WO2010100333A1 - Micro-mechanical sensor of angular velocity - Google Patents

Micro-mechanical sensor of angular velocity Download PDF

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Publication number
WO2010100333A1
WO2010100333A1 PCT/FI2010/050159 FI2010050159W WO2010100333A1 WO 2010100333 A1 WO2010100333 A1 WO 2010100333A1 FI 2010050159 W FI2010050159 W FI 2010050159W WO 2010100333 A1 WO2010100333 A1 WO 2010100333A1
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WO
WIPO (PCT)
Prior art keywords
masses
micro
spring
motion
mechanical resonator
Prior art date
Application number
PCT/FI2010/050159
Other languages
French (fr)
Inventor
Anssi Blomqvist
Original Assignee
Vti Technologies Oy
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Vti Technologies Oy filed Critical Vti Technologies Oy
Priority to EP10748387.7A priority Critical patent/EP2404138B1/en
Priority to JP2011552480A priority patent/JP5670356B2/en
Priority to KR1020117022831A priority patent/KR101676264B1/en
Priority to CN201080014785.8A priority patent/CN102365524B/en
Publication of WO2010100333A1 publication Critical patent/WO2010100333A1/en
Priority to IL214925A priority patent/IL214925A0/en

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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
    • G01C19/5719—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using planar vibrating masses driven in a translation vibration along an axis
    • G01C19/5733—Structural details or topology
    • G01C19/574—Structural details or topology the devices having two sensing masses in anti-phase motion
    • G01C19/5747—Structural details or topology the devices having two sensing masses in anti-phase motion each sensing mass being connected to a driving mass, e.g. driving frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B81—MICROSTRUCTURAL TECHNOLOGY
    • B81B—MICROSTRUCTURAL DEVICES OR SYSTEMS, e.g. MICROMECHANICAL DEVICES
    • B81B3/00—Devices comprising flexible or deformable elements, e.g. comprising elastic tongues or membranes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B81—MICROSTRUCTURAL TECHNOLOGY
    • B81B—MICROSTRUCTURAL DEVICES OR SYSTEMS, e.g. MICROMECHANICAL DEVICES
    • B81B3/00—Devices comprising flexible or deformable elements, e.g. comprising elastic tongues or membranes
    • B81B3/0018—Structures acting upon the moving or flexible element for transforming energy into mechanical movement or vice versa, i.e. actuators, sensors, generators
    • 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
    • G01C19/5607—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using vibrating tuning forks
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
    • G01P3/02—Devices characterised by the use of mechanical means
    • G01P3/14—Devices characterised by the use of mechanical means by exciting one or more mechanical resonance systems

