The invention relates to a component, in particular, a micromechanical, micro-electromechanical (MEMS) or rather micro-opto-electro-mechanical (MOEMS) component, which has a split, galvanically isolated active structure.
Micro-electromechanical components (MEMS) or rather micro-opto-electro-mechanical components (MOEMS) often comprise active structures. In this connection, in particular, mobile structures or structures, which equally include mobile and optical components (e.g. mobile mirrors), are to be understood by “active structure”. The term “active area” designates the area or rather volume of the component, in which the active structure lies or rather moves.
In micromechanical sensors, such as accelerometers and gyros, which are based on the function of a mechanical oscillator, i.e. on the movement of an active structure, both the drive of the oscillator and the detection of the deflection of the oscillator can be realized via movable electrodes on the active structure and fixed electrodes of the component. Essentially, there are two possibilities for this:
In a direct current method (DC method), the movable structure is connected to ground. Separate electrodes are used for the drive and detection functions, wherein the drive function must take into account the quadratic dependency of the drive force of the voltages applied. The detection function is based either on a measurement of charge transfers on electrodes biased with direct voltage or on a measurement of the capacitances of the detection electrodes. In the first case, no detection can be made due to charge drifts at zero frequency, which, for example, is given for a constant acceleration in accelerometers, in the second case, disruptive capacitances are measured, which reduces the accuracy to be achieved.
In a carrier frequency method, the movable structure is at the inlet of a charge amplifier and, thus, is connected to virtual ground. The charge amplifier provides the detection signal. The same electrodes are used for drive and detection, wherein drive and detection are realized separately, for example, through time multiplex in two phases. A direct voltage is applied in the drive phase, while a voltage with a carrier frequency is applied to the electrodes in the detection phase. In the simplest case, the carrier frequency can include a defined voltage jump and causes a deflection-dependent charge transfer on the movable electrode, which is then detected by the charge amplifier. In doing so, disruptive interactions between drive and detection can emerge. In sensors with a plurality of levels of freedom, for example, gyros or sensors with double oscillators, it can be necessary to use a complicated time multiplex method, in order to enable a separation of individual detection signals.
It is, therefore, an object of the invention to provide a micromechanical component that eliminates the aforementioned disadvantages of possible drive and detection methods as well as a method for operating such a component. In addition, it is an object of the invention to provide a component and a method, respectively, wherein a self-mixing function can be realized for drive and detection at the operating frequency of the component.
The object is solved by the subject matter of the independent claims. Preferred embodiments can be found in the sub-claims.
Embodiments of the component according to the invention and of the method according to the invention are explained in more detail in the following text based on the figures, with similar elements being designated with identical reference numerals. In addition, elements of the embodiments shown can also be arbitrarily combined with one another, as long as nothing to the contrary is mentioned.
The term “substrate” describes structures, which consist of one material only, for example, a silicon wafer or a glass plate, which, however, can also include a composite of a plurality of layers and materials. Accordingly, the first substrate 11 and/or the second substrate 15 can be fully electrically conductive, be electrically conductive in regions only, or consist of one electrically insulating material or of electrically insulating materials. In case that the first substrate 11 consists of an electrically insulating material, the first insulation layer 12 may also not exist. Similarly, the second insulation layer 14 can be saved, if the second substrate 15 consists of an electrically non-conductive material.
Also the term “structure layer” describes structures consisting of one material only, e.g. a silicon layer, which, however, can also include a composite made of a plurality of layers and materials, as long as at least one region of the structure layer 13 is electrically conductive. The electrically conductive regions of the structure layer 13 enable the application or readout of electric potentials on predetermined regions of the structure layer 13. Preferably, the structure layer 13 is fully electrically conductive.
The first cover layer 16, which is arranged on the surface of the second substrate 15 facing away from the structure layer 13, and the second cover layer 19, which is arranged on the surface of the first substrate 11 facing away from the structure layer 13, can consist of the same material, for example, a metal, or of different materials. They can serve to shield an active area of the component 1 from external electrical fields or other environmental impacts, such as humidity. In addition, they can serve to provide a defined electric potential on the first substrate 11 and on the second substrate 15, respectively. However, the first cover layer 16 and the second cover layer 19 are optional.
