WO2002014787A1 - Mikromechanischer drehratensensor und verfahren zu seiner herstellung - Google Patents
Mikromechanischer drehratensensor und verfahren zu seiner herstellung Download PDFInfo
- Publication number
- WO2002014787A1 WO2002014787A1 PCT/EP2001/009066 EP0109066W WO0214787A1 WO 2002014787 A1 WO2002014787 A1 WO 2002014787A1 EP 0109066 W EP0109066 W EP 0109066W WO 0214787 A1 WO0214787 A1 WO 0214787A1
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- WIPO (PCT)
- Prior art keywords
- rotation rate
- rate sensor
- sensor according
- micromechanical rotation
- wafer
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
- G01C19/5705—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using masses driven in reciprocating rotary motion about an axis
- G01C19/5712—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using masses driven in reciprocating rotary motion about an axis the devices involving a micromechanical structure
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49007—Indicating transducer
Definitions
- the present invention relates to a micromechanical rotation rate sensor according to the preamble of claim 1, and a method for producing a micromechanical rotation rate sensor.
- Gimbal-suspended, micromechanical rotation rate sensors have e.g. two oscillating frames with a central inertial mass. The mass is brought to resonant vibrations around an excitation axis by an electrostatic drive. When the sensor rotates about an axis of rotation that is perpendicular to the excitation axis, the Coriolis force acts on the oscillating inertial mass. As a result, an oscillation is periodically excited about a readout axis, which is directed perpendicular to the excitation axis and to the axis of rotation. The amplitude of the oscillation thus generated is a direct measure of the yaw rate to be measured. The reading of the amplitude can e.g. electrostatically.
- Such micromechanical rotation rate sensors can e.g. in automotive engineering, in aerospace engineering, and in exploration and production processes.
- the rotation rate sensors can be used for vehicle stabilization, for driving dynamics control and for navigation systems or also within systems for autonomous driving.
- platforms of this type can be stabilized and their position regulated.
- Navigation systems e.g. GPS / INS are supplemented by such rotation rate sensors, especially in the field of avionics.
- Drill heads can be controlled with rotation rate sensors.
- rotation rate sensors are used to control robots.
- US Pat. No. 4,598,585 describes a yaw rate sensor with a gimbal structure in which a frame is mounted such that it can vibrate about a y-axis. Inside the frame is an element that is vibratable about an x-axis on the Frame is attached. An inertial mass is arranged on the inner element. Drive elements serve to set the frame in vibration around the y-axis. The deflection of the inner element due to the Coriolis force is measured capacitively.
- the known micromechanical rotation rate sensors have the disadvantage that the measurement accuracy is often inadequate. Very large cross-sensitivities usually also occur. In addition, there is often a high sensitivity to vibrations. In addition, the known yaw rate sensors are usually associated with high manufacturing costs.
- the object of the invention is therefore to create a micromechanical rotation rate sensor and to provide a method for its production which has a high sensor sensitivity and low cross sensitivity.
- the rotation rate sensor should be robust, have low sensitivity to mechanical vibrations and be inexpensive to manufacture.
- micromechanical yaw rate sensor according to claim 1 and the method for producing a micromechanical yaw rate sensor according to claim 22. Further advantageous features, details and aspects of the invention are evident from the dependent claims, the description and the drawings.
- the micromechanical rotation rate sensor comprises a first oscillating element, which is pivotably mounted about a first axis, a second
- Vibrating element which is pivotally mounted about a second axis, which is directed perpendicular to the first axis, an excitation unit to set the first vibrating element in vibration about the first axis and a readout unit for detecting vibrations of the second vibrating element about the second axis, wherein at least two additional mass elements are attached to the first oscillating element, which are aligned symmetrically to a plane which is defined by the first and second axes.
- the symmetrically aligned, additional mass elements result in a significantly higher sensor resolution and sensitivity.
- the additional masses or additional mass elements can be made extremely large. This results in a wide outsourcing of the center of gravity symmetrically to the axis of rotation, which causes an extreme increase in sensor sensitivity.
- the symmetrical structure reduces the cross-sensitivity to yaw rates outside the sensitivity axis of the sensor and reduces the sensitivity to acceleration acting on the sensor.