Definitions

  • the invention relates to sensors of angular velocity, particularly to vibrating micro-mechanical sensors of angular velocity.
  • FIG 1 a diagram is shown of a prior art simple coupled resonator, in which the coupling spring J is an identical one-dimensional spring like the other ones.
  • the simple coupling resonator consists of two masses ml, m2 and three identical one-dimensional springs J.
  • the structure according to Figure 1 efficiently separates the masses' common mode of motion from the differential mode.
  • the structure is unfavorable from the standpoint of acceleration sensitivity, since the masses are more easily displaced in the same phase (the frequency of the mode being lower) than in opposite phase, because the coupling spring will not participate in the motion in the same phase.
  • the spring structures described in the patent publication have some drawbacks. For example, sensitivity to linear acceleration, because, like the simple coupled resonator described above, they have more slackness for common mode than for opposite phase motion. Thus, blows and vibration displace the masses more easily than does the desired excitation required for the vibration mode in opposite phases. Further, non-linearity in the primary mode is hard to control, because the spring structures participate in both modes. In fact, it would be preferable completely to separate the coupling spring structures for the different modes from each other, such that the non-linearity of the primary mode suspension could be dimensioned independently from the secondary suspension.
  • a coupling suspension is, for example, implemented in the patent application FI 20095201, for which priority is claimed, for primary motion in the y direction of excitation frames, and also presented in Figure 2, which shows a sensor of angular velocity for the Z axis, in which is shown an example of a seesaw type coupled spring structure in the top and bottom ends in the y axis direction.
  • the angular velocity sensor structure of figure 2 completely lacks coupling between the masses inside the frames, whereby, in the x axis direction, the masses operate as nearly independent acceleration sensors. Being uncoupled, they are mechanically almost as sensitive to (common mode) mechanical interference as they are to any opposite phase Coriolis force to be detected.
  • the question remains open, how preferably to design a coupling suspension for the masses, which would prevent their motion in the same phase, but still would not participate in the primary motion in the y axis direction.
  • a seesaw suspension similar to the one described above constitutes a working solution with masses moving along, as such, parallel and side by side located axes, but considering a tightly packed structure, takes rather a lot of space.
  • Such a structure provided with masses moving opposite to each other on a common axis, which in a way is even wasteful, is roughly illustrated in Figure 3.
  • Figure 3 One can clearly see from Figure 3, that such a structure occupies almost the whole space between the masses, which previously was used for the excitation comb structures of the primary motion.
  • micro-mechanical resonator according to the invention is characterized in what is mentioned in the characterizing part of the independent claim related to the same.
  • the sensor according to the invention is characterized in what is mentioned in the characterizing part of the independent claim related to the same.
  • the vehicle according to the invention is characterized in what is mentioned in the characterizing part of the independent claim related to the same.
  • the navigator according to the invention is characterized in what is mentioned in the characterizing part of the independent claim related to the same.
  • the system of micromechanical resonators comprises at least one micromechanical resonator that comprises two masses (Ml M2 ) that are coupled in direction of their common motion axis with spring structure (401, 402, 403, 404a, 404b, 404c)that comprises at least two beams (402) connected to the masses and spring suspension (404a, 404b, 404c) parallel to the motion axis coupling the beams that deflects perpendicularly to the motion .
  • Figure 1 illustrates a diagram of a simple coupled resonator according to prior art as such
  • Figure 2 illustrates, as such, such a Z axis sensor of angular velocity, which features a seesaw type coupled spring structure
  • Figure 3 illustrates a diagram of the space utilization of, as such, a seesaw type spring structure.
  • Figure 4 illustrates a diagram of a spring structure according to an embodiment of the invention
  • Figure 5 illustrates a Z axis angular velocity sensor structure according to an embodiment of the invention
  • Figure 6 illustrates the primary mode of a Z axis angular velocity sensor structure according to an embodiment of the invention
  • Figure 7 illustrates the detection mode of a Z axis angular velocity sensor structure according to an embodiment of the invention.
