WO2008018347A2 - Angular velocity sensor - Google Patents
Angular velocity sensor Download PDFInfo
- Publication number
- WO2008018347A2 WO2008018347A2 PCT/JP2007/065108 JP2007065108W WO2008018347A2 WO 2008018347 A2 WO2008018347 A2 WO 2008018347A2 JP 2007065108 W JP2007065108 W JP 2007065108W WO 2008018347 A2 WO2008018347 A2 WO 2008018347A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- vibrator
- detection
- angular velocity
- vibration
- rotation axis
- Prior art date
Links
- 238000001514 detection method Methods 0.000 claims abstract description 315
- 238000006073 displacement reaction Methods 0.000 claims abstract description 19
- 230000007935 neutral effect Effects 0.000 claims description 2
- 230000035945 sensitivity Effects 0.000 description 26
- 239000000758 substrate Substances 0.000 description 22
- 238000013016 damping Methods 0.000 description 21
- 230000000694 effects Effects 0.000 description 8
- 230000015556 catabolic process Effects 0.000 description 5
- 238000006731 degradation reaction Methods 0.000 description 5
- 229910052710 silicon Inorganic materials 0.000 description 5
- 239000010703 silicon Substances 0.000 description 5
- 230000008859 change Effects 0.000 description 3
- 230000000593 degrading effect Effects 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 238000005339 levitation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
Classifications
-
- 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
-
- 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
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L29/00—Semiconductor devices specially adapted for rectifying, amplifying, oscillating or switching and having potential barriers; Capacitors or resistors having potential barriers, e.g. a PN-junction depletion layer or carrier concentration layer; Details of semiconductor bodies or of electrodes thereof ; Multistep manufacturing processes therefor
- H01L29/66—Types of semiconductor device ; Multistep manufacturing processes therefor
- H01L29/84—Types of semiconductor device ; Multistep manufacturing processes therefor controllable by variation of applied mechanical force, e.g. of pressure
Definitions
- the present invention relates to a sensor for detecting an angular velocity.
- the vibration type angular velocity sensor employs a system in which a Coriolis force (also referred to as “deflecting force”; hereinafter, referred to as "Coriolis force”) generated when an angular velocity, which is an object to be detected, is input to the sensor from an outside, is detected as a displacement of vibration of a vibrator, while the vibrator is allowed to generate reference vibration with a predetermined amplitude.
- a direction of the Coriolis force is determined by a direction of the reference vibration and by a direction of the angular velocity.
- the vibrator have a structure in which the vibrator can easily generate vibration in the direction of the reference vibration and also in the direction of the Coriolis force (detecting direction) .
- a so-called double frame system in which a vibrator for reference vibration (reference vibration) and a vibrator for detection (detection vibrator) are separately provided.
- Japanese Patent No. 3,336,730 discloses a structure, as one mode of the angular velocity sensor of the double frame system, in which the detection vibrator is supported by the reference vibrator, and a detection unit for detecting a relative displacement between the reference vibrator and the detection vibrator is provided. Accordingly, such a problem is alleviated that a component of the vibration of the reference vibrator which is generated in the detecting direction is superimposed with a detection signal of the detection unit.
- US Patent No. 6,374,672 discloses a structure in which an inclination of the detection vibrator corresponding to the angular velocity is detected by allowing a doughnut-type reference vibrator, which supports the disc-like detection vibrator, to generate reciprocating rotational vibration. As a result, such a problem is alleviated that degradation of the accuracy of the detection signal which is caused by the vibration of the detection vibrator due to the vibration of the reference vibrator.
- a displacement amount of the detection vibrator for detecting the angular velocity is generally only about one of many hundreds to one of many thousands of a displacement amount of the reference vibration of the reference vibrator. For this reason, it is necessary to detect a small motion of the detection vibrator in a large motion of the reference vibrator. Accordingly, when a noise component (e.g., vibration caused in a direction different from the direction of the reference vibration) of the vibration is generated by the reference vibration, the noise component is detected by the detection unit. In a case where the angular velocity detection is performed with high accuracy, the noise component may be a major factor of degradation of the accuracy in detection of the angular velocity.
- the ' reference vibrator has asymmetric properties caused by an error of a processing accuracy in a manufacturing process, with respect to a structure of the reference vibrator, a structure of a member for supporting the reference vibrator, a drive force applied by a drive unit of the reference vibrator, and the like.
- the reference vibrator " generates vibration with a wobbling component in a direction other than a predetermined direction of the reference vibration. The same is applied to the angular velocity sensor of the double frame system;
- Causes of the noise generated by the reference vibration can be roughly classified into the following two causes. That is: (1) vibration itself of the reference vibration is detected as a detection signal in error by the detection unit; (2) vibration of the detection vibrator excited by the reference vibration (for example, also when an angular velocity ⁇ is not input) is detected as a detection signal in error by the detection unit.
- FIGS. 7B and 7C are a vibrating body 10 for reference and a vibrating body 16 for detection, and the angular velocity is detected by a detection unit 15 based on a change of a relative position between the vibrating body 10 for reference and the vibrating body 16 for detection.
- FIG. 7C is a cross-sectional view taken along the line 7C-7C of FIG. 7B.
- the detection unit 15 detects the relative position between the vibrating body for reference and the vibrating body for detection. Accordingly, the noise is hardly generated in the detection signal. In other words, the noise due to the above-mentioned cause (1) can be reduced.
- the vibrating body 16 for detection is supported by a structure in which, the vibration toward the detecting direction (X- axis direction of FIG. 7B) is easily generated. Accordingly, when the reference vibration with a direction of linear reciprocating vibration in plane with the detecting direction has a component of the linear reciprocating vibration toward the detecting direction, small vibration (noise component of vibration) may be generated in the vibrating body for detection even in a case where the angular velocity is not input. As a result, in a case where the angular velocity is detected with high accuracy, the small noise generated in the detection signal by the above- mentioned cause (2) may degrade the detection accuracy.