- the sensor is inexpensive to manufacture and can be designed to be extremely robust.
- the common center of gravity of the two mass elements advantageously lies at the intersection of the first and second axes. This results in maximum symmetry.
- the additional mass elements are preferably manufactured separately from the first and / or second oscillating element, in particular the shape, size or material of the mass elements being specifically selected in order to determine the parameters of the sensor.
- the mass distribution, the total mass and the distribution of the moments of inertia of the sensor can be specifically selected. This results in additional configuration options for optimizing the sensor with regard to resolution, cross-sensitivity, shock sensitivity, reduced influence of manufacturing tolerances, or reduced sensitivity to vibrations.
- the free choice of materials for the additional mass elements allows additional masses to be formed with special physical properties that are particularly suitable depending on the requirements of the rotation rate sensor.
- the sensor element can be trimmed by a special choice of the additional masses, without changes or effects having to be made to the other structures or to the etched-out gimbal structure.
- the additional masses can be manufactured inexpensively with high precision.
- Balls are particularly preferably used as mass elements, which can be produced inexpensively with a very low geometry tolerance of, for example, 0.1%.
- the use of balls results in a very high reproducibility of the mass distribution of the rotation rate sensor.
- Cuboids, cones, pyramids or truncated pyramids and cylinders can also be used as mass elements, which can also be produced very inexpensively and with a low geometry tolerance. It is particularly favorable to arrange the cones or pyramids with their tips aligned with one another. As a result, the focal points of the individual mass elements are outsourced as far as possible or as far apart as possible.
- the additional mass elements e.g. magnetic properties. This causes a mutual attraction of the additional mass elements so that they align themselves completely symmetrically. Further advantages are the resulting adhesion to the substrate, the possibility of self-calibration, and the
- the additional mass elements are preferably made of a material that has a higher density than the material of the first and / or the second oscillating element. This leads to a more favorable distribution of the moments of inertia.
- e.g. Metals, in particular steel are used as material for the additional mass elements, whereas where for the rest of the sensor structure or for the first and second vibrating elements, e.g. Silicon is used.
- the additional masses are not compatible with the processing steps e.g. must be for a silicon wafer from which the oscillating elements or the oscillatable structure is advantageously produced. This can result in an extreme increase in sensor sensitivity in a very cost-effective manner.
- the first oscillating element is a rocker and the second oscillating element is a frame, the rocker and the frame forming a cardanic, oscillatable structure, which is fastened in a holding structure.
- the rotation rate sensor is advantageously produced from at least three joined wafers, which are preferably processed individually.
- the rotation rate sensor has, for example, a bottom wafer, a middle part wafer and a lid wafer. This results in a reduced complexity in the manufacturing process, as well as the possibility to test the individual components. Furthermore, the yield is increased, which results in reduced costs for the sensors. Furthermore, pit and electrode structures that are inside the sensor after being assembled can be freely designed.
- the first and the second oscillating element are preferably formed in the central part wafer.
- the middle part wafer can be processed on the top and bottom. This ensures symmetry with the center plane, since the masses or additional mass elements can be attached symmetrically. The temperature drift of the sensor properties is reduced by the symmetry.
- the bottom and / or the lid wafer is advantageously made of alkali-containing glass wafers, such as, for example, borofloat or pyrex glass, of which, for example, at least one wafer is provided with an electrode structure. Scattering and crosstalk capacities are thereby reduced, since the electrode structure is located on insulating material.
- the thermal expansion coefficient is adapted to the silicon of the middle part wafer, which is why the thermal stresses during production can be kept low and which results in a reduced temperature sensitivity of the sensor during operation.
- the use of alkali-containing glass wafers also enables a reliable connection to the middle part wafer made of silicon by means of an anodic bonding process.
- the gap distance between the middle part wafer and the bottom wafer or between the middle part wafer and the lid wafer is small in relation to the lateral electrode extension.
- This distance between adjoining wafers is used for electrostatic excitation and / or for capacitive readout of the actuator and / or sensor oscillation of the oscillating elements.