The first contact surface 17 consists of a conductive material, and serves the provision or readout (detection) of an electric potential on a certain region of the structure layer 13. The contact surface 17 can be contacted by means of a wire 18, as illustrated in
In the structure layer 13 an active structure 20 is formed, which can move at least in one direction in an active area 21. The active area 21 is, for example, realized by a first recess 111 formed in a surface of the first substrate 11 facing the structure layer, and a second recess 151 formed in a surface of the second substrate 15 facing the structure layer 13. The active structure 20 comprises at least a first region 22 and a second region 23, which are each electrically conductive, and are rigidly physically connected to one another along a first axis. The first region 22 and the second region 23 are electrically insulated from one another by an insulating region 24. The insulating region 24 extends across the whole depth of the structure layer 13, i.e. it extends from a first surface 131 of the structure layer 13 continuously to a second surface 132 of the structure layer 13. The first surface 131 faces the first substrate 11, while the second surface 132 faces the second substrate 15. The insulating region 24 can, for example, be realized by an insulating material, and can—both in the top view and in cross section—be arranged arbitrarily and have arbitrary forms. This means that the insulating region 24 can, in the top view, run straight or curved, for example, and can, in cross section, run straight or curved perpendicular to the first surface 131 and to the second surface 132 or at a defined angle to those surfaces. In addition, also the width of the insulating region 24 can vary in cross section, as long as full electric insulation of the first region 22 from the second region 23 of the structure layer 13 is ensured.
A top view of the structure layer of the component 1 from
According to the first embodiment, the component 1 further comprises a fifth electrode 41, which is firmly connected to the first substrate 11 and/or to the second substrate 15 and extends outwards from it in the second direction along the second axis into the active area 21, wherein the fifth electrode 41 is arranged between the first electrode 221 and the third electrode 231. Furthermore, the component 1 can comprise a sixth electrode 51, which is firmly connected to the first substrate 11 and/or to the second substrate 15 and extends outwards from it in the first direction along the second axis into the active area 21 and is arranged between the second electrode 222 and the fourth electrode 232. Thus, the fifth electrode 41 and the sixth electrode 51 correspond to some extent to the electrode 32 or rather the electrode 33 illustrated in
In a first embodiment of the method for operating a component 1, a first voltage U0, which is a direct voltage, is applied to the first electrode 221 and to the second electrode 222, i.e. to the first region 22. The negative first voltage, i.e. −U0, is applied to the third electrode 231 and to the fourth electrode 232, i.e. to the second region 23. Thus, the first electrode 221 and the fifth electrode 41 form a first partial capacitance C1, while the third electrode 231 and the fifth electrode 41 form a second partial capacitance C2. The partial capacitances C1 and C2 induce a charge onto the fifth electrode 41, whereby:
Q=C
1
·U
0
−C
2
·U
0=(C1−C2)·U0 (1).
The fifth electrode 41 is connected to a charge amplifier 60, which comprises an operational amplifier 61 and a feedback capacitance 62. The charge amplifier 60 converts the charge Q induced onto the fifth electrode 41 into a voltage, which can be tapped at the first outlet 70. Thus, the fifth electrode 41 serves as a readout electrode, with the charge Q read out being proportional to the difference C1−C2, which is a measure for the deflection of the active structure 20, so that this deflection can be measured.
A second voltage U1 can be applied via the sixth electrode 51, wherein that voltage U1 is a drive or rather resetting voltage. The second voltage U1 can be a direct voltage, for example, in accelerometers, or an alternating voltage, for example, in gyros. With the aid of the second voltage U1, a resetting force F can be exercised on the active structure 20, wherein the resetting force F is proportional to the first voltage U0 and to the second voltage U1. The resetting force F is calculated as follows:
F=(U1−U0)2−(U1+U0)2=4·U1·U0 (2).
Since the first voltage U0 occurs both in the readout process according to formula (1) and during the resetting process according to formula (2), modulation can be conducted on the drive side and demodulation on the readout side with the aid of the first voltage U0.
If in the previously described components immersing combs are used for the first to sixth electrodes 221, 222, 231, 232, 41, and 51, so that the capacitances are a linear function of the deflection in X direction, no additional deflection-dependent forces emerge. Such an embodiment of the electrodes is illustrated in
However, if one has capacitors with parallel, approximating electrodes, as illustrated in
K=(U1−U0)2+(U1+U0)2=2U12+2U02 (3).
This effect can be used for the tuning of the resonance frequency of the active structure 20. However, this effect can also be undesired, since the negative spring constant K depends on the second voltage U1 at any time, and, therefore, can only be set jointly with the resetting force and not separate from it.