  • Figure 8 illustrates the effect of linear acceleration in the detection direction in a Z axis angular velocity sensor structure according to an embodiment of the invention.
  • Figure 9 illustrates an embodiment of the invention, with a secondary coupling.
  • a spring structure according to an embodiment of the invention is illustrated as an example, the structure being arranged to couple the masses Ml and M2 vibrating on a common axis into opposite phase vibration.
  • a spring structure 401, 402, 403, 404a, 404b, 404c coupling the two masses which spring structure is composed of two stiff bars 402 and a bending spring 404a, 404b, 404c connecting the two bars 402.
  • the bars are suspended 403 such, that they are allowed to turn about a support point located in one end. At the other end, the bars are connected 401 to the masses Ml, M2 to be coupled.
  • a simple example of the spring structure according to the embodiment of the invention is presented.
  • a spring structure according to an embodiment of the invention is illustrated as an example, the structure being arranged with a view to an angular velocity sensor structure similar to the one in Figure 2, wherein a coupling in the Y direction of the detection axis for the masses Ml and M2 has been formed by means of the structure according to the embodiment of the invention.
  • two springs 404a, 404b, 404c, positioned according to the embodiment of the invention are shown such, that they, at the ends, couple the masses into an opposite phase vibration mode on the detection axis.
  • the coupling spring structures do not participate in the primary motion in any essential manner, since those said bars 402 are attached to the masses Ml and M2 with springs, which are loose in the x direction (in relation to the springs in the y direction) , but stiff in the y direction (in relation to the springs in the x direction) .
  • the primary mode of the structure is being illustrated.
  • the coupling spring structures at the masses' ends, according to an embodiment of the invention do not appreciably, or almost not at all, participate in the primary mode.
  • a blow or an external linear acceleration component in the direction of the detection axis causes a displacement in both masses in the same phase.
  • the bars turn in the same direction, which forces the coupling spring into an S-shaped bending in accordance with Figure 8.
  • the spring is considerably stiffer than in the case above.
  • the coupling spring structure can be made even equally or over 4 times stiffer to displacement of the masses in the same direction than to opposite phase displacement.
  • the spring can be designed to be even 10 times stiffer to in-phase deflection compared to anti-phase deflection .
  • a system of micromechanical resonators comprises at least one micromechanical resonator that comprises two masses (Ml M2) that are coupled in direction of their common motion axis with spring structure (401, 402, 403, 404a, 404b, 404c)that comprises at least two beams (402) connected to the masses and spring suspension (404a, 404b, 404c) parallel to the motion axis coupling the beams that deflects perpendicularly to the motion .
  • the structure according to that comprises means for connecting an electric voltage between a first part of the resonator and a second part in order to provide a capacitive structure between said parts, to be used for producing a capacitively readable signal, when the motion according to vibration of the spring structure changes the distance, and thus the capacitance, between said first and second parts.
  • At least one of the bars at the end is arranged with regard for piezoelectric effects for providing an excitation structure.
  • one of said end bars is arranged to change its form in response to an electric signal being applied to it.
  • one of said bars is arranged such, that the piezoelectric voltage corresponding to its bending can be measured at a certain part of the bar, to be used in the filtering of interference and/or other signal processing.
  • a navigator can be provided, which includes a function, in which the direction of motion at a certain point in time can be determined by means of the angular velocity determined by a certain sensor of the navigator and by means of a clock.
  • the attachment points to the masses of the suspension according to one embodiment of the invention are located on the same straight line extending in the direction of the motion axes. Due to that, the reaction forces of the spring do not induce a moment on the masses, like e.g. a seesaw spring. Furthermore, the suspension can be designed such, that it will not participate in any significant manner, if at all, in the masses' motions in the directions of other axes.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Hardware Design (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Automation & Control Theory (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Gyroscopes (AREA)