- the relationship between the gap distance and the lateral electrode extension is e.g. less than 1:20, preferably less than 1:50, and particularly preferably less than 1: 100 or even 1: 1000. This results in very large capacitance values, which in turn produce high electrical signals for the sensors or large electrostatic forces for the actuators enable.
- the gap distance for the actuator structure which enables the excitation vibration of the first vibration element, is preferably greater than the gap distance for the sensor structure, which enables the read-out vibration of the second vibration element.
- the actuator oscillation can take place with a very high mechanical amplitude.
- the damping of the vibration is lower with a larger gap distance (squeezed film damping), which leads to a higher mechanical amplitude with resonant excitation.
- the small gap distance in the sensor structure results in a large capacitance and thus a high electrical output signal.
- the wafer from which the mechanical structure or the first and second oscillating element is etched is advantageously made from single-crystal silicon.
- the vibratable structure or gimbal structure of the sensor is made, for example, of a full wafer etched, ie manufactured in bulk technology.
- the structure capable of oscillation comprises, for example, the first and second oscillation elements and is preferably structured out of the middle part wafer.
- the use of monocrystalline silicon results in a very low material damping and, furthermore, negligible signs of fatigue and aging.
- the production in silicon technology leads to low
- silicon has a high mechanical strength with low density, which results in a robust and resilient mechanical structure.
- the first and / or the second oscillating element is non-rectangular, i.e. the structure capable of vibrating has a non-right-angled geometry or a symmetrical convex free form.
- the vibrating elements can e.g. be round or have edges that adjoin each other at an angle of more than 90 °.
- the vibrating elements can be 8-cornered.
- the torsion frequency is essentially determined by the torsion or rotating band as the suspension itself.
- the rotary band can thus be shortened considerably and a Z-mode of the sensor that can be set almost independently of the torsion frequency and is directed perpendicular to the wafer plane can be achieved.
- Non-right-angled geometries can be found in which the torsional natural frequencies of the rocker or the inner vibratable structure and the frame or the outer vibratable structure are the lowest eigenmodes of the structure and all other modes come to lie at significantly higher frequencies. This enables the required frequency spacing between the mechanical interference spectrum, for example in a harsh environment, and the operating and eigenmodes of the sensor to be guaranteed.
- Coriolis force is generated, the lowest eigenmodes of the vibratable structure, which is formed by the first and the second vibrating element. This results in a high robustness of the mechanical structure against shock loads and mechanical vibrations.
- the rotation rate signal has a bandwidth of 0 to 100 Hz, for example.
- Low-frequency interference signals the bandwidth of which is comparable to the bandwidth of the rotation rate, cannot or only very strongly suppresses the sensor behavior due to the position of the natural frequencies of the sensor structure.
- the area ratio between the second vibrating element and the first vibrating element is greater than 5: 1, preferably greater than 10: 1.
- This area ratio between the frame, which forms the outer sensor structure or the second vibrating element, and the rocker, which forms the inner actuator structure or the first vibrating element, results in a further increase in the electrical capacity
- the micromechanical rotation rate sensor preferably has a metallization to form an electrode or electrode structure which is covered with a dielectric layer. This results in passivation, so that the metallization is protected against corrosion. Leakage currents between the insulated electrodes are significantly reduced. Since the metallization in particular only sits on fixed, stationary parts of the sensor, there are hardly any restrictions with regard to the type and the method of passivation.
- the micromechanical rotation rate sensor advantageously comprises one or more electrodes, which are surrounded by a closed conductor track.
- the conductor track can be contacted specifically.
- the corresponding supply lines can also be surrounded by the closed conductor track. This measure reduces the electrical crosstalk between the electrodes for the sensors and / or for the actuators. Since the metallized electrodes e.g. only in the lid and / or bottom wafer and not in this case on the structured middle part, the Guardel electrodes are easy to contact and have less constraints in terms of their geometry and properties than if they had to be attached to the middle part.
- the micromechanical rotation rate sensor preferably has an ohmic pressure contact for connecting the middle part wafer to the bottom wafer or to a bond pad of the bottom wafer.
- the lid wafer can also be contacted in this way.