The second embodiment illustrated in
According to an embodiment for operating the component in the second embodiment, a third voltage U2 is applied to the seventh and eighth electrodes 52, 53, which serves for compensation of the spring constants of the first spring 25 and of the second spring 26, by which the active structure 20 is movably connected to the first substrate 11 and/or to the second substrate 15. The resetting force F and the spring constant K induced on the drive side, which are to be set on the component and thus are preset, can be calculated here as follows:
F=4·(U1−U2)·U0 (4).
K=4·U02+2U12+2U22 (5).
Thus, parameters α and β can be introduced, for which applies:
α=U1−U2 (6).
β=U1+U2 (7).
If one inserts formulas (6) and (7), respectively, into the formulas (4) and (5), respectively, then one obtains:
F=4·α·U0 (8).
K=4·U02+α2+β2 (9).
Thus, signal processing, which serves to detect movement of the active structure 20 or control the applied drive and resetting force, respectively, and of the spring constants, i.e. to control the second voltage U1 and the third voltage U2, is to solve the following equations:
This signal processing can be realized by a control unit 80, which is schematically illustrated in
The previously illustrated and described embodiments of the method for operating a component are characterized in that a direct voltage has been applied to the electrodes of the active structure 20. As already described in the prior art, however, an alternating voltage can also be applied to the active structure, whereby self-mixing drive and readout functions can be realized. “Self-mixing” means that in gyros, which operate at an operating frequency ω0 (resonance frequency), a resetting force can be obtained at the operating frequency ω0 by applying direct voltages to the drive electrodes, whereas a deflection at the operating frequency ω0 supplies direct voltage values to the readout electrodes, respectively to the charge amplifier, i.e. for detection.
With reference to
As illustrated in
In addition, the component 1 has a ninth electrode 42 and a tenth electrode 43, which both are each connected to the first substrate 11 and/or to the second substrate 15, and extend outwards from it in the second direction along the second axis, i.e. the Y axis, into the active area 21. The ninth electrode 42 is arranged so that the first electrode 221 is arranged between the first fifth electrode 411 and the ninth electrode 42, whereas the tenth electrode 43 is arranged so that the third electrode 231 is arranged between the second fifth electrode 412 and the tenth electrode 43.
The component 1 further comprises a first signal-processing unit and a second signal-processing unit 72. The first fifth electrode 411 and the ninth electrode 42 are connected to the first signal-processing unit 71, which determines a charge difference between these two electrodes, and provides a charge QR or a voltage corresponding thereto at a first outlet 73. The second fifth electrode 412 and the tenth electrode 43 are connected to the second signal-processing unit 72, which also determines a charge difference and provides a charge QI or rather a voltage corresponding thereto at a second outlet 74.
The component 1 further has a first sixth electrode 511 and a second sixth electrode 512, which are both arranged between the second electrode 222 and the fourth electrode 232 and otherwise extend as the sixth electrode 51 described with regard to the
According to the third embodiment of the method for operating the component, a third voltage UR is applied to the seventh electrode 52, while the negative third voltage −UR is applied to the first sixth electrode 511.
A fourth voltage UI is applied to the second sixth electrode 512, while the negative fourth voltage −UI is applied to the eighth electrode 53.
The third voltage UR and the fourth voltage UI are direct voltages, the polarity of which, however, can be periodically reversed at a low frequency.
Thus, the force acting on the active structure 20 can be calculated as follows:
F=U
R
·U
0·cos(ω0·t)+UI·U0·sin(ω0·t) (14).
The readout charges QR and QI are as follows:
Q
R
=ΔC·U
0·cos(ω0·t) (15).
Q
I
=ΔC·U
0·cos(ω0·t) (16).
The capacitance difference ΔC resulting from the difference of the partial capacitances C2−C1 is a measure for the deflection of the active structure 20.
Thus, both the normal and the quadrature components can be correctly processed both on the drive side and on the readout side.
To compensate for the drift of a charge amplifier at ω=0, the polarity of the first voltage U0·cos(ω0·t) and of the second voltage U0·sin(ω0·t) applied to the active structure 20 as well as of the third voltage UR and of the fourth voltage UI applied to the drive electrodes can be periodically reversed at a lower frequency. In this case, the readout charges QR and QI are demodulated in the same cycle.