Abstract

The invention presents a micro-mechanical resonator, comprising two masses coupled in the direction of a common axis by a spring structure such, that the spring structure comprises a spring that couples at least a first bar connected to the masses and a second bar extending in the motion axis direction, said spring being arranged to bend in a direction perpendicular to the motion direction of the motion axis. The invention also relates to a micro-mechanical resonator matrix, a sensor and a navigation device.

Description

Micro-mechanical Sensor of Angular Velocity
The invention relates to sensors of angular velocity, particularly to vibrating micro-mechanical sensors of angular velocity.
Background
Central features required of sensors of angular velocity are resistance to vibration and impact. Particularly in applications in the automotive industry, for example, such as driving stability control systems, these requirements are extremely tight. Even a violent external blow, e.g. from a stone, or vibration caused by a car stereo, should not interfere with the output of the sensor of angular velocity.
In many micro-mechanical resonators, like e.g. sensors of angular velocity, designing a coupling spring between the moving masses would be preferable, which spring would enable opposite phase motion of the masses and, at the same time, would resist common mode motion of the masses. Such an arrangement is needed particularly for distinguishing various disturbances from the actual signal, such as instances of mechanical impact. Usually, the signal detected from the masses is differential, whereas acceleration influencing them equally causes a common mode displacement.
In Figure 1, a diagram is shown of a prior art simple coupled resonator, in which the coupling spring J is an identical one-dimensional spring like the other ones. Thus, the simple coupling resonator consists of two masses ml, m2 and three identical one-dimensional springs J. The structure according to Figure 1 efficiently separates the masses' common mode of motion from the differential mode. However, the structure is unfavorable from the standpoint of acceleration sensitivity, since the masses are more easily displaced in the same phase (the frequency of the mode being lower) than in opposite phase, because the coupling spring will not participate in the motion in the same phase.
In the US patent publication US 6,752,017 B2 particularly depicted are coupled spring structures for a Z-axis gyro, wherein the detection motion is a vibration in opposite phases of masses on a common axis of motion. A common feature of these spring structures is, that they participate in defining both the primary mode and the secondary mode frequencies, and, according to the patent publication, they are positioned between the masses to be coupled, which are located next to each other.
However, the spring structures described in the patent publication have some drawbacks. For example, sensitivity to linear acceleration, because, like the simple coupled resonator described above, they have more slackness for common mode than for opposite phase motion. Thus, blows and vibration displace the masses more easily than does the desired excitation required for the vibration mode in opposite phases. Further, non-linearity in the primary mode is hard to control, because the spring structures participate in both modes. In fact, it would be preferable completely to separate the coupling spring structures for the different modes from each other, such that the non-linearity of the primary mode suspension could be dimensioned independently from the secondary suspension.
A clearly better solution from the viewpoint of mechanical interference, when having vibrating masses with parallel axes, is a seesaw type coupling spring, since it is stiffer for displacement in the same phase than for displacement in opposite phases. Such a coupling suspension is, for example, implemented in the patent application FI 20095201, for which priority is claimed, for primary motion in the y direction of excitation frames, and also presented in Figure 2, which shows a sensor of angular velocity for the Z axis, in which is shown an example of a seesaw type coupled spring structure in the top and bottom ends in the y axis direction.
However, the angular velocity sensor structure of figure 2 completely lacks coupling between the masses inside the frames, whereby, in the x axis direction, the masses operate as nearly independent acceleration sensors. Being uncoupled, they are mechanically almost as sensitive to (common mode) mechanical interference as they are to any opposite phase Coriolis force to be detected. Thus, the question remains open, how preferably to design a coupling suspension for the masses, which would prevent their motion in the same phase, but still would not participate in the primary motion in the y axis direction.
A seesaw suspension similar to the one described above constitutes a working solution with masses moving along, as such, parallel and side by side located axes, but considering a tightly packed structure, takes rather a lot of space. Such a structure provided with masses moving opposite to each other on a common axis, which in a way is even wasteful, is roughly illustrated in Figure 3. One can clearly see from Figure 3, that such a structure occupies almost the whole space between the masses, which previously was used for the excitation comb structures of the primary motion.
Thus, the problem remains unsolved, how to implement a structure, at the same time compact and still capable of operating in opposite phase vibrating mode more willingly than in the same phase, and how to then, as a consequence of the opposite phase mode, one could utilize the advantages offered by the opposite phase for e.g. removing interference.
With the technique according to the embodiments of the invention, a solution is obtained to the problem presented above and also to other associated problems; and, if not completely resolved, the effects of the problems will be at least alleviated.
The micro-mechanical resonator according to the invention is characterized in what is mentioned in the characterizing part of the independent claim related to the same.
The sensor according to the invention is characterized in what is mentioned in the characterizing part of the independent claim related to the same.
The vehicle according to the invention is characterized in what is mentioned in the characterizing part of the independent claim related to the same.
The navigator according to the invention is characterized in what is mentioned in the characterizing part of the independent claim related to the same.
The system of micromechanical resonators comprises at least one micromechanical resonator that comprises two masses (Ml M2 ) that are coupled in direction of their common motion axis with spring structure (401, 402, 403, 404a, 404b, 404c)that comprises at least two beams (402) connected to the masses and spring suspension (404a, 404b, 404c) parallel to the motion axis coupling the beams that deflects perpendicularly to the motion .
In the dependent claims, other preferable embodiments of the invention are presented.
List of Figures
In the Figures 1—3, reference is made to prior art as such (Figure 1) or to technique presented elsewhere and known to the applicant at the date of filing for processing of the present application (Figure 2, and Figure 3, patent document FI 20095201), as follows:
Figure 1 illustrates a diagram of a simple coupled resonator according to prior art as such,
Figure 2 illustrates, as such, such a Z axis sensor of angular velocity, which features a seesaw type coupled spring structure,
Figure 3 illustrates a diagram of the space utilization of, as such, a seesaw type spring structure.
