves the proof-mass.
The magnetic source (114) of the MEMS gyroscope (106) illustrated in FIG. 3 can be implemented in many ways, one of which is illustrated in FIG. 7. Referring to FIG. 7, conductive wire 142 is displaced on/in proof-mass 112. In one example, conductive wire 142 can be placed on the lower surface of the proof-mass (112), wherein the lower surface is facing the magnetic sensors (118 in FIG. 3) on the sensor substrate (110, in FIG. 3). Alternatively, the conductive wire (142) can be placed on the top surface of the proof-mass (112), i.e. on the opposite side of the proof-mass (112) in view of the magnetic sensor (118). In another example, the conductive wire (142) can be placed inside the proof-mass, e.g. laminated or embedded inside the proof-mass (112), which will not be detailed herein as those examples are obvious to those skilled in the art of the related technical field.
The conductive wire (142) can be implemented in many suitable ways, one of which is illustrated in FIG, 7. In this example, the conductive wire (142) comprises a center conductive segment 146 and tapered contacts 144 and 148 that extend the central conductive segment to terminals, through the terminals of which current can be driven through the central segment. The conductive wire (142.) may have other configurations. For example, the contact tapered contacts (144 and 148) and the central segment (146) maybe U-shaped such that the tapered contacts may be substantially parallel but are substantially perpendicular to the central segment, which is not shown for its obviousness.
The magnetic sensor 18) illustrated in FIG. 3 can be implemented to comprise a reference sensor (150) and a signal sensor (152) as illustrated in FIG. 8. Referring to FIG. 8, magnetic senor 118 on/in sensor substrate 120 comprises reference sensor 150 and signal sensor 152. The reference sensor (150) can be designated for dynamically measuring the magnetic signal background in which the target magnetic signal (e.g. the magnetic field from the conductive wire 146 as illustrated in FIG. 7) co-exists. The signal sensor (152) can be designated for dynamically measuring the target magnetic signal (e.g. the magnetic field from the conductive wire 146 as illustrated in FIG. 7). In other examples, the signal sensor (152) can he designated for dynamically measuring the magnetic signal background in which the target magnetic signal (e.g. the magnetic field from the conductive wire 146 as illustrated in FIG. 7) co-exists, while the signal sensor (150) can be designated for dynamically measuring the target magnetic signal (e.g. the magnetic field from the conductive wire 146 as illustrated in FIG. 7).
The reference sensor (150) and the signal sensor (152) preferably comprise magneto-resistors, such as AMRs, giant-magneto-resistors (such as spin-valves, hereafter SV), or tunneling-magneto-resistors (TMR). For demonstration purpose, FIG. 9 illustrates a magneto-resistor structure, which can be configured into CIP (current-in-plane, such as a spin-valve) or a CPP (current-perpendicular-to-plane, such as TMR structure), As illustrated in FIG. 9, the magneto-resistor stack comprises top pin-layer 154, free-layer 156, spacer 158, reference layer 160, bottom pin layer 162, and substrate 120. Top pin layer 154 is provided for magnetically pinning free layer 156. The top pin layer can be comprised of IrMn, PtMn nr other suitable magnetic materials. The free layer (156) can be comprised of a ferromagnetic material, such as NiFe, CoFe, CoFeB, or other suitable materials or the combinations thereof. The spacer (158) can be comprised of a non-magnetic conductive material, such as Cu, or an oxide material, such as Al₂O₃or MgO or other suitable materials. The reference layer (160) can be comprised of a ferromagnetic magnetic material, such as NiFe, CoFe, CoFeB, or other materials or the combinations thereof. The bottom pin layer (162) is provided for magnetic pinning the reference layer (160), which can be comprised of a IrMn, PtMn or other suitable materials or the combinations thereof The substrate (120) can be comprised of any suitable materials, such as glass, silicon, or other materials or the combinations thereof.
In examples wherein the spacer (158) is comprised of a non-magnetic conductive layer, such as Cu, the magneto-resistor (118) stack can be configured into a CIP structure (i.e. spin-valve, SV), wherein the current is driven in the plane of the stack layers. When the spacer 58) is comprised of an oxide such as Al₂O₃, MgO or the like, the magneto-resistor stack (118) can be configured into a CPP structure (i.e. TMR), wherein the current is driven perpendicularly to the stack layers.