- the angular velocity sensor disclosed in US Patent No. 6,374,672 has a structure in which a reference vibrator 76 has a rotation axis perpendicular to a substrate 68, and a detection vibrator 70 has rotation axes 72 and 74 parallel to the substrate 68, thereby performing a reciprocating rotational motion about each of rotation axes as a center.
- the reference vibrator and the detection vibrator perform the reciprocating rotational motion about the difference rotation axes. Accordingly, the vibration of the noise component of the detection vibrator 70 is hardly transmitted, thereby making it difficult to generate the vibration " of the noise component of the detection vibrator 70.
- an effect of the reference vibration on the detection vibrator can be reduced to a large • extent . In other words, the noise due to the above-mentioned cause (2) can be reduced.
- the detection unit detects an electrostatic capacity between a pair of semicircular detection electrodes (not shown) , which are provided on a side of a substrate (bonded to the substrate 68) fixed to the both vibrators, and the detection vibrator 70 opposing to the pair of electrodes.
- a positional relationship between the fixed substrate and the detection vibrator 70 can be detected.
- the reference vibrator 76 generates reciprocating rotational vibration deviating from the rotation axis, or in a case where the reference vibrator 76 has a motion component with inclination with respect to the fixed substrate, even when the detection vibrator 70 is not oscillated, a relationship between opposing areas of the reference vibrator 76 and the pair of semicircular detection electrodes is changed. For this reason, by the above- mentioned cause (1) , the small noise may be generated in the detection signal. Thus, when the angular velocity is detected with high accuracy, the small noise due to the above-mentioned cause (1) may degrade the detection accuracy.
- the rotation axes 72 and 74 are deviated by the reference vibration of the reference vibrator 76.
- the rotation axis of the detection vibrator 70 is deviated from a parallel line which separates the pair of semicircular detection electrodes provided on i:he fixed substrate side.
- the wobbling component of the reference vibrator 76 may be mixed in the inclination component of the detection vibrator 70 which is detected by the detection unit. This may become a cause of degradation of the detection accuracy in the case where the angular velocity is detected with high accuracy (one reason for the above-mentioned cause (1) )
- an angular velocity sensor including: a reference vibrator supported so as to generate reciprocating rotational vibration about a first rotation axis as a center; a detection vibrator supported by the reference vibrator so as to generate reciprocating rotational vibration about a second rotation axis, which is different from the first rotation axis, as a center; a reference vibration generating unit for allowing the reference vibrator to generate .reciprocating rotational vibration; and a detection unit for detecting a displacement amount of the detection vibrator with respect to the reference vibrator, which is in association with the reciprocating rotational vibration of the detection vibrator.
- FIGS. IA and IB are exploded perspective views for illustrating an angular velocity sensor according to Example 1 of the present invention.
- FIGS. 2A, 2B, and 2C are exploded perspective views for illustrating an angular velocity sensor according to Example 2. of the present invention.
- FIGS. 3A and 3B are exploded perspective views for illustrating an angular velocity sensor according to Example 3 of the present invention.
- FIGS. 4A, 4B, and 4C are exploded perspective views for illustrating an angular velocity sensor according to Example 4 of the present invention.
- FIGS. 5A.and 5B are exploded perspective views for illustrating an angular velocity sensor according to Example 5 of the present invention.
- FIG. 6 is a cross-sectional view for illustrating a cross-section of a support member of a detection vibrator according to Example 5 of the present invention.
- FIGS. 7A, IB, and 7C are views for illustrating a conventional angular velocity sensor.
- An angular velocity sensor includes a reference vibrator, a detection vibrator, a reference vibration generating unit, and a detection unit that are described below.
- the reference vibrator is supported by a support substrate so as to generate reciprocating rotational vibration about a first rotation axis as a center.
- the detection vibrator is supported by the reference vibrator so as to generate reciprocating rotational vibration such that, for example, the detection vibrator rotates about a second rotation axis orthogonal to the first rotation axis, by a Coriolis force generated corresponding to reciprocating rotational vibration of the reference vibrator and an angular velocity input from an outside.
- the reference vibration generating unit allows the reference vibrator to generate reciprocating rotational vibration by, for example, an electrostatic force about the first rotation axis as a center.
- the detection unit detects a relative position between the reference vibrator and the detection vibrator by, for example, an electrostatic capacity therebetween, and detects the Coriolis force corresponding to a magnitude of the rotation of the detection vibrator about the second rotation axis as a center, thereby detecting the angular velocity.
- the reference vibrator serving as a member for holding the detection vibrator is formed of, for example, silicon.
- the support substrate serving as a member for holding the reference vibrator from the outside of an outer edge thereof may be also formed of, for example, silicon.
- a principle for solving the above-mentioned problems of the angular velocity sensor according to the present invention including this embodiment is described as follows.
- the inventors In order to provide the angular velocity sensor "in which noise generated in a detection signal is reduced by the reference vibration, the inventors have focused on “ (1) vibration directions of the reference vibrator and the detection vibrator” and “(2) the detection unit for detecting vibration of the' detection vibrator”.
- the present invention it is assumed that "(1) vibration directions of the reference vibrator and the detection vibrator” are determined by reciprocating rotational vibration about each rotation axis thereof as a center, and "(2) the detection unit for detecting the vibration of the detection vibrator” is a unit for detecting the relative position between ' the reference vibrator and the detection vibrator.
- the vibrators each perform a reciprocating rotational motion about a different rotation axis, so a vibrational component of the reference vibrator is hardly transmitted to the detection vibrator, and thus the above-mentioned cause (2) can be overcome.
- the ⁇ detection unit is also displaced according to the wobbling component, so a reciprocating vibrational component or a vibrational wobbling component of the reference vibrator is hardly detected, and thus the above-mentioned cause (1) can be overcome.
- FIGS. IA and IB are exploded perspective views for illustrating an angular velocity sensor according to Example 1 of the present invention.
- the angular velocity sensor includes a support substrate 1, a reference vibrator 2, a support member 3 for supporting the reference vibrator 2, a detection vibrator 4, a support member 5 for supporting the detection vibrator 4, a drive unit 6 (reference vibration generating unit) for driving the reference vibrator 2, and a detection unit 7 for detecting vibration of the detection vibrator 4.