- the entire structure of the middle part wafer has an electrical potential. This makes it possible for the middle part wafer to be electrically connected via standardized wire bond pads which, for example, have a size of 100 ⁇ m ⁇ 100 ⁇ m. As a result, the entire connection pads can be located on one level and arranged side by side. This considerably reduces the effort involved in electrically contacting the sensor element with the associated electronics for actuators and sensors.
- the manufacturing effort of the middle part wafer is significantly reduced. Furthermore, the structure capable of oscillation shows only very low material damping and has no mechanical tension. This also contributes to a reduced temperature dependence of the sensor properties.
- the sensor interior can be hermetically sealed, e.g. buried conductor tracks for contacting the electrodes in the sensor interior.
- the connection between the bond pads and the electrode surfaces in the interior of the sensor by means of buried conductor tracks means that the interior of the sensor can be hermetically sealed and can therefore neither become dirty nor corrode or be changed by moisture or other environmental influences.
- the method according to the invention for producing a micromechanical yaw rate sensor comprises the steps: providing at least three wafers; Structuring the individual wafers, a cardanic, oscillatable structure being formed in one of the wafers; Forming an excitation unit to excite a first vibration of the structure; Forming a readout unit for detecting a second vibration of the structure, which is perpendicular to the first vibration; and joining the wafers, wherein the wafer with the oscillatable structure is connected to a further wafer on both sides.
- This method makes it possible to arrange extremely large symmetrical additional masses on the oscillatable middle section and thereby achieve a significantly higher sensor resolution.
- additional mass elements can be attached to the vibratable structure symmetrically to the axis of the first and / or the second vibration.
- the wafer with the vibratable structure can be processed on its top and bottom.
- the vibratable structure or gimbal structure of the sensor is etched from a single, full wafer, and the suspension of the mechanical or vibratable structure, which forms the middle part of the sensor, is produced in a single etching step.
- This achieves a high degree of manufacturing accuracy of the geometric structure or structure capable of vibrating, since e.g. there is no need to adjust several masks to each other.
- the middle part itself is therefore symmetrical with high accuracy top-bottom. This excludes an essential source for the quadrature error.
- There is also a free design of the lateral geometry e.g. when using the anisotropic plasma etching technique.
- a metallization structure is applied to the bottom wafer of the three wafers by means of thin-film technology, which forms, for example, capacitor areas, supply lines and connection pads.
- thin-film technology forms, for example, capacitor areas, supply lines and connection pads.
- Thin-film technology enables the production of small structures with reproducible thicknesses, which are necessary for a reproducible gap distance.
- the conductor track width is 10 ⁇ m
- the conductor track and electrode thickness is 140 nm
- the gap distance is, for example, 1.5 ⁇ m.
- the electrical connection of the sensor element to the actuator and sensor electronics takes place, for example, via standardized wire bond pads. Their size is, for example, 100 ⁇ m x 100 ⁇ m.
- the rotation rate sensor or the first oscillation element can be excited in a variety of ways, for example electrostatically, piezoelectrically, magnetostrictively or also magnetically or using additional magnetic masses.
- the rotation rate sensor is provided with electrostatic, piezoelectric, magnetostrictive or also magnetic elements or additional magnetic masses.
- a control device can be provided which has electronics for regulating and / or forcing the excitation oscillation.
- the electronics can be designed by appropriate circuits so that the first oscillating element oscillates in its iron frequency.
- it can also be designed in such a way that the oscillation of the first oscillating element is forced at a specific frequency, which does not have to be the natural frequency.
- the influence of the readout electrodes for measuring the vibration of the second vibrating element is further minimized.
- the individual electrodes of a pair of excitation electrodes can be divided and controlled separately by the electronics in order to switch off or compensate for the above-mentioned influence.
- the readout method can also be implemented in several known ways and in particular e.g. capacitively or optically.
- the rotation rate sensor is provided with capacitances or optical elements for reading out the vibration of the second vibration element generated by the Coriolis force.
