Patent Description:
As known, MEMS mirror devices are used in portable apparatuses, such as for example smartphones, tablets, notebooks, PDAs, for optical applications, in particular to direct light radiation beams generated by a light source (for example laser) with desired modes. Thanks to their small size, these devices allow compliance with stringent requirements regarding space occupation, in terms of both area and thickness.

For example, MEMS mirror devices are used in miniaturized projector apparatuses (so-called picoprojectors), capable of projecting images from a distance and generating desired light patterns, in particular on a screen or on a similar display surface.

MEMS mirror devices generally include a tiltable structure carrying a reflecting or mirror surface of suitable material (e.g. aluminum, or gold, depending on whether the projection is in the visible or in the infrared). The tiltable structure is usually elastically supported above a cavity and is manufactured from a semiconductor body so as to be movable, for example with tilt or rotation movement, out of a main extension plane, to direct an impinging light beam in a desired manner.

The rotation of the tiltable structure is controlled through an actuation system which may be, for example, of electrostatic, electromagnetic or piezoelectric type.

MEMS mirror devices with piezoelectric actuation have the advantage of requiring reduced actuation voltages and power consumption with respect to devices with electrostatic or electromagnetic actuation. Furthermore, they allow providing piezoresistive sensor elements configured to detect the drive condition of the mirror and to provide a feedback signal to allow a feedback control of the same driving.

Typically, applications using MEMS mirror devices provide for a deflection of the light beam along two axes, which may be achieved by two uniaxial MEMS mirror devices, arranged downstream to each other (in the direction of light propagation) or by a single biaxial MEMS mirror device.

In the case of a biaxial device, the tiltable structure is configured to rotate around two axes; for example, it may rotate around a first axis with resonant movement, to generate a fast horizontal scan on the screen or display surface, and around a second axis with a linear or quasi-static movement (i.e. at a much lower frequency than the frequency of the resonant movement), to generate a slow vertical scan. In this manner, for example a line or raster scan may be obtained on the same screen or display surface.

Alternatively, the rotation around the second rotation axis may also occur at the resonance frequency, to generate a fast scan, in this case vertical, and overall a so-called "Lissajous" scan pattern on the screen or display surface.

Some examples of MEMS mirror devices of biaxial type and with piezoelectric actuation are described for example in <CIT> and <CIT>, in the name of the same Applicant.

Other MEMS mirror devices are disclosed, e.g., in <CIT>, <CIT>, <CIT> e <CIT>.

In all cases, the tiltable structure (micromirror) is supported by an elastic structure (formed by elastic elements also called "springs") which transfer the scanning movement generated by the actuation system to the tiltable structure and which, to this end, deform elastically.

Generally, the elastic structures and the actuation structures are formed in the same semiconductor layer which forms the tiltable structure, monolithically thereto. Therefore, they have a thickness equal to the tiltable structure.

However, this is not optimal and may limit the performances of the MEMS device. In fact, on the one hand it is desired that the tiltable structure be stiff, so as to have a high robustness against shocks in the thickness direction (and therefore it generally has a high thickness), and on the other hand it is desired that the elastic structures and the actuators have high actuation efficiency and effectively transfer the actuation movement to the tiltable structure, which strongly depends on their thickness.

Furthermore, even the optimal elastic characteristics of the actuation structure and the elastic parts are not the same: for the elastic structure it is desired that it have an optimized stiffness for the efficient transmission of the actuation, shock robustness and rejection of spurious modes activated by external excitation; for the actuation structure it is desired that it has a low stiffness to improve the actuation efficiency. The optimal characteristics indicated for the elastic structure and for the actuation structure depend, inter alia, on the thickness of the respective structures, but in a different and conflicting manner.

Currently, therefore, the (equal) thickness of the tiltable structure, the elastic structure and the actuation structure is chosen on the basis of a trade-off between the characteristics of stiffness and efficiency of the various structures.

A biaxial micro-electro-mechanical mirror device is described in <CIT> (<CIT>). In this device, the structures have three different thicknesses. The actuation structure and the elastic structures associated with a first rotation axis SA (forming a Slow, quasi static Axis) have a first thickness and are formed in a first semiconductor layer which is thin, so as to operate at low working voltages; the tiltable structure and the elastic structures associated with a second rotation axis FA (forming a Fast Axis, at resonance frequency) have a second thickness, greater than the first thickness, and are formed in a second semiconductor layer, thicker than the first semiconductor layer, so as to have a high resonance frequency. Coupling frames and external frames are formed using both the first and the second semiconductor layers and therefore have maximum thickness.

While providing considerable advantages over previous MEMS mirror devices, in some applications, however, this solution does not allow the desired actuation efficiency to be achieved.

In fact, forming the actuation and elastic structures associated with the first rotation axis SA of the same thickness does not allow obtaining a high actuation efficiency of the axis thereof (here, of the slow axis).

The aim of the present invention is to provide a solution which overcomes the drawbacks of the prior art.

According to the present invention, a MEMS device and the manufacturing process thereof are provided, as defined in the attached claims.

For a better understanding of the present invention, some embodiments thereof are now described, purely by way of non-limiting example, with reference to the attached drawings, wherein:.

The following description refers to the arrangement shown; consequently, expressions such as "above", "below", "top", "bottom", "right", "left" relate to the attached Figures and are not to be interpreted in a limiting manner, except where explicitly indicated.

<FIG> shows a micro-electro-mechanical mirror device <NUM>, of biaxial type, manufactured using MEMS technology, hereinafter also referred to as device <NUM>.

The device <NUM> is formed in a die <NUM>' of semiconductor material, in particular silicon, and comprises a fixed structure <NUM>, defined in the die <NUM>'. In particular, the fixed structure <NUM> forms an external rim or frame <NUM>' which delimits and surrounds a cavity <NUM>.

The fixed structure <NUM> is suspended above the cavity <NUM> and is elastically coupled to a tiltable structure <NUM>, having a top surface (for example of circular or elliptical shape) extending in a horizontal plane XY of a Cartesian coordinate system XYZ. The tiltable structure <NUM> is arranged here so as to rotate around a first rotation axis SA, parallel to a first horizontal axis X of the horizontal plane XY, and around a second rotation axis FA, parallel to a second horizontal axis Y of the same horizontal plane XY.

For example, the first rotation axis SA represents a Slow Axis, quasi static, while the second rotation axis FA represents a Fast Axis, at resonance frequency. The first and the second rotation axes SA, FA also represent a first and a second median symmetry axis for the device <NUM>.

The tiltable structure <NUM> carries at the top a reflecting surface <NUM>', defining a mirror surface and having main extension in the horizontal plane XY.

The fixed structure <NUM> forms a first and a second support (or anchor) element 5A, 5B, extending longitudinally along the first rotation axis SA, from the external frame <NUM>' inside the cavity <NUM>, towards the tiltable structure <NUM>, on opposite sides thereof.

The micro-electro-mechanical mirror device <NUM> further comprises an internal frame <NUM> extending over the cavity <NUM>.

In the illustrated embodiment and in top-plan view, the internal frame <NUM> has an elongated shape along the second horizontal axis Y; in particular, here, the internal frame <NUM> has a generically rectangular shape, with short sides arranged along the first horizontal axis X and long sides arranged along the second horizontal axis Y.

The internal frame <NUM> internally defines a window <NUM>; the tiltable structure <NUM> is arranged inside the window <NUM> and is elastically coupled to the internal frame <NUM> by a first and a second suspension elastic element 9A, 9B, compliant to torsion around the second rotation axis FA.

In the illustrated embodiment and in top view of <FIG>, the first and the second suspension elastic elements 9A, 9B have linear extension, extending along the second rotation axis FA, parallel to the second horizontal axis Y, on opposite sides with respect to the tiltable structure <NUM>, from the tiltable structure <NUM> to a respective short side of the internal frame <NUM>.

As discussed in detail below, the internal frame <NUM> is elastically coupled to the first and the second support elements 5A, 5B.

The device <NUM> further comprises an actuation structure <NUM>, coupled to the tiltable structure <NUM> and configured to cause the rotation thereof around the first rotation axis SA and around the second rotation axis FA, in a substantially decoupled manner.

The actuation structure <NUM> is in general arranged between the internal frame <NUM> and the external frame <NUM>' of the fixed structure <NUM> and also helps to support the same internal frame <NUM> on the cavity <NUM>.

The actuation structure <NUM> comprises a first pair of actuation arms that may be driven to cause the rotation of the tiltable structure <NUM> around the first rotation axis SA, in this case with a quasi-static movement.

The first pair of actuation arms is therefore here formed by a first and a second slow actuation arm 12A, 12B, arranged on opposite sides of the first rotation axis SA, symmetrically thereto, and therefore of the first support element 5A.

In the embodiment illustrated in <FIG>, the slow actuation arms 12A, 12B of the first pair have a generally rectangular shape, with greater extension along the first horizontal axis X.

In the device <NUM>, the first and the second slow actuation arms 12A, 12B are coupled integrally and directly, on an own first side, to the external frame <NUM>' of the fixed structure <NUM>; they are also coupled on an own second side, opposite to the first, to the internal frame <NUM>, in an elastic manner, by a first, respectively second transmission elastic element 14A, 14B.

Each slow actuation arm 12A, 12B is suspended above the cavity <NUM> and comprises, as explained in more detail below, a piezoelectric structure <NUM> (represented with a dashed line in <FIG>) and a bearing structure <NUM>.

In particular, and as shown in detail in <FIG>, each bearing structure <NUM> is coupled to the external frame <NUM>' and to the respective transmission elastic element 14A, 14B, and each piezoelectric structure <NUM> has an extension, in the horizontal plane XY, slightly smaller than the respective slow actuation arm 12A, 12B.

The first and the second transmission elastic elements 14A, 14B have a high stiffness with respect to movements out of the horizontal plane XY (along the vertical axis Z) and are compliant with respect to torsion around rotation axes parallel to the first rotation axis SA.

In the embodiment illustrated in <FIG>, the first and the second transmission elastic elements 14A, 14B are of linear type and extend parallel to the first horizontal axis X, between the first, respectively, the second slow actuation arm 12A, 12B and a same long side of the internal frame <NUM>, in proximity of the first rotation axis SA, at a reduced distance from the same first rotation axis SA.

As an alternative to what shown, the first and the second transmission elastic elements 14A, 14B may be of folded type, in a manner obvious to the person skilled in the art.

The actuation structure <NUM> also comprises a second pair of actuation arms, that may also be driven to cause the rotation of the tiltable structure <NUM> around the first rotation axis SA with a quasi-static movement.

The second pair of actuation arms is here formed by a third and a fourth slow actuation arm 12C, 12D, arranged on the opposite side with respect to the first rotation axis SA and the second support element 5B.

Similarly to the first and the second slow actuation arms 12A, 12B, the third and the fourth slow actuation arms 12C, 12D have, in top-plan view, longitudinal extension parallel to the first horizontal axis X and to the second support element 5B. In practice, the second pair of slow actuation arms 12C, 12D is arranged symmetrically to the first pair of slow actuation arms 12A, 12B with respect to the second rotation axis FA.

Furthermore, each slow actuation arm 12C, 12D of the second pair is integrally coupled, at an own side, to the external frame <NUM>' of the fixed structure <NUM> and is elastically coupled, at an opposite side, to the internal frame <NUM> through a respective third and fourth transmission elastic element 14C, 14D.

Similarly to the first and the second slow actuation arms 12A, 12B and as discussed in detail hereinafter, the third and the fourth slow actuation arms 12C, 12D each comprises an own piezoelectric structure <NUM> (represented by a dashed line in <FIG>) and an own bearing structure <NUM>.

Furthermore, also the third and the fourth transmission elastic elements 14C, 14D are, in the embodiment shown, of linear type, but may be formed as folded springs.

As also discussed hereinafter, each slow actuation arm 12A-12D of the first and the second pairs has a different elastic behavior with respect to the respective transmission elastic element 14A-14D, in particular it is of different material, so as to optimize the elastic characteristics of both the actuation arms 12A-12D and the respective transmission elastic elements 14A-14D according to the respective function.

The actuation structure <NUM> further comprises a third pair of actuation arms, here formed by a first and a second fast actuation arm 17A, 17B, that can be driven to cause the rotation of the tiltable structure <NUM> around the second rotation axis FA, with resonant movement.

The first and the second fast actuation arms 17A, 17B are interposed between the first, respectively, the second support element 5A, 5B and the internal frame <NUM>.

In particular, the first and the second fast actuation arms 17A, 17B are elastically coupled to the internal frame <NUM> by a first, respectively a second torsional elastic element 16A, 16B, having a high stiffness with respect to movements out of the horizontal plane XY (along the orthogonal axis Z) and compliant to torsion around the first rotation axis SA.

In the illustrated embodiment, and in top-plan view, the first and the second fast actuation arms 17A, 17B have a generically rectangular shape, with greater extension along the first horizontal axis X.

In particular, the first and the second fast actuation arms 17A, 17B have a respective first end integrally coupled to the first, respectively the second support element 5A, 5B (whereof they are an extension) and a respective second end elastically coupled to the internal frame <NUM> through by the first, respectively, the second torsional elastic element 16A, 16B.

Furthermore, the first and the second torsional elastic elements 16A, 16B extend along the first rotation axis SA, between the second end of the first and, respectively, the second fast actuation arm 17A, 17B and a respective long side of the internal frame <NUM> they are coupled to, at a respective central portion.

In the illustrated embodiment, the first and the second torsional elastic elements 16A, 16B are of linear type; however, they may be of folded type.

Similarly to what discussed for the first and the second pairs of actuation arms, each fast actuation arm 17A, 17B comprises a bearing structure <NUM> (here of silicon) and a respective piezoelectric structure <NUM>.

In a manner not illustrated, the device <NUM> further comprises a plurality of pads, carried by the fixed structure <NUM> at the external frame <NUM>', electrically connected to the piezoelectric structures <NUM> of the slow actuation arms 12A-12D, and of the fast actuation arms 17A, 17B by electrical connection lines, to allow the electrical biasing thereof by electrical signals coming from the outside of the same electromechanical device <NUM> (for example from a biasing device of an electronic apparatus having the device <NUM> integrated therein).

As shown in <FIG>, a support wafer (or cap) <NUM> is also coupled below the fixed structure <NUM>, through a suitable bonding region <NUM>, and has a recess <NUM>, below the cavity <NUM> and at the tiltable structure <NUM>, to allow the rotation of the tiltable structure <NUM>.

As shown in the sections of <FIG>, in the device <NUM>, the bearing structure <NUM> of the slow actuation arms 12A-12D is not formed in the same silicon layer as the bearing structures <NUM> of the fast actuation arms 17A, 17B and of the transmission elastic elements 14A-14D, but in a distinct layer, of more resilient material (having a lower Young's modulus), in particular a polymeric material such as dry film photoresist.

In particular, with reference to <FIG>, the die <NUM>' comprises a first semiconductor layer, here silicon, generally indicated by <NUM> and forming the bottom part of the internal frame <NUM>, of the fixed structure <NUM> and of the support elements 5A, 5B, as well as the tiltable structure <NUM> and the suspension elastic elements 9A, 9B (see also <FIG>); and a second semiconductor layer, here also silicon, generally indicated by <NUM> and forming the top part of the internal frame <NUM>, of the support elements 5A, 5B and of the fixed structure <NUM>, as well as the torsional elastic elements 16A, 16B and the bearing structures <NUM> of the fast actuation arms 17A, 17B.

The semiconductor layers <NUM>, <NUM> are completely removed at the slow actuation arms 12A-12D and therefore each piezoelectric structure <NUM> is suspended below the respective bearing structure <NUM>, as visible in the schematic representations of <FIG>, <FIG>, <FIG> and <FIG>, as described in detailed below.

In particular, <FIG> shows a cross-section of the device <NUM> taken through the third transmission elastic element 14C (but the same section is applicable for the other transmission elastic elements 14A, 14B and 14D and therefore <FIG> and the following description refer to a generic transmission elastic element <NUM>). As noted, the transmission elastic element <NUM> extends between the internal frame <NUM> and the bearing structure <NUM> of the respective actuation arm (here generically indicated by <NUM>) and is formed by the second semiconductor layer <NUM> (i.e. the underlying first semiconductor layer <NUM> is removed). The transmission elastic elements <NUM> therefore have elasticity and robustness characteristics linked to the semiconductor material used (here silicon) and to the thickness of the second semiconductor layer <NUM>.

<FIG> shows a cross-section of the device <NUM> taken through the second torsional elastic element 16B (but the same section is applicable to the first torsional elastic element 16A and therefore <FIG> and the following description refer to a generic torsional elastic element <NUM>). As noted, the torsional elastic element <NUM> extends between the internal frame <NUM> and the respective fast actuation arm (here generically indicated by <NUM>) and is formed by the sole second semiconductor layer <NUM>. The torsional elastic