- the angular velocity sensor includes the reference vibrator 2 formed of two separate members.
- the angular velocity sensor of this example can be produced by bonding the portion of the reference vibrator 2 illustrated in FIG. IB to a lower portion of the reference vibrator 2 illustrated in FIG. IA.
- the annular reference vibrator 2 is supported by the substrate 1 with the support member 3 having four portions formed at equal, angle intervals about a rotation axis A.
- the axis A is a first rotation axis which is perpendicular to the disc-like detection vibrator 4 when the detection vibrator is placed at a neutral position where no force is applied to the detection vibrator.
- the reference vibrator 2 can generate reciprocating rotational vibration in a direction indicated by an arrow C about the first rotation axis A as a center, while being supported by the support member 3.
- the detection vibrator 4 is supported by the reference vibrator 2 with the support member 5 which has two portions extending along a predetermined straight line (axis B) .
- the axis B is a second rotation axis which is in parallel with the substrate 1 and orthogonal to the axis A.
- the detection vibrator 3 has a structure capable of generating reciprocating rotational vibration in a direction indicated by an arrow D about the second rotation axis B as a center, while being supported by the support member 5 which serves as a spring.
- the drive unit 6 allows the reference vibration 2 to generate reciprocating rotational vibration (reference vibration) toward the direction of the arrow C about the first rotation axis A as a center.
- reference vibration reference vibration
- predetermined reference vibration is constantly generated.
- the detection vibrator 4 the Coriolis force corresponding to the reference vibration and the magnitude of the angular velocity component of the angular velocity ⁇ is generated in the direction of the arrow D.
- the detection vibrator 4 generates reciprocating rotational vibration toward " the direction of the arrow D about the second rotation axis B as a center.
- the detection unit 7 detects the relative position between the reference vibrator 2 and the detection vibrator 4, thereby measuring the displacement of the vibration of the detection vibrator 4. From the magnitude of the vibration displacement thus measured, the magnitude of the angular velocity component about the axis E as a center is detected with respect to the input angular velocity ⁇ .
- the detection unit 7 is a unit for measuring an electrostatic capacity between the detection electrode 7 having two separate portions provided on a portion of the reference vibrator 2 illustrated in FIG. IB, and the detection electrode 7 (indicated by the broken line in FIG. IA) provided on a back surface of the detection vibrator 4.
- the detection electrode 7 has a flat-plate portion which is to be positioned on the reference vibrator 2, so the detection electrode 7 can be easily formed.
- a plane corresponding to the portion of the reference, vibrator 2 on which the detection electrodes 7 of FIG. IB are formed is in parallel with a plane corresponding to the detection vibrator 4 on which the detection electrode 7 is formed, with a certain gap, when the angular velocity ⁇ is not input.
- the annular peripheral portion corresponding to the portion of the reference vibrator 2 illustrated in FIG. IB becomes higher than the central portion and serves as a spacer, thereby obtaining the gap.
- the detection electrode 7 provided on the reference vibrator 2 illustrated in FIG. IB is disposed on the plane corresponding to the portion of the reference vibrator 2 opposing to the detection vibrator 4, and is separated in two with a semicircular shape by the straight line F which is in parallel with the axis B.
- the reference vibration is • generated in a reciprocating rotational vibration direction C about the first rotation axis A as a center.
- the detection vibrator 4 is supported by the reference vibrator 2 with the support member 5, so reciprocating rotational vibration in the direction indicated by the arrow D about the second rotation axis B as a center is most liable to be generated, and vibration in the other directions is not hardly generated.
- the detection vibrator 4 generates reciprocating rotational vibration in the direction C about the first axis A as a center, along with the motion of the reference vibrator 2. Accordingly, the relative relationship between the detection vibrator 4. and the reference vibrator 2 is not changed.
- the positional relationship between the second rotation axis- B and the central line F of the detection u electrode 7 is also fixed, which maintains a parallel relationship therebetween.
- the detection vibrator 4 According to the generated Coriolis force, about the second rotation axis B as a center, the detection vibrator 4 generates reciprocating rotational vibration in the direction of the arrow D.
- the rotation axis A and the rotation axis B are orthogonal to each other, so the vibration due to the Coriolis force is generated more efficiently about the rotation axis B.
- the positional relationship between the rotation axis B and the central line F of the detection electrode 7 is fixed, so the change in electrostatic capacity between the detection electrode 7 formed on the portion of the reference vibrator 2 and the detection electrode 7 formed on the detection vibrator 4 can be represented as a function of only an angle of inclination of the • detection vibrator 4 about the second rotation axis B as a center.
- the detection unit 7 can detect, with accuracy, the magnitude of the reciprocating rotational vibration in the direction of the arrow D which is generated by the detection vibrator 4 about the second rotation axis as a center, without being affected by the reference vibration. In other words, a displacement amount of the detection vibrator with respect to the reference vibrator can be obtained.
- the Coriolis force " and the angular velocity can be detected with high accuracy, thereby realizing an angular velocity sensor capable of. detecting the angular velocity with high accuracy.
- the magnitude of the generated Coriolis force corresponds to the magnitude of the reference vibration.
- the positional relationship between the axis B and the central line F of the detection electrode 7 is not changed. Accordingly, it is possible to provide a sensor capable of obtaining higher sensitivity with respect to the angular velocity ⁇ and detecting the angular velocity with higher accuracy.
- the reference vibration when the reference vibration is generated, the positional relationship between the rotation axis B and the central line F of the detection electrode 7 is changed.
- the detection vibrator 4 has a structure in which the detection vibrator 4 is supported so as to be capable of performing the reciprocating rotational motion, and hardly generates vibration in a direction other than the reciprocating rotational vibration direction about the second rotation axis B as a center.
- the reference vibrator 2 is supported from the peripheral portion by four supporting members 3, which realizes a structure in which the vibration toward the rotational direction about the second rotation axis B as a center is hardly generated.