Since, as mentioned above, the Figures 1—3 were referencing technique presented elsewhere, below, examples are presented referring to Figures 4—9, for illustrating embodiments of the invention, presented in the present application. Thus, the intention is not to limit the embodiments exclusively to embodiments according to the presented examples, nor within those, exclusively according to the proportions being disclosed in the figures. The embodiments of the invention can be combined with each other, as applicable. Figure 4 illustrates a diagram of a spring structure according to an embodiment of the invention, Figure 5 illustrates a Z axis angular velocity sensor structure according to an embodiment of the invention,
Figure 6 illustrates the primary mode of a Z axis angular velocity sensor structure according to an embodiment of the invention,
Figure 7 illustrates the detection mode of a Z axis angular velocity sensor structure according to an embodiment of the invention, and
Figure 8 illustrates the effect of linear acceleration in the detection direction in a Z axis angular velocity sensor structure according to an embodiment of the invention.
Figure 9 illustrates an embodiment of the invention, with a secondary coupling.
A Description in More Detail of a Set of Embodiments of the Invention
In Figure 4, a spring structure according to an embodiment of the invention is illustrated as an example, the structure being arranged to couple the masses Ml and M2 vibrating on a common axis into opposite phase vibration. Thus, in the structure according to an embodiment of the invention, there is a spring structure 401, 402, 403, 404a, 404b, 404c coupling the two masses, which spring structure is composed of two stiff bars 402 and a bending spring 404a, 404b, 404c connecting the two bars 402. The bars are suspended 403 such, that they are allowed to turn about a support point located in one end. At the other end, the bars are connected 401 to the masses Ml, M2 to be coupled. In Figure 4, a simple example of the spring structure according to the embodiment of the invention is presented.
In Figure 5 a spring structure according to an embodiment of the invention is illustrated as an example, the structure being arranged with a view to an angular velocity sensor structure similar to the one in Figure 2, wherein a coupling in the Y direction of the detection axis for the masses Ml and M2 has been formed by means of the structure according to the embodiment of the invention. In the Figure 5, in a Z axis angular velocity sensor structure, two springs 404a, 404b, 404c, positioned according to the embodiment of the invention are shown such, that they, at the ends, couple the masses into an opposite phase vibration mode on the detection axis.
Then, according to an embodiment of the invention, the coupling spring structures do not participate in the primary motion in any essential manner, since those said bars 402 are attached to the masses Ml and M2 with springs, which are loose in the x direction (in relation to the springs in the y direction) , but stiff in the y direction (in relation to the springs in the x direction) . In Figure 6, the primary mode of the structure is being illustrated. The coupling spring structures at the masses' ends, according to an embodiment of the invention, do not appreciably, or almost not at all, participate in the primary mode. When the structure, vibrating in primary mode, is turned about the axis (Z) perpendicular to the surface plane, Coriolis forces, equal in strength but opposite in direction, act on the moving masses in the direction of the y axis. In Figure 7, the detection mode of the Z axis angular velocity sensor structure is illustrated. The coupling spring structures 404a, 404b, 404c at the ends of the masses Ml and M2, according to an embodiment of the invention, couple the movements of the masses to each other and synchronize them into opposite phase .
As the masses get displaced toward each other, they turn the bars 402 towards each other, which bars bend the coupling spring 404a, 404b, 404c between them in a direction perpendicular to the direction of motion in accordance with Figure 7. This is the weakest bending mode of the centrally located spring connecting the bars.
A blow or an external linear acceleration component in the direction of the detection axis causes a displacement in both masses in the same phase. As the masses are displaced in the same direction, the bars turn in the same direction, which forces the coupling spring into an S-shaped bending in accordance with Figure 8. In this S-mode, the spring is considerably stiffer than in the case above. By suitable dimensioning, the coupling spring structure can be made even equally or over 4 times stiffer to displacement of the masses in the same direction than to opposite phase displacement. In an embodiment the spring can be designed to be even 10 times stiffer to in-phase deflection compared to anti-phase deflection .
According to an embodiment of the invention, a system of micromechanical resonators comprises at least one micromechanical resonator that comprises two masses (Ml M2) that are coupled in direction of their common motion axis with spring structure (401, 402, 403, 404a, 404b, 404c)that comprises at least two beams (402) connected to the masses and spring suspension (404a, 404b, 404c) parallel to the motion axis coupling the beams that deflects perpendicularly to the motion . According to an embodiment of the invention, the structure according to that comprises means for connecting an electric voltage between a first part of the resonator and a second part in order to provide a capacitive structure between said parts, to be used for producing a capacitively readable signal, when the motion according to vibration of the spring structure changes the distance, and thus the capacitance, between said first and second parts. According to an embodiment of the invention, there is a multitude of said connecting means to be used in producing a multitude of signals .
According to one embodiment of the invention, at least one of the bars at the end is arranged with regard for piezoelectric effects for providing an excitation structure. According to one embodiment of the invention, one of said end bars is arranged to change its form in response to an electric signal being applied to it. According to one embodiment of the invention, one of said bars is arranged such, that the piezoelectric voltage corresponding to its bending can be measured at a certain part of the bar, to be used in the filtering of interference and/or other signal processing.
Advantages of the embodiments of the invention, compared to prior art as such, are extremely modest space usage requirement and linear attachment. Compared to the seesaw type suspension, the solution according to the embodiment of the invention takes about half as much space, whereby additionally an advantage of the structure according to the embodiment of the invention is the possibility of positioning it along the edge of the component, due to its long spring. According to one embodiment of the invention, a navigator can be provided, which includes a function, in which the direction of motion at a certain point in time can be determined by means of the angular velocity determined by a certain sensor of the navigator and by means of a clock.
According to one variant of the embodiment, there is no need to be restricted to exclusively planar examination in the location determination.
The attachment points to the masses of the suspension according to one embodiment of the invention are located on the same straight line extending in the direction of the motion axes. Due to that, the reaction forces of the spring do not induce a moment on the masses, like e.g. a seesaw spring. Furthermore, the suspension can be designed such, that it will not participate in any significant manner, if at all, in the masses' motions in the directions of other axes.