- FIG. 1 shows a section through a micromechanical rotation rate sensor according to a preferred embodiment of the invention
- FIG. 2 shows a plan view of the middle part of the rotation rate sensor according to the preferred embodiment
- Fig. 4 is a section showing the edge region of the sensor with the connection between the middle part and the bottom part.
- FIG. 1 shows a micromechanical rotation rate sensor 10, which is formed from a cover part 1, a middle part 2 and a bottom part 3. These parts are individually processed wafers that were finally assembled.
- the middle part 2 forms an oscillatable structure with a first oscillating element 4 and with a second oscillating element 5.
- the first oscillating element 4 forms a rocker and the second oscillating element 5 forms a frame in which the rocker can be pivoted about a first
- Axis of rotation A is mounted.
- the frame or the second oscillating element 5 is mounted within the sensor so as to be pivotable about a second axis of rotation B, which runs perpendicular to the first axis of rotation A in the wafer plane.
- the additional mass elements 6a, 6b are arranged symmetrically to the central part 2 or to the central part plane, which is formed by the axes of rotation A and B.
- the additional mass elements 6a and 6b are arranged symmetrically to the axis of rotation A and symmetrically to the axis of rotation B, ie there is symmetry to the two axes of rotation A and B and to the intersection of the two axes of rotation A and B.
- Electrodes 7 together with a controller (not shown) form an excitation unit in order to set the first vibrating element 4 or the rocker in vibrations about the axis of rotation A.
- Further electrodes 8 together with electronics (not shown) form a readout unit in order to detect the vibrations of the second vibrating element 5 or the frame about the axis of rotation B. The vibrations are excited and read out electrostatically or capacitively.
- the middle part 2 has an electrical potential.
- the gap distances d, e1, e2 serve for electrostatic excitation or for the capacitive readout of the actuator and sensor vibration of the oscillatable structure of the middle part 2.
- the gap distances d, e 1, e2 are in relation to the lateral extension of the electrode structure or to the lateral extension of the Electrodes 8, which are used to read the vibration of the frame or second vibrating element 5, are very small.
- the ratio of the gap distance d and the gap distance e2 to the lateral extension of the electrode 8 is approximately 1: 100 or less. This results in very high capacitance values for the sensors or large electrostatic forces for the actuators.
- the gap distance e 1 between the base part 3 and the first vibrating element 4, which enables the first vibrating element 4 to be tilted or pivoted about the axis of rotation A, is greater than the gap distance e2 between the bottom part 3 and the second vibrating element or frame 5, the the tilting around the axis of rotation B enables.
- This enables a large mechanical amplitude for resonant excitation, while on the other hand a high electrical output signal is achieved due to the small gap distance in the reading and the associated large capacity.
- the lid part 1 has at its edge a projection 11 through which it is firmly connected to the edge 21 of the middle part.
- a projection 11 By the projection 1 1 or the thereby formed, raised compared to the central region of the lid part, an interior 9 is formed within the sensor 10, the two vibrating elements 4, 5 and the vibratable structure enough space to perform the excitation or. Readout vibration offers.
- the bottom part 3 also has on its surface a protruding connection area or area 31 which is used to connect the
- Bottom part 3 serves to the middle part 2 and thereby offers space for the vibrations.
- the base part 3 which can be a base wafer or part of a base wafer, has a greater lateral extent than the other wafer parts or wafers which form the cover part 1 and the middle part 2. In other words, the bottom part 3 has an edge region which extends beyond the edge of the middle part 2 or the cover part 1.
- Contact surfaces 32 in the form of connection pads are provided on the surface of the base part 3 or of the wafer in the edge region, which serve to contact the metallizations or electrodes 7, 8 in the interior 9 of the sensor.
- the contact surfaces 32 are connected to the electrodes 7, 8 via conductor tracks 33, the contact surfaces 32, the conductor tracks 33 and the electrodes 7, 8 being formed in one plane on the surface of the base part 3 or lower wafer.
- the conductor tracks 33 are buried conductor tracks, i.e. they are integrated or incorporated into the wafer. This results in a hermetic or vacuum-tight closure of the interior 9.
- FIG. 2 shows a top view of the middle part 2, which can be part of a wafer or also an entire wafer, of the rotation rate sensor according to the preferred embodiment.