- the detection unit 7 detects the positional relationship between the reference vibrator 2 and the detection vibrator 4, so the vibration wobble of the reference vibrator 2 is not detected 'as a signal, As a result, it is possible to obtain the displacement amount of the detection vibrator with respect to the reference vibrator. In other words, it is possible to provide an angular velocity sensor in which the accuracy of the detection signal is hardly degraded even when the wobbling component of the reference vibrator 2 is present.
- the reference vibrator 2 is held by the support member 3 from the peripheral portion thereof, thereby making it extremely difficult for the reference vibrator 2 to cause the vibration wobble in the rotational direction about the second rotation axis B as a center. Accordingly, it is possible to provide an angular velocity sensor in which the accuracy of the detection signal is hardly degraded.
- the structure of this example it is possible to dispose the detection electrode 7 of the detection unit without taking into consideration of the interference due to the vibration wobble of the reference vibration with respect to the 5 vertical direction of the substrate 1.
- a structure other than the structure of this example in order to avoid a mechanical interference due to the vibration wobble caused in the vertical direction, it is necessary to make a distance between the reference
- FIGS. 2A, 2B, and 2C are exploded perspective views for illustrating an angular velocity sensor according to Example 2 of the present invention.
- the direction (direction of the first rotation axis A) in which the reference vibration is generated is different from that of Example 1.
- Example 2 is similar to Example 1 except for that point.
- the angular velocity sensor includes the support substrate 1, the reference vibrator 2, the support member 3 for supporting the reference vibrator.2, the detection vibrator 4, the support member 5 for supporting the detection vibrator 4, the drive unit 6 for driving the reference vibrator 2, and the detection unit 7 for • detecting vibration of the detection vibrator 4. Also in this example, as illustrated in FIGS.
- the reference vibrator 2 includes two separate members.
- the structure can be obtained by bonding the portion of the reference vibrator 2 illustrated in FlG. 2B to a lower portion of the reference vibrator 2 illustrated in FIG. 2A, and by further bonding the support substrate 1 of FIG. 2C to a lower portion of the bonded support substrate 1.
- the reference vibrator 2 With the axis A, which is in parallel with the disc-like detection vibrator 4, as a center, the reference vibrator 2 generates reciprocating rotational vibration in the direction of the arrow C.
- the drive unit 6 allows the reference vibrator 2 to generate reciprocating rotational vibration, as reference vibration, in the direction of the arrow C about the first axis A as a center.
- the semicircular drive electrode 6 (indicated by broken lines) which is separated into two by the straight line in parallel with the rotation axis A.
- the semicircular drive electrode 6 which is separated into two by the straight line in parallel with the rotation axis A is formed in the same manner. Electrostatic attraction is generated between those drive electrodes ⁇ , thereby constituting the drive unit 6.
- the Coriolis force corresponding to the reference vibration and the magnitude of the angular velocity ⁇ is generated in the direction of the arrow D. Due to the Coriolis force, the reciprocating rotational vibration of the detection vibrator 4 is generated toward the direction of the arrow D about the second rotation axis B as a center.
- the principle of the detection by the detection unit 7 is as described in Example 1.
- FIGS. 3A and 3B are exploded perspective views for illustrating an angular velocity sensor according to Example 3 of the present invention.
- Example 3 is different from Example 1 in that the detection vibrator 4 has recessed portions or through-holes.
- Example 3 is similar to Example 1 except for that point.
- the angular velocity sensor includes the support substrate 1, the reference vibrator 2, the support member 3 for supporting the reference vibrator 2, the detection vibrator 4, the support member 5 for supporting the detection vibrator 4, the drive unit 6 for driving the reference vibrator 2, and the detection unit 7 for detecting vibration of the detection vibrator 4.
- the angular velocity sensor according to this example can also be produced by bonding the portion of the reference vibrator 2 illustrated in FIG. 3B to a lower portion of the reference vibrator 2 illustrated in FIG. 3A.
- the detection vibrator 4 according to this example has a plurality of through-holes 10 formed therein. As the detection vibrator 4 is more distant from the second rotation axis B, the through-holes 10 are provided with higher density.
- the vibration of the detection vibrator 4 for detecting the Coriolis force is generated, the detection vibrator 4 generates reciprocating rotational vibration about the second rotation axis B as a center.
- a point closer to the rotation axis B is represented as Ul, and a point distant from the rotation axis B is represented as U2.
- the detection vibrator 4 generates a larger displacement at the point 02 which is distant from the rotation axis B than at the point Ul which is closer to the rotation axis B.
- the point U2 is more affected by the air damping caused between the detection vibrator 4 and the portion of the reference vibrator 2 of FIG. 3B.
- the point Ul which is closer to the rotation axis B is less affected by the air damping because the displacement at the point Ul does not become too large even when the detection vibrator 4 generates vibration ' to a large extent.
- this example has a structure- in which the effect of the air damping becomes relatively large in the central portion of the detection vibrator 4, so the vibration of the detection vibrator 4 in the vertical direction is hardly generated.
- the air damping is more reduced by the through-holes 10 at positions apart from the rotation axis B.
- this example has a structure in which the air damping can be reduced particularly in an area (area with large displacement) which is liable to be affected by the air damping (vibration state is changed due to the air resistance) when the detection vibrator 4 generates reciprocating rotational vibration about the second rotation axis B as a center.
- the detection vibrator 4 it is possible to distribute the effect of the air damping so that the detection vibrator 4 easily generate reciprocating rotational vibration about the second rotation axis B as a center and hardly perform the vertical motion. For this reason, the detection vibrator 4 can easily generate desired reciprocating rotational vibration, and hardly generates vibrations other than the desired one. Accordingly, it is possible to provide an angular velocity sensor which is high in detection sensitivity and low in noise.
- a surface area of the detection electrode 7 becomes smaller, so it is expected that the detection sensitivity is slightly degraded. However, if each size of the through-holes 10 is minute, a reduction rate of the detection sensitivity is smaller than a reduction rate of the surface area.
- a degree of the influence of the air damping may be changed depending on the size of the through-holes 10.
- a size and shape of the through-holes 10 may be optimized.
- the through-holes 10 are provided in the detection vibrator 4, but may be provided in other areas.
- the through-holes 10 may be provided in the area of the portion of the reference vibrator 2 opposing to the detection vibrator 4.