Claims

Patent Claims
1. A micro-mechanical resonator, comprising two masses (Ml, M2 ) coupled in the direction of their common motion axis of motion by a spring structure (401, 402, 403, 404a, 404b, 404c) such, that the spring structure comprises a spring (404a, 404b, 404c) coupling at least a certain first bar connected to the masses and a certain second bar extending in the motion axis direction, the spring being arranged to bend in a direction perpendicular to the motion direction of the motion axis .
2. Micro-mechanical resonator according to Claim 1, characterized in, that its spring structure is arranged to bend into s-shape by a displacement of the masses in the same direction .
3. Micro-mechanical resonator according to Claim 1 or 2, characterized in, that its spring structure is arranged to be stiffer to a displacement of said masses in the same phase than to displacement in opposite phase.
4. Micro-mechanical resonator according to any one of the preceding claims, wherein at least one of said two masses (Ml, M2 ) has a comblike structure.
5. Micro-mechanical resonator according to any one of the preceding claims, wherein said comblike structure is provided in order to achieve a certain surface area.
6. Micro-mechanical resonator according to any one of the preceding claims, wherein said comblike structure is provided in order to achieve a certain capacitance between a certain part of the resonator and some part other than the comb structure .
7. A micro-mechanical resonator matrix, comprising at least one micro-mechanical resonator according to one of the preceding claims.
8. A sensor, comprising at least one micro-mechanical resonator according to one of the preceding claims.
9. A vehicle, comprising a sensor according to Claim 8, said vehicle being at least one of the following: A toy, a piece of footwear, a bicycle, a moped, a motorcycle, a car, a train, a ship and an airplane.
10. A navigation device, comprising a sensor according to Claim 8.
11. A system of micromechanical resonators comprising at least one micromechanical resonator that comprises two masses (Ml M2 ) that are coupled in direction of their common motion axis with spring structure (401, 402, 403, 404a, 404b, 404c) that comprises at least two beams (402) connected to the masses and spring suspension (404a, 404b, 404c) parallel to the motion axis coupling the beams that deflects perpendicularly to the motion.
PCT/FI2010/050159 2009-03-02 2010-03-01 Micro-mechanical sensor of angular velocity WO2010100333A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
EP10748387.7A EP2404138B1 (en) 2009-03-02 2010-03-01 Micro-mechanical sensor of angular velocity
JP2011552480A JP5670356B2 (en) 2009-03-02 2010-03-01 Angular velocity micromechanical sensor
KR1020117022831A KR101676264B1 (en) 2009-03-02 2010-03-01 Micro-mechanical sensor of angular velocity
CN201080014785.8A CN102365524B (en) 2009-03-02 2010-03-01 Micro-mechanical sensor of angular velocity
IL214925A IL214925A0 (en) 2009-03-02 2011-09-01 Micro-mechanical resonator

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FI20095201A FI20095201A0 (en) 2009-03-02 2009-03-02 Oscillating micromechanical angular velocity sensor
FI20095201 2009-03-02
FI20095903 2009-09-02
FI20095903A FI122232B (en) 2009-03-02 2009-09-02 Micromechanical angle sensor

Publications (1)

Publication Number Publication Date
WO2010100333A1 true WO2010100333A1 (en) 2010-09-10

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PCT/FI2010/050160 WO2010100334A1 (en) 2009-03-02 2010-03-01 Vibrating micro-mechanical sensor of angular velocity

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US (2) US8997565B2 (en)
EP (2) EP2404139B1 (en)
JP (2) JP5670356B2 (en)
KR (2) KR101673887B1 (en)
CN (2) CN102365524B (en)
FI (2) FI20095201A0 (en)
IL (2) IL214925A0 (en)
TW (2) TWI481817B (en)
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