In
As illustrated in
The first electrode 221 extends outwards from the first region 22 in the first direction along the second axis, i.e. the Y axis, while, however, the second electrode 222 extends outwards from it in the second direction along the second axis, wherein the second direction runs opposite the first direction. The third electrode 231 and the fourth electrode 232 are arranged in the second region 23, wherein the third electrode extends outwards from the second region 23 in the first direction along the second axis, and the fourth electrode extends outwards from the second region 23 in the second direction along the second axis. The fifth electrode 251 and the sixth electrode 252 are arranged in the third region 250, wherein the fifth electrode extends outwards from the third region 250 in the first direction along the second axis, and the sixth electrode extends outwards from the third region 250 in the second direction along the second axis. The seventh electrode 261 and the eighth electrode 262 are arranged in the fourth region 260, wherein the seventh electrode extends outwards from the fourth region 260 in the first direction along the second axis, and the eighth electrode extends outwards from the fourth region 260 in the second direction along the second axis.
According to the fourth embodiment, the component further comprises a ninth electrode 44 and a tenth electrode 45, which are firmly connected to the first substrate 11 and/or to the second substrate 15 and extend outwards from it in the second direction along the second axis into the active area 21, wherein the ninth electrode 44 is arranged between the first electrode 221 and the third electrode 231, and the tenth electrode 45 is arranged between the fifth electrode 251 and the seventh electrode 261. Furthermore, the component comprises an eleventh electrode 54 and a twelfth electrode 55, which are firmly connected to the first substrate 11 and/or to the second substrate 15 and extend outwards from it in the first direction along the second axis into the active area 21, wherein the eleventh electrode 54 is arranged between the second electrode 222 and the fourth electrode 232, and the twelfth electrode is arranged between the sixth electrode 252 and the eighth electrode 262.
The active structure and, thus, the first to eighth electrodes 221 to 262 can move along the first axis, i.e. the X axis, which is symbolized by the arrow.
In the fourth embodiment of the method for operating a component, a first voltage U0·cos(ω0·t) is applied to the first electrode 221 and to the second electrode 222, i.e. to the first region 22. The negative first voltage, i.e. −U0·cos(ω0·t), is applied to the third electrode 231 and to the fourth electrode 232, i.e. to the second region 23. Thus, the first electrode 221 and the ninth electrode 44 form a first partial capacitance C1, while the third electrode 231 and the ninth electrode 44 form a second partial capacitance C2. The partial capacitances C1 and C2 induce a charge QR onto the ninth electrode 44, which can be amplified with the aid of a simple charge amplifier 60a and read out as voltage at a first outlet 73.
A time-delayed second voltage U0·sin(ω0·t) is applied to the fifth electrode 251 and to the sixth electrode 252, i.e. to the third region 250. The negative second voltage, i.e. −U0·sin(ω0·t), is applied to the seventh electrode 261 and to the eighth electrode 262, i.e. to the fourth region 260. Thus, the fifth electrode 251 and the tenth electrode 45 form a third partial capacitance C3, while the seventh electrode 271 and the tenth electrode 45 form a fourth partial capacitance C4. The partial capacitances C3 and C4 induce a charge QI onto the tenth electrode 45, which can be amplified with the aid of another simple charge amplifier 60b and read out as voltage at a second outlet 74.
A third voltage UR can be applied via the eleventh electrode 54, while a fourth voltage UI is applied to the twelfth electrode 55. The third voltage UR and the fourth voltage UI are direct voltages, the polarity of which, however, can be periodically reversed at a low frequency.
Thus, the resetting force F acting on the active structure 20 can also be calculated according to formula (14). However, contrary to the third embodiment illustrated in
The illustrated embodiments of the component according to the invention and of the method according to the invention for operating such a component enable complete separation of the functions for drive and detection. Both non-mixing configurations with each an electrode for the drive and an electrode for the detection and self-mixing configurations with a plurality of electrodes for the drive and the detection can be realized. In addition, the negative spring constant of the springs 25 and 26, by which the active structure 20 is connected to the first substrate 11 and/or the second substrate 15, can be used for tuning the resonance frequency of the active structure 20. However, it is also possible to eliminate the effect of the negative spring constant.
When applying a direct voltage to the electrodes of the active structure 20, a linear tension force function can be realized for the drive, wherein harmful capacitances are ineffective in the detection of the deflection of the active structure 20, whereby a higher accuracy of the detection can be achieved. If multiple oscillators, i.e. active structures consisting of a plurality of structures movably supported relative to one another, are used, then the drive and detection functions can be fully separated from one another, so that no time multiplex is necessary. In addition, it is possible to use low bandwidths of the drive voltage for the drive and the charge amplifiers for the detection in gyros operating at an operating frequency ω0.
Number | Date | Country | Kind |
---|---|---|---|
10 2014 002 823.2 | Feb 2014 | DE | national |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2015/000303 | 2/11/2015 | WO | 00 |