- the detection sensitivity of the angular velocity ⁇ can be increased as a weight of the detection vibrator 4 becomes larger.
- by forming the through- holes 10 in the reference vibrator 2 it is possible to detect the angular velocity ⁇ without reducing the weight of the detection vibrator 4, that is, without degrading the detection sensitivity.
- the through-holes 10 may be provided in both the area of the detection vibrator 4 and the area of the reference vibrator 2 opposing to the detection vibrator 4.
- the influence of the air damping can be reduced to a large extent, and the detection vibrator 4 can more easily generate reciprocating rotational vibration. Accordingly, it is possible to detect the angular velocity with high accuracy.
- the through-holes 10 are provided in both the area of the detection vibrator 4 and the area of the reference vibrator 2 opposing to the detection vibrator 4, it is desirable to provide , the through-holes 10 such that the through-holes 10 of each of the vibrators are not overlapped with each other.
- the through-holes 10 are provided in the detection vibrator 4 or in the reference vibrator 2, the influence of the air damping can be reduced also by the use of the recessed portions instead of the through-holes 10. As a result, the recessed portions are more easily produced than the through-holes .
- a plurality of recessed portions may be separated from each other, but if a groove is used to laterally connect the recessed portions and has open ends, the effect of the air damping can be reduced more effectively. (Example 4) FIGS.
- Example 4A, 4B, and 4C are exploded perspective views for illustrating an angular velocity sensor according to Example 4 of the present invention.
- Example 4 is different from Example 1 in that a plurality of detection vibrators are provided and rotation axes are orthogonal to each other.
- the reference vibrator includes three annular portions, and the detection electrode of the detection unit is not provided to the reference vibrator.
- Example 4 is similar to Example 1 except for that point.
- the angular velocity sensor includes the support substrate 1, the reference vibrator 2, the support member 3 for supporting the reference vibrator 2, the detection vibrator 4, the support member 5 for supporting the detection vibrator 4 , the drive unit 6 for driving the reference vibrator 2, a second detection vibrator 8, a support member 9 for supporting the second detection vibrator 8, and the detection unit 7 for detecting vibration of the detection vibrator 4 and the second detection vibrator 8.
- the reference vibrator 2 includes three separate members.
- the angular velocity sensor according to this example can be produced by bonding the portion of the reference vibrator 2 illustrated in FIG. 4A to an upper portion of the reference vibrator 2- illustrated in FIG. 4B, and by further bonding the portion of the reference vibrator 2 illustrated in FIG. 4C to a lower portion of the reference vibrator 2 illustrated in FIG. 4B.
- the second detection vibrator 8 and the detection vibrator 4 are stacked in the direction of the first rotation axis A.
- the second detection vibrator 8 performs the reciprocating rotational motion in a direction indicated by an arrow H about a third axis G, which is perpendicular to the axis A and the axis B, as a center.
- the second detection vibrator 8 performs the reciprocating rotational motion about the third rotation axis G as a center.
- the reciprocating rotational motion of the first detection vibrator 4 is as described in Example 1. Specifically, the axis E indicates a central axis of the angular velocity to be detected by the detection vibrator 4.
- the detection unit 7 includes the detection electrode on each of the detection vibrator 4 and the second detection vibrator 8.
- the detection electrode has a shape obtained by equally dividing a circle by straight lines in parallel with the rotation axis B and the rotation axis G (detection electrodes W, X, Y, and Z) .
- the detection electrodes X, Y, Z, and W opposing to each other . form, in pairs,- an electrostatic capacity. Accordingly, the detection unit 7 can detect the electrostatic capacity of each of the detection electrodes X, Y, Z, and W.
- the shape of the detection electrode By employment of the shape of the detection electrode, it is possible to detect the reciprocating rotational motion of the detection vibrator 4 about the second rotation axis B as a center, and the reciprocating rotational .motion of the second detection vibrator 8 about the third rotation axis G as a center, at the same time. Specifically, by calculating a difference between a value obtained by adding the electrostatic capacity of the detection electrodes W and X, and a value obtained by adding the electrostatic capacity of the detection electrodes Y and Z, it is possible to detect the reciprocating rotational motion of the detection vibrator 4 about the second rotation axis B as a center.
- the detection principle is the same as that of Example 1 in which the detection electrode is provided to the portion of the reference vibrator 2. According to this example, it is possible to detect a biaxial angular velocity with the same chip area as that in the structure illustrated in FIG. IA and IB. Accordingly, it is possible to provide a small sensor capable of detecting the biaxial angular velocity with high .accuracy.
- the reference vibrator 2 and the detection unit 8 do not • surround the detection vibrator. Accordingly, it is possible to reduce the effect in which the reciprocating rotational motion of the detection vibrator is inhibited by the air damping.
- this example has a symmetric structure (FIG. IB is a central surface of the symmetric structure) with r-espect to the direction of the axis A, so generation of the vibration wobble itself of the reference vibrator can be reduced. Accordingly, it is possible to detect the angular velocity with higher accuracy.
- the detection vibrator 4 or the second detection vibrator 8 may be provided with recessed portions or through-holes in the following manner. That is, the through-holes are provided in the detection vibrator 4 with a density in proportion to a distance from the second rotation axis B. Further, the through-holes are provided in the second detection vibrator 8 with a density in proportion to a distance from the third rotation axis G. With that structure, it is possible to reduce the influence of the air damping on the vibration so that the detection vibrator 4 and the second detection vibrator 8 can easily perform the reciprocating rotational motion in a desired direction.
- the through-holes provided in the detection vibrator 4 and the through-holes provided in the second detection vibrator 8 are arranged so as not to be overlapped with each other. As a result, it is possible to reduce the influence of the air damping on the vibration without largely degrading the detection sensitivity of the detection electrode.
- FIGS. 5A and 5B are exploded perspective views for illustrating an angular velocity sensor according to Example 5 of the present invention.
- Example 5 is different from Example 1 in that a cross-section of the support member 5 of the detection vibrator 4 has an X- shape.
- Example 5 is similar to Example 1 except for that point .