In the example as illustrated in FIG. 9, the free layer (156) is magnetically pinned by the top pin layer (154), and the reference layer (160) is also magnetically pinned by bottom pin layer 162. The top pin layer (15.4) and the bottom pin layer (162) preferably having different blocking temperatures. In this specification, a blocking temperature is referred to as the temperature, above which the magnetic pin layer is magnetically decoupled with the associated pinned magnetic layer. For example, the top pin layer (154) is magnetically decoupled with the free layer (156) above the blocking temperature T_Bof the top pin layer (154) such that the free layer (156) is “freed” from the magnetic pinning of top pin layer (154). Equal to or below the blocking temperature T_Bof the top pin layer (154), the free layer (156) is magnetically pinned by the top pin layer (154) such that the magnetic orientation of the free layer (156) is substantially not affected by the external magnetic field. Similarly, the bottom pin layer (162) is magnetically decoupled with the reference layer (160) above the blocking temperature T_Bof the bottom pin layer (162) such that the reference layer (160) is “freed” from the magnetic pinning of bottom pin layer (162). Equal to or below the blocking temperature T_Bof the bottom pin layer 62), the reference layer (160) is magnetically pinned by the bottom pin layer (162) such that the magnetic orientation of the reference layer (162) is substantially not affected by the external magnetic field.
The top and bottom pin layers (154 and 162, respectively) preferably have different blocking temperatures. When the free layer (156 is “freed” from being pinned by the top pin layer (154), the reference layer (160) preferably remains being pinned by the bottom pin layer (162). Alternatively, when the free layer (156) is still pinned by the top pin layer (154), the reference layer (160) can be “freed” from being pinned by the bottom pin layer (162). In the later example, the reference layer (160) can be used as a “sensing layer” for responding to the external magnetic field such as the target magnetic field, while the free layer (156) is used as a reference layer to provide a reference magnetic orientation,
The different blocking temperatures can be accomplished by using different magnetic materials for the top pin layer (154) and bottom pin layer (162). In one example, the top pin layer (154) can be comprised of IrMn, while the bottom pin layer (162) can be comprised of PtMn, vice versa. In another example, both of the top and bottom pin layers (154 and 162) may be comprised of the same material, such as IrMn or PtMn, but with different thicknesses such that they have different blocking temperatures.
It is noted by those skilled in the art that the magneto-resistor stack (118) is configured into sensors for sensing magnetic signals. As such, the magnetic orientations of the free layer (156) and the reference layer (160) are substantially perpendicular at the initial state. Other layers, such as protective layer Ta, seed layers for growing the stack layers on substrate 120 can be provided. It is further noted that the magnetic stack layers (118) illustrated in FIG. 9 are what is often referred to as “bottom pin” configuration in the field of art. In other examples, the stack can be configured into what is often referred as “top pinned” configuration in the field of art, which will not be detailed herein.
in some applications, multiple magnetic sensing mechanisms can be provided, an example of which is illustrated in FIG. 10. Referring to FIG. 10, magnetic sensing mechanisms 116 and 164 are provided fur detecting the movements of proof-mass 112. The multiple magnetic sensing mechanisms can be used for detecting the movements of proof-mass 112 in driving mode and sensing mode respectively. Alternatively, the multiple magnetic sensing mechanisms 116 and 164 can be provided for detecting the same modes (e.g. the driving mode and/or the sensing mode).
In operation, angular velocity in Z direction (perpendicular to the driving and sensing direction) causes the motion of the proof-mass in the sensing direction. However, acceleration in the sensing direction also causes the motion of the proof-mass in the sensing direction. As a consequence, motion of the proof-mass in the sensing direction is a mixture of both of the angular velocity in the Z direction and acceleration in the sensing direction when both exist. The signal measured by the magnetic sensing mechanism is thus a mixture of the signals associated with the proof-mass motion in both directions. A solution to separate signals from the angular velocity in Z direction and acceleration in the sensing direction can be provision of multiple proof-masses, an example of which is illustrated in FIG. 11. It is noted that the example illustrated in FIG. 11 having two proof-masses is only for demonstration purposes. Other variations within the scope of this disclosure are also applicable. For example, more than two proof-masses, such as four or eight proof-masses can be provided in a MEMS gyroscope.