- the inner vibrating element 4 or the rocker is connected to the outer vibrating element 5 or frame by means of two opposite, oscillatory or torsional suspensions 41.
- the oscillating suspension 41 allows the rocker to tilt or swing about the axis A, which extends through the two suspensions 41.
- the frame or the outer vibrating element 5 is u
- the vibration-capable suspension 42 of the frame or second vibration element 5 on the holding structure 21 allows the frame to tilt or swing about the axis B, which extends through the two suspensions 42 and is oriented perpendicular to the axis of rotation A of the first vibration element 4.
- the upper additional mass element 6a is fastened symmetrically in the center of the vibratable structure formed from the rocker and frame and at the same time in
- the second additional, identically designed mass element 6b is arranged directly below (see FIG. 1).
- the vibrating elements 4, 5 have edges 4a, 5a, which are not aligned at right angles to one another, but form an angle ⁇ which is greater than 90 ° C.
- the structure capable of oscillation which consists of the two oscillation elements 4 and 5 has a non-right-angled geometry, by means of which an enlargement of the capacitance areas is achieved with a higher flexural rigidity and thus higher natural frequencies of the frame.
- the suspension 42 or the hinge of the frame can also be greatly shortened. Overall, the natural frequency spectrum of the mechanical structure can be made more economical due to the non-rectangular geometry. The other advantages of the non-rectangular geometry have already been described above.
- FIG. 3 shows a top view of a metallization formed on the base part 3.
- the metallization forms the two flat electrodes 8, which are used for capacitive reading of the vibration of the frame or second vibrating element 5, which is generated due to the Coriolis force when the sensor rotates about a sensitive axis directed perpendicular to the axes of rotation of the vibrating elements 4 and 5 ,
- the electrodes 7 are not shown here, but are configured similarly.
- the entire structure of the middle part wafer or middle part 2 has an electrical potential which corresponds to the metallizations or electrodes 7, 8 on the bottom part 2 opposite. As a result, it is not necessary to also apply metallizations to the vibratable structure, which are opposite the electrodes 7, 8 for excitation and for reading (see FIG. 1).
- Each electrode 7, 8 is completely surrounded by a ring electrode 12, which encloses both the electrode 7, 8 and the conductor track 33 leading to the outside and the external contact surface 32.
- the ring electrode 12 can be contacted separately via its own contact surface 34 located outside the sensor interior.
- the ring electrode 12, which forms a conductor track, reduces the electrical crosstalk between the electrodes 7, 8 for sensors and actuators.
- Figure 4 shows the connection between the middle part 2 and the bottom part 3 in the edge region of the sensor 10 in an enlarged view.
- the middle part wafer or middle part 2 is connected via an ohmic pressure contact 35 to a bond or connection pad of the bottom wafer 3, which is designed in the form of a contact surface 36 on the bottom part 3.
- the entire connection pads are on one level and are arranged side by side.
- the middle part wafer 2 consists of single crystal
- bottom part 3 and the lid part 2 e.g. from alkali-containing glass wafers, e.g. Borofloat or Pyrex glass. At least one of the wafers is provided with an electrode structure.
- alkali-containing glass wafers e.g. Borofloat or Pyrex glass.
- At least one of the wafers is provided with an electrode structure.
- other materials are also possible for the sensor parts, the choice of material depending on the respective requirements.
- the mass elements 6a, 6b are steel balls, which are each supported in a bulge on the top and bottom of the rocker or the first oscillating element 4.
- the steel balls face each other exactly, so that a high geometry is guaranteed.
- magnetic steel balls are used which align themselves with one another.
- other shapes and materials are of course also used to design the Mass elements 6a, 6b possible, the sensor parameters being able to be set by suitable selection.
- excitation methods such as piezoelectric, magnetostrictive, or magnetic excitation methods.
- the readout method can also be carried out in other known ways, wherein optical readout methods are also possible in addition to capacitive readings.
- the wafers for the cover part 1 and for the base part 3 are structured in such a way that there are recesses in their center for the mass elements 6a, 6b. are, with enough scope to carry out the vibrations.