- FIGS. 5A and 5B are similar to FIG. 1 except for the shape of a cross-section of the support member 5 of the detection vibrator 4.
- FIG. 6 is a diagram illustrating the shape of the cross-section of the support member 5 of the detection vibrator 4.
- the cross-section of the support member 5 of the detection vibrator 4 has the X-shape, and mechanical characteristics thereof are equivalent to those of a structure obtained by combining multiple plate-shape springs.
- directions in which each plate- shape spring is most liable to be deflected are indicated by arrows J.
- the plate-shape springs are arranged such that the arrows J cross to each other.
- each plate-shape spring inhibits the deflection of another plate-shape spring.
- the support member 5 has the X-shape in the cross-section, so the detection vibrator 4 easily generates reciprocating rotational vibration about the second rotation axis B as a center. Accordingly, it is possible to reduce the vibration in the other directions. As a result, the magnitude of the detection vibration of the detection vibrator 4 per unit angular velocity is increased, and the sensitivity of the detection for the angular velocity is improved.
- the vibration of the detection vibrator 4 other than the reference vibration and the detection vibration due to the vibration wobble is hardly generated, so the detection noise generated by the vibrator can be reduced.
- a shape of the angular velocity sensor according to the present invention by the use of the MEMS.
- a plurality of substrates are processed by the use of the MEMS, and the substrates are bonded to each other, thereby achieving the structure of the angular velocity sensor.
- Silicon often used for the MEMS is superior to metal in normal mechanical characteristics.
- a difference between physical properties due to crystal orientations of silicon may affect the mechanical characteristics.
- the accuracy of processing of a thick three-dimensional structure using the MEMS is apt to be lower than that of general mechanical processing. Accordingly, in the angular velocity sensor using the MEMS, a wobble due to the reference vibration is easily generated.
- the present invention By applying the present invention to the angular velocity sensor using the MEMS, even when the wobble due to the reference vibration is generated, the noise caused by the wobble can be reduced. Accordingly, it is possible to realize an angular velocity sensor which is low in noise caused by the wobble due to the reference vibration and with high accuracy, by the use of silicon or the like, while maintaining the characteristic of the high sensitivity.
- a detecting technigue using the electrostatic capacity is applied to detection unit 7, there is no need to consider the mechanical interference due to the vibration wobble, so it is possible to provide the electrodes with a small distance therebetween and provide a small gap by the use of the MEMS.
- the present invention can solve the problems of the angular velocity sensor using the MEMS, and can provide an angular velocity sensor with higher accuracy.
- the object to be detected by the detection unit according to the present invention is the displacement amount of the detection vibrator with respect to the reference vibrator.
- the electrostatic attraction generated between the flat- plate electrodes (see FIGS. 2A, 2B, and 2C) or between the interdigital electrodes (for example, see FIGS. IA and IB) is used as the drive unit 6, but the drive unit 6 is not limited thereto. Any drive unit can be used as long as it can allow the reference vibrator 2 to generate reference vibration in a desired direction.
- the semicircular detection electrode of the detection unit 7 is provided on the reference vibrator, but the structure is not limited thereto.
- the detection electrode may be provided on the detection vibrator 4 (or on the second detection vibrator 8) .
- the detection unit 7 detects the displacement amount of the detection vibrator with respect to the reference vibrator, but the structure is not limited thereto. Any unit can be used as long as- it can detect the motion about the rotation axis of the detection vibrator. For example, while the sensitivity is degraded as compared with the case of the detection , by the electrostatic capacity, it is possible to adopt a mode in which a strain detection unit including a piezoresistor -using a piezoresistor effect or a ' piezoelectric element using a piezoelectric effect is provided for the support member of the detection vibrator.
- the detection vibrator, and the support members are structured as illustrated in the drawings, but the structures thereof are not limited thereto. Any structure can be employed as long as it enables the reference vibrator and the detection vibrator to ' perform reciprocating rotation about a desired different axis as a center.
- the reference • vibrator is allowed to generate reciprocating rotational vibration by another force as the reference vibration generation unit, while the reference vibrator is levitated by an electrostatic levitation method or a magnetic levitation method.
- the angular velocity sensor according to the present invention is capable of detecting an angular velocity with higher accuracy.
- the angular velocity sensor according to the present invention it is possible to, for example, realize a posture detection device and a posture control device with high accuracy.
- the posture detection device can be used for, for example, detection and correction of blurring due to hand shake of a camera, and car navigation.
- the posture control device can be used for, for example, a robot having a posture control function.