Referring to FIG. 11, proof-masses PM1 170 and PM2 172 are provided in a MEMS gyroscope, The proof-masses (170 and 172) are connected to anchor 115 through flexures 111 and 113 such that the proof-masses are capable of moving in the driving and sensing directions. It is noted that the proof-masses 170 and 172) are associated with other mechanical structures to enable the motion of the proof-masses, and those mechanical structures are not shown herein for simplicity. Driving mechanisms 117 and 119 are provided for driving the proof-masses (170 and 172) in their driving modes. The driving mechanisms may comprise capacitors or magnetic driving mechanisms or other suitable structures.
To separate the angular velocity in the Z direction and acceleration in the sensing direction, the proof-masses PM1 and PM2 move in opposite directions along the driving directions. For example, the proof-masses PM1 and PM2 move at the same time toward anchor 115 or at the same time, away from anchor 115. Because the proof-masses PM1 and PM2 have opposite velocities in the driving direction, they also move in opposite directions in the sensing direction under the Coriolis force due to angular velocity in the Z direction. In existence of accelerate in the sensing direction, both of the proof- masses 170 and 172 move in the same direction at the same time. By analyzing the moving directions of the proof- masses 170 and 172, signals caused by the angular velocity in the Z direction and acceleration in the sensing direction can be separated.
As an example, FIG. 12 illustrates the MEMS substrate of a MEMS gyroscope having multiple proof-masses and using magnetic driving mechanism. Referring to FIG. 12, proof- masses 170 and 172 are formed in MEMS substrate 108. The proof- masses 170 and 172 are connected to and held by anchor 115 through flexures. The proof- masses 170 and 172 each are connected to a magnetic driving mechanism. For example, proof-mass 170 is connected to movable coil 123 that moves with proof-mass 170. Movable coil 123 is coupled to static coil 121 that is affixed to anchor 125 such that static coil 121 does not move relative to substrate 108 when proof- masses 170 and 172 are moving,
By driving current in the coupled coils in selected directions, the coils generate attractive and repel forces, as illustrated in FIG. 13a and FIG. 13b . Referring to FIG. 13 a, the direction of the current through movable coil 123 can be fixed, for example counter-clockwise. When the current in static coil 121 has a clockwise direction, the coils 121 and 123 generate attractive force. Because the static coil (121) is affixed to anchor 125 and static, the movable coil (123) is moves towards the static coil (121) under the attractive force, and so does the proof-mass (170). When both of the current in the static coil (121) and movable coil (123) have counter-clockwise direction, as illustrated in FIG. 13 bc, the force between the two coils is repellent. The movable coil (123), on does the proof-mass (170), moves away from the static coil (121) under the repellent force.
By changing the direction of the current in the static coil white keeping the current direction in the movable coil unchanged, the proof-mass (170) can be moved towards and away from the static coil (121). In other examples, the current direction of the static coil (121) can be unchanged during operation, while the direction of the current in the movable coil (123) is varied. In another example, both of the directions of the current in the static and movable loops can be varied during operation to driving the movable loop, as well as the proof-mass, away and towards the anchor (125). In any examples, the frequency of changing the current direction can be equal or close to the resonate frequency of the proof-mass in the driving direction, It is noted that multiple static and movable loop pairs can be provided for a proof-mass to increase the driving efficiency, even though FIG. 4a shows two coil pairs.
Proof-mass 172 can be driving in the same way as proof-mass 170 by using the magnetic driving mechanism associated therewith. In order to separate signal of the Z direction angular velocity from the acceleration in the sensing direction, proof- masses 170 and 172 are driving in opposite directions in the sensing mode as discussed above with reference to FIG. 11, which will not be repeated herein.
For detecting the motion of the proof-masses (170 and 172), multiple magnetic sensing mechanisms are provided, and example of which is illustrated in FIG. 14. Referring to FIG. 14, Proof-mass 170 is provided with a conducting wire (174) as a magnetic field source for generating magnetic field. The conducting wire (174) can be formed at the bottom surface of proof-mass 170 as discussed above with reference to FIG. 3, Associated with conducting wire 170 is magnetic sensor 176 for measuring the magnetic field from conducting wire 174, The magnetic sensor (176) is formed on sensor substrate 110 as shown in FIG. 3. The magnetic sensor 176 can be the same as magnetic sensor 118 as discussed above with reference to FIG. 3. It is noted that magnetic sensor 176, when comprised of a solid-state spintronic structure, such as a spin-valve or magnetic-tunnel-junction, can be offset from conducting wire 174 along the direction of the sensing mode. Specifically, the geometric center of magnetic sensor 176 is offset from the closest conducting wire passing by. Similar to that for proof-mass 170, proof-mass 172 is provided with conducting wire 178 and associated sensing mechanism 180, which will not be repeated herein.