- a central area of the respective wafer surface is also lowered relative to the edge area, so that in this area of the cover and bottom part there is a gap distance to the central part 2, which enables the oscillatable structure of the central part to oscillate.
- the middle part wafer is processed on the top and bottom so that the symmetry to the middle plane is guaranteed.
- the vibratable structure of the sensor consisting of frame and rocker, is etched from a full wafer, the suspensions 41, 42 (see FIG. 2) being produced in one etching step.
- mass elements 6a, 6b are attached to the top and bottom of the wafer, which is provided as the middle part 2, for example by gluing or magnetically.
- a metallization structure is applied by means of thin-film technology, which forms the electrodes or capacitor surfaces as well as the leads and connection pads.
- the metallization for passivation is covered with a dielectric layer.
- the symmetrical sensor effectively avoids sources of error, such as temperature drift in particular, and results in improved measurement results.
- the symmetrical additional masses on the middle part 2 result in a significantly higher sensor resolution.
- the highly symmetrical mechanical structure of the sensor leads to high long-term stability and low offset drift. This means that the sensor works stably over the long term and delivers more precise measurement results. It can be subjected to mechanical loads without the measurement results being falsified under such loads.
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Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2002519873A JP2004506883A (ja) | 2000-08-18 | 2001-08-06 | マイクロメカニカル回転速度センサおよびその製造方法 |
| EP01980234A EP1309835A1 (de) | 2000-08-18 | 2001-08-06 | Mikromechanischer drehratensensor und verfahren zu seiner herstellung |
| US10/344,925 US6898972B2 (en) | 2000-08-18 | 2001-08-06 | Micromechanical speed sensor |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10040537.1 | 2000-08-18 | ||
| DE10040537A DE10040537B4 (de) | 2000-08-18 | 2000-08-18 | Mikromechanischer Drehratensensor und Verfahren zu seiner Herstellung |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2002014787A1 true WO2002014787A1 (de) | 2002-02-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/EP2001/009066 Ceased WO2002014787A1 (de) | 2000-08-18 | 2001-08-06 | Mikromechanischer drehratensensor und verfahren zu seiner herstellung |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6898972B2 (enExample) |
| EP (1) | EP1309835A1 (enExample) |
| JP (1) | JP2004506883A (enExample) |
| DE (1) | DE10040537B4 (enExample) |
| WO (1) | WO2002014787A1 (enExample) |
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| EP1455162A1 (en) * | 2003-03-06 | 2004-09-08 | Samsung Electronics Co., Ltd. | Rotary gyroscope |
| EP1342988A3 (en) * | 2002-03-07 | 2006-08-23 | Alps Electric Co., Ltd. | Capacitive sensor |
| EP1342986A3 (en) * | 2002-03-07 | 2006-08-23 | Alps Electric Co., Ltd. | Capacitive sensor |
| US7102268B2 (en) * | 2003-05-13 | 2006-09-05 | Sony Corporation | Micromachine and method of fabricating the same |
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| DE10231730B4 (de) * | 2002-07-13 | 2012-08-30 | Robert Bosch Gmbh | Mikrostrukturbauelement |
| DE10347215A1 (de) * | 2003-10-10 | 2005-05-12 | Bosch Gmbh Robert | Mikromechanischer Sensor |
| CA2601384A1 (en) * | 2005-03-16 | 2006-10-26 | Cluster Resources, Inc. | Automatic workload transfer to an on-demand center |
| US7387040B2 (en) * | 2005-08-19 | 2008-06-17 | Honeywell International Inc. | Methods and systems for mounting sensors for use in a harsh vibration environment |