- the reference vibrator has a vibrational component (vibrational wobbling component) other than the reference vibration
- a vibrational component vibrational wobbling component
- the structure of the present invention in the detection unit, the reciprocating vibrational component or the vibrational wobbling' component of the reference vibration is hardly detected (the above-mentioned cause (1) is overcome) , so the noise in the detection signal can be reduced.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Ceramic Engineering (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Computer Hardware Design (AREA)
- Gyroscopes (AREA)
- Pressure Sensors (AREA)
Abstract
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BRPI0715477-1A BRPI0715477A2 (en) | 2006-08-09 | 2007-07-26 | ANGULAR SPEED SENSOR |
CN2007800294535A CN101501446B (en) | 2006-08-09 | 2007-07-26 | Angular velocity sensor |
EP07791788A EP2052206A2 (en) | 2006-08-09 | 2007-07-26 | Angular velocity sensor |
KR1020097004843A KR101163826B1 (en) | 2006-08-09 | 2007-07-26 | Angular velocity sensor |
US12/304,966 US8336380B2 (en) | 2006-08-09 | 2007-07-26 | Angular velocity sensor |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2006-216694 | 2006-08-09 | ||
JP2006216694A JP5159062B2 (en) | 2006-08-09 | 2006-08-09 | Angular velocity sensor |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2008018347A2 true WO2008018347A2 (en) | 2008-02-14 |
WO2008018347A3 WO2008018347A3 (en) | 2008-05-02 |
Family
ID=39033394
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2007/065108 WO2008018347A2 (en) | 2006-08-09 | 2007-07-26 | Angular velocity sensor |
Country Status (8)
Country | Link |
---|---|
US (1) | US8336380B2 (en) |
EP (1) | EP2052206A2 (en) |
JP (1) | JP5159062B2 (en) |
KR (1) | KR101163826B1 (en) |
CN (1) | CN101501446B (en) |
BR (1) | BRPI0715477A2 (en) |
RU (1) | RU2405126C1 (en) |
WO (1) | WO2008018347A2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010041209A1 (en) | 2008-10-08 | 2010-04-15 | Nxp B.V. | Oscillator device |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5432440B2 (en) * | 2007-07-04 | 2014-03-05 | キヤノン株式会社 | Oscillator device |
JP5247182B2 (en) * | 2008-02-19 | 2013-07-24 | キヤノン株式会社 | Angular velocity sensor |
JP5473253B2 (en) * | 2008-06-02 | 2014-04-16 | キヤノン株式会社 | Structure having a plurality of conductive regions and manufacturing method thereof |
JP2010054263A (en) * | 2008-08-27 | 2010-03-11 | Pioneer Electronic Corp | Rotation oscillation gyroscope |
US8499629B2 (en) * | 2008-10-10 | 2013-08-06 | Honeywell International Inc. | Mounting system for torsional suspension of a MEMS device |
US8266961B2 (en) * | 2009-08-04 | 2012-09-18 | Analog Devices, Inc. | Inertial sensors with reduced sensitivity to quadrature errors and micromachining inaccuracies |
JP5424847B2 (en) | 2009-12-11 | 2014-02-26 | キヤノン株式会社 | Electromechanical converter |
JP5473579B2 (en) | 2009-12-11 | 2014-04-16 | キヤノン株式会社 | Control device for capacitive electromechanical transducer and control method for capacitive electromechanical transducer |
JP5414546B2 (en) | 2010-01-12 | 2014-02-12 | キヤノン株式会社 | Capacitance detection type electromechanical transducer |
JP5603739B2 (en) | 2010-11-02 | 2014-10-08 | キヤノン株式会社 | Capacitance type electromechanical transducer |
US8847143B2 (en) | 2011-04-27 | 2014-09-30 | Honeywell International Inc. | Systems and methods for an encoder and control scheme |
JP5947511B2 (en) | 2011-09-08 | 2016-07-06 | キヤノン株式会社 | Electromechanical converter |
TWI476444B (en) * | 2011-12-22 | 2015-03-11 | Nat Inst Chung Shan Science & Technology | Double-projection apparatus |
CN104215236B (en) * | 2013-06-05 | 2016-12-28 | 中国科学院地质与地球物理研究所 | A kind of anti-phase vibratory gyroscope of MEMS and manufacturing process thereof |
KR101459487B1 (en) * | 2013-12-17 | 2014-11-07 | 현대자동차 주식회사 | Display apparatus for vehicle |
JP6472313B2 (en) | 2015-04-16 | 2019-02-20 | キヤノン株式会社 | Probe and information acquisition device |
FI127203B (en) * | 2015-05-15 | 2018-01-31 | Murata Manufacturing Co | Vibrating micromechanical sensor of the angular velocity |
US10665207B2 (en) * | 2017-12-13 | 2020-05-26 | Kyocera Document Solutions Inc. | Back-and-forth displacement detecting device and information processing device |
JP7516009B2 (en) | 2019-02-20 | 2024-07-16 | キヤノン株式会社 | Oscillators, imaging devices |
JP2023028939A (en) * | 2021-08-20 | 2023-03-03 | 本田技研工業株式会社 | Support device for ship, support method for ship, and program |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2797580A (en) * | 1955-07-18 | 1957-07-02 | Bosch Arma Corp | Gyroscope suspension |
GB2198231A (en) * | 1986-11-28 | 1988-06-08 | Stc Plc | Rotational motion sensor |
US5955668A (en) * | 1997-01-28 | 1999-09-21 | Irvine Sensors Corporation | Multi-element micro gyro |
US5987986A (en) * | 1994-07-29 | 1999-11-23 | Litton Systems, Inc. | Navigation grade micromachined rotation sensor system |
US20020189351A1 (en) * | 2001-06-14 | 2002-12-19 | Reeds John W. | Angular rate sensor having a sense element constrained to motion about a single axis and flexibly attached to a rotary drive mass |
US20030200803A1 (en) * | 2002-04-30 | 2003-10-30 | Honeywell International Inc. | Pulse width modulation drive signal for a MEMS gyroscope |
EP1455162A1 (en) * | 2003-03-06 | 2004-09-08 | Samsung Electronics Co., Ltd. | Rotary gyroscope |
EP1677074A1 (en) * | 2003-10-20 | 2006-07-05 | Sony Corporation | Angular velocity detector, angular velocity detection method by angular velocity detector and production method of angular velocity detector |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4598585A (en) * | 1984-03-19 | 1986-07-08 | The Charles Stark Draper Laboratory, Inc. | Planar inertial sensor |
US5488862A (en) * | 1993-10-18 | 1996-02-06 | Armand P. Neukermans | Monolithic silicon rate-gyro with integrated sensors |
JP3336730B2 (en) | 1994-02-28 | 2002-10-21 | 株式会社村田製作所 | Angular velocity sensor |
JPH1089968A (en) * | 1996-09-12 | 1998-04-10 | Murata Mfg Co Ltd | Angular velocity sensor |