In yet another example, the MEMS gyroscope as discussed above with reference to FIG. 3 can have multiple proof-masses and capacitive driving mechanisms, an example of which is illustrated in FIG. 15. Referring to FIG. 15, proof- masses 170 and 172 are provided. The proof-masses are driven by capacitive combs. For example, proof-mass 170 is connected to one set of capacitive plates of a capacitor comb; and the other set of capacitor plates 10 are connected to anchor 127. By changing the voltage between the capacitive plates, electrostatic force can be generated, The electrostatic force drives proof-mass 170 to move in the driving direction.
Similar to proof-mass 170, proof-mass 172 is also connected to a set of capacitor plates; and the other set of capacitor plates of a capacitor comb is connected to an anchor. By changing the voltages between the plates, proof-mass 172 can be moved under electrostatic force caused by the variation of the voltage.
The same to that in magnetic driving scheme as discussed above with reference to FIG. 14, the capacitor combs associated with proof- masses 170 and 172 are operated asynchronously such that proof- masses 170 and 172 move in opposite directions along the driving direction. In response to the same angular velocity in Z direction, proof- masses 170 and 172 move in opposite directions along the sensing direction.
Regardless of driving mechanisms, a proof-mass of a MEMS gyroscope may have multiple magnetic sources, an example of which is illustrated in FIG. 16a . Referring to FIG. 16a , the MEMS gyroscope comprises proof- masses 170 and 172. At least one of the proof- masses 170 and 172 comprises multiple magnetic sources. For example, proof-mass 170 is attached thereto conducting wires 14, 24 and 16, each of which is capable of generating magnetic field. The conducting wires can be serially connected as shown in FIG. 16a . Associated with each conducting wire, a magnetic sensor is provided but on the sensor substrate, which is illustrated as blocks with dotted lines. For example, magnetic sensors 22, 20 and 18 are associated with and aligned to conducting wires 14, 24 and 16 separately. By placing the conducting wires with distances larger than the sensitivity of the magnetic sensors, magnetic field signals from neighboring wires may not be measured by a magnetic sensor.
In operation, current is driven through conducting wires 14, 24 and 16. The current carrying wires generate magnetic field in their vicinities. The magnetic sensors measure the magnetic field from the associated conducting wires. The multiple magnetic source configuration can be of great value especially when multiple magnetic sensors are desired, such as Wheatstone bridge configuration.
It is noted that the magnetic sensors (18, 20, and 22) are aligned to the conducting wires 14, 24 and 16 in terms of the magnetic field generated by the conducting wires. Taking magnetic sensor 22 for example as illustrated in FIG. 16b , magnetic sensor 22, which can be a spin-valve or a magnetic-tunnel-junction (MTJ) or other spintronic devices, has an (magnetic) easy axis along its length and (magnetic) hard axis along its width, wherein the easy and hard axes are often perpendicular. The easy axis of magnetic sensor 22 is substantially parallel to the driving direction (the direction of the driving mode); and the hard axis is substantially parallel to the sensing direction (direction of the sensing mode).
The conducting wire 14 is disposed such that the current it carries flows along the direction of the driving mode. The direction of the current is perpendicular to the hard axis of the magnetic sensor 22 that is the sensing direction of the magnetic sensor 22. During operation, current flows through the conducting wire 14, and generates magnetic field. The magnetic field along the driving direction (the direction along the driving mode) is substantially uniform especially when the conducting wire has a length that is much larger than the magnetic sensor, which is illustrated in FIG. 16c , Because of this uniformity, the magnetic field is insensitive to the movement of the conducting wire and the proof-mass. As a consequence, measuring the movement of the proof-mass through the measurement of the magnetic field along the driving direction is difficult.