| JP5165294B2 (ja) * | 2007-07-06 | 2013-03-21 | 三菱電機株式会社 | 静電容量式加速度センサ |
| DE102013212365A1 (de) | 2013-06-27 | 2014-12-31 | Robert Bosch Gmbh | Kapazitiver Drehratensensor und Verfahren zum Herstellen eines kapazitiven Drehratensensor |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| DE3509948A1 (de) * | 1984-03-19 | 1985-09-26 | The Charles Stark Draper Laboratory, Inc., Cambridge, Mass. | Planarer traegheitssensor |
| US5016072A (en) * | 1988-01-13 | 1991-05-14 | The Charles Stark Draper Laboratory, Inc. | Semiconductor chip gyroscopic transducer |
| US5195371A (en) * | 1988-01-13 | 1993-03-23 | The Charles Stark Draper Laboratory, Inc. | Semiconductor chip transducer |
| US5203208A (en) * | 1991-04-29 | 1993-04-20 | The Charles Stark Draper Laboratory | Symmetrical micromechanical gyroscope |
| US6032531A (en) * | 1997-08-04 | 2000-03-07 | Kearfott Guidance & Navigation Corporation | Micromachined acceleration and coriolis sensor |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5329815A (en) * | 1991-12-19 | 1994-07-19 | Motorola, Inc. | Vibration monolithic gyroscope |
| US5408877A (en) * | 1992-03-16 | 1995-04-25 | The Charles Stark Draper Laboratory, Inc. | Micromechanical gyroscopic transducer with improved drive and sense capabilities |
| DE19523895A1 (de) * | 1995-06-30 | 1997-01-02 | Bosch Gmbh Robert | Beschleunigungssensor |
| DE19641284C1 (de) * | 1996-10-07 | 1998-05-20 | Inst Mikro Und Informationstec | Drehratensensor mit entkoppelten orthogonalen Primär- und Sekundärschwingungen |
| DE19745083A1 (de) * | 1997-10-11 | 1999-04-15 | Bodenseewerk Geraetetech | Drehratensensor |
-
2000
- 2000-08-18 DE DE10040537A patent/DE10040537B4/de not_active Expired - Fee Related
-
2001
- 2001-08-06 WO PCT/EP2001/009066 patent/WO2002014787A1/de not_active Ceased
- 2001-08-06 EP EP01980234A patent/EP1309835A1/de not_active Withdrawn
- 2001-08-06 US US10/344,925 patent/US6898972B2/en not_active Expired - Fee Related
- 2001-08-06 JP JP2002519873A patent/JP2004506883A/ja not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3509948A1 (de) * | 1984-03-19 | 1985-09-26 | The Charles Stark Draper Laboratory, Inc., Cambridge, Mass. | Planarer traegheitssensor |
| US5016072A (en) * | 1988-01-13 | 1991-05-14 | The Charles Stark Draper Laboratory, Inc. | Semiconductor chip gyroscopic transducer |
| US5195371A (en) * | 1988-01-13 | 1993-03-23 | The Charles Stark Draper Laboratory, Inc. | Semiconductor chip transducer |
| US5203208A (en) * | 1991-04-29 | 1993-04-20 | The Charles Stark Draper Laboratory | Symmetrical micromechanical gyroscope |
| US6032531A (en) * | 1997-08-04 | 2000-03-07 | Kearfott Guidance & Navigation Corporation | Micromachined acceleration and coriolis sensor |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1342988A3 (en) * | 2002-03-07 | 2006-08-23 | Alps Electric Co., Ltd. | Capacitive sensor |
| EP1342986A3 (en) * | 2002-03-07 | 2006-08-23 | Alps Electric Co., Ltd. | Capacitive sensor |
| EP1455162A1 (en) * | 2003-03-06 | 2004-09-08 | Samsung Electronics Co., Ltd. | Rotary gyroscope |
| US7043987B2 (en) | 2003-03-06 | 2006-05-16 | Samsung Electronics Co., Ltd. | Rotary gyroscope |
| CN100340841C (zh) * | 2003-03-06 | 2007-10-03 | 三星电子株式会社 | 旋转回转仪 |
| US7102268B2 (en) * | 2003-05-13 | 2006-09-05 | Sony Corporation | Micromachine and method of fabricating the same |
Also Published As
| Publication number | Publication date |
|---|---|
| DE10040537A1 (de) | 2002-03-07 |
| US6898972B2 (en) | 2005-05-31 |
| DE10040537B4 (de) | 2004-05-13 |
| JP2004506883A (ja) | 2004-03-04 |
| EP1309835A1 (de) | 2003-05-14 |
| US20040011130A1 (en) | 2004-01-22 |
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