JPH1096633A (en) * | 1996-09-21 | 1998-04-14 | Murata Mfg Co Ltd | Angular speed detector |
DE19828424C1 (en) * | 1998-06-25 | 1999-12-02 | Litef Gmbh | Micromechanical revolution rate sensor base on the Coriolis principle |
US6374672B1 (en) * | 2000-07-28 | 2002-04-23 | Litton Systems, Inc. | Silicon gyro with integrated driving and sensing structures |
JP2004191224A (en) * | 2002-12-12 | 2004-07-08 | Natl Space Development Agency Of Japan | Angular velocity sensor, manufacturing method for the same, method of measuring angular speed using angular velocity sensor |
US6978673B2 (en) * | 2003-02-07 | 2005-12-27 | Honeywell International, Inc. | Methods and systems for simultaneously fabricating multi-frequency MEMS devices |
JP2006003131A (en) * | 2004-06-15 | 2006-01-05 | Canon Inc | Potential sensor |
JP2006119002A (en) * | 2004-10-22 | 2006-05-11 | Sony Corp | Angular velocity detector |
US7382137B2 (en) * | 2005-05-27 | 2008-06-03 | Canon Kabushiki Kaisha | Potential measuring apparatus |
JP5105949B2 (en) * | 2007-04-27 | 2012-12-26 | キヤノン株式会社 | Sensor |
-
2006
- 2006-08-09 JP JP2006216694A patent/JP5159062B2/en not_active Expired - Fee Related
-
2007
- 2007-07-26 EP EP07791788A patent/EP2052206A2/en not_active Withdrawn
- 2007-07-26 KR KR1020097004843A patent/KR101163826B1/en not_active IP Right Cessation
- 2007-07-26 US US12/304,966 patent/US8336380B2/en not_active Expired - Fee Related
- 2007-07-26 WO PCT/JP2007/065108 patent/WO2008018347A2/en active Application Filing
- 2007-07-26 BR BRPI0715477-1A patent/BRPI0715477A2/en not_active Application Discontinuation
- 2007-07-26 RU RU2009108316/28A patent/RU2405126C1/en not_active IP Right Cessation
- 2007-07-26 CN CN2007800294535A patent/CN101501446B/en not_active Expired - Fee Related
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2797580A (en) * | 1955-07-18 | 1957-07-02 | Bosch Arma Corp | Gyroscope suspension |
GB2198231A (en) * | 1986-11-28 | 1988-06-08 | Stc Plc | Rotational motion sensor |
US5987986A (en) * | 1994-07-29 | 1999-11-23 | Litton Systems, Inc. | Navigation grade micromachined rotation sensor system |
US5955668A (en) * | 1997-01-28 | 1999-09-21 | Irvine Sensors Corporation | Multi-element micro gyro |
US20020189351A1 (en) * | 2001-06-14 | 2002-12-19 | Reeds John W. | Angular rate sensor having a sense element constrained to motion about a single axis and flexibly attached to a rotary drive mass |
US20030200803A1 (en) * | 2002-04-30 | 2003-10-30 | Honeywell International Inc. | Pulse width modulation drive signal for a MEMS gyroscope |
EP1455162A1 (en) * | 2003-03-06 | 2004-09-08 | Samsung Electronics Co., Ltd. | Rotary gyroscope |
EP1677074A1 (en) * | 2003-10-20 | 2006-07-05 | Sony Corporation | Angular velocity detector, angular velocity detection method by angular velocity detector and production method of angular velocity detector |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010041209A1 (en) | 2008-10-08 | 2010-04-15 | Nxp B.V. | Oscillator device |
US8717111B2 (en) | 2008-10-08 | 2014-05-06 | Nxp, B.V. | Oscillator device |
Also Published As
Publication number | Publication date |
---|---|
WO2008018347A3 (en) | 2008-05-02 |
JP5159062B2 (en) | 2013-03-06 |
KR101163826B1 (en) | 2012-07-09 |
EP2052206A2 (en) | 2009-04-29 |
JP2008039669A (en) | 2008-02-21 |
RU2405126C1 (en) | 2010-11-27 |
CN101501446A (en) | 2009-08-05 |
KR20090042301A (en) | 2009-04-29 |
US8336380B2 (en) | 2012-12-25 |
RU2009108316A (en) | 2010-09-20 |
BRPI0715477A2 (en) | 2014-05-06 |
CN101501446B (en) | 2012-07-04 |
US20090193893A1 (en) | 2009-08-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8336380B2 (en) | Angular velocity sensor | |
JP4687577B2 (en) | Inertial sensor | |
JP5649972B2 (en) | Yaw rate sensor | |
JP3924026B2 (en) | Vibration structure and method for controlling natural frequency of vibration structure | |
JP5822177B2 (en) | Gyro sensor, electronic equipment | |
JP5247182B2 (en) | Angular velocity sensor | |
US9273962B2 (en) | Physical quantity sensor and electronic device | |
US8250916B2 (en) | Inertial sensor | |
JP2006215016A (en) | Sensor having both functions of gyroscope and accelerometer | |
JP2014112085A (en) | Spring for micro electro-mechanical systems (mems) device | |
JPH09189557A (en) | Microgyroscope | |
JP2005514608A6 (en) | Rotational speed sensor | |
JP2007256235A (en) | Inertia force sensor | |
JP2009222475A (en) | Compound sensor | |
JP4654667B2 (en) | Gyro sensor and angular velocity detection method | |
US11796319B2 (en) | Sensor and electronic device | |
JP4983107B2 (en) | Inertial sensor and method of manufacturing inertial sensor | |
JP2012112819A (en) | Vibration gyro | |
JP5125138B2 (en) | Compound sensor | |
JP2007256234A (en) | Inertia force sensor | |
JP2008232704A (en) | Inertia force sensor | |
JP2008261771A (en) | Inertia force sensor | |
JP2012229989A (en) | Spring structure, physical quantity sensor, and electronic apparatus | |
JP2009222476A (en) | Compound sensor | |
JP2010197061A (en) | Inertia force detecting element |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WWE | Wipo information: entry into national phase |
Ref document number: 200780029453.5 Country of ref document: CN |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 07791788 Country of ref document: EP Kind code of ref document: A2 |
|
WWE | Wipo information: entry into national phase |
Ref document number: 12304966 Country of ref document: US |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2007791788 Country of ref document: EP |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
WWE | Wipo information: entry into national phase |
Ref document number: 1289/CHENP/2009 Country of ref document: IN Ref document number: 1020097004843 Country of ref document: KR |
|
ENP | Entry into the national phase |
Ref document number: 2009108316 Country of ref document: RU Kind code of ref document: A |
|
ENP | Entry into the national phase |
Ref document number: PI0715477 Country of ref document: BR Kind code of ref document: A2 Effective date: 20090123 |