The magnetic field from the conducting wire 145, however, has a much higher magnetic field gradient along the sensing direction, which is illustrated in FIG. 16d . Higher magnetic field gradient benefits higher sensitivity of measuring the movement of the proof-mass through the measurement of the magnetic field generated by the conducting wire. Therefore, it is preferred that the conducting wire is disposed relative to the magnetic sensor and the proof-mass in a way such that, the current in the conducting wire is substantially perpendicular to the hard axis (also the sensing direction) of the magnetic sensor, and substantially perpendicular to the sensing direction of the sensing mode of the proof-mass.
It will be appreciated by those skilled in the art that the configuration as discussed above with reference to FIG. 6b is also applicable to other MEMS gyroscopes, such as MEMS gyroscopes having one proof-mass, and MEMS gyroscopes having more than two proof-masses, which will not be detailed herein due to their obviousness.
In examples using spintronic magnetic sensors such as spin-valves or magnetic-tunnel-junctions, a reference magnetic sensor is often provided for providing reference signals. The measured magnetic signals from magnetic sensors can be compared with the reference signals followed by amplification. In the example as shown in FIG. 16a , each magnetic sensor (e.g. 22, 20, and 18) can be associated with a reference sensor. The reference sensors are often identical in terms of structures, but are isolated from external magnetic field by being covered by a magnetic insulation layer, such as a soft magnetic material. In yet another example, a reference sensor can be provided for multiple magnetic sensors associated with a proof-mass, as illustrated in FIG. 17.
Referring to FIG. 17, magnetic sensors 18, 20, and 22. are provided for measuring magnetic field from magnetic sources 16, 24, and 14 respectively. The magnetic sources 14, 24, and 16 are attached to proof-mass 170 for measuring movements of proof-mass 170. Reference sensor 26 is provided for magnetic sensors 18, 20, and 22, The reference sensor (26) is substantially the same as magnetic sensors 118, 20, and 22, but is magnetically insulated by being covered with a magnetic insulation layer such that reference sensor 26 is not responsive to external magnetic field.
The measured magnetic signals from magnetic sensors 18, 20, and 22 are compared with the output signal form the reference sensor (26), and the output of the comparison can be amplified. The reference sensor (26) can be placed at any suitable location in the vicinity of the magnetic sensors 18, 20, and 22. In the example as illustrated in FIG. 17, the reference sensor (26) can be placed in the vicinity of magnetic sensor (18). It is noted by those skilled in the art that even though a reference sensor is provided for a proof-mass, such as proof-mass 170, other proof-masses, such as proof-mass 172 may or may not be provided with a reference sensor.
It will be appreciated by those of skilled in the art that a new and useful MEMS gyroscope has been described herein. In view of the many possible embodiments, however, it should be recognized that the embodiments described herein with respect to the drawing figures are meant to be illustrative only and should not be taken as limiting the scope of what is claimed. Those of skill in the art will recognize that the illustrated embodiments can be modified in arrangement and detail. Therefore, the devices and methods as described herein contemplate all such embodiments as may come within the scope of the following claims and equivalents thereof. In the claims, only elements denoted by the words “means for” are intended to be interpreted as means plus function claims under 35 U.S.C. §112, the sixth paragraph.

Claims

We claim:

1. A MEMS gyroscope, comprising:

a first substrate, comprising:

a movable portion that is capable of moving in response to an angular velocity;

a driving mechanism associated with said movable portion for moving the movable portion along a driving direction in a driving mode;

a conducting wire of a magnetic source on the movable portion for generating magnetic field; and

a second substrate, comprising:

a magnetic sensor that is a spintronic device for measuring the magnetic field from the conducting wire,

wherein the magnetic sensor has an easy axis and hard axis;

wherein the hard axis is substantially parallel to a sensing direction of a sensing mode of the movable portion; and

wherein the conducting wire is disposed such that the current it carries is substantially perpendicular to the sensing direction of the sensing mode of the proof-mass.

2. The MEMS gyroscope of claim 1, wherein the spintronic device comprises a spin-valve.

3. The MEMS gyroscope of claim 1, wherein the spintronic device comprises a tunnel-magnetic-resistor.

4. The MEMS gyroscope of claim 1, wherein the driving mechanism comprises a group of capacitors.

5. The MEMS gyroscope of claim 1, wherein the driving mechanism comprises a magnetic driving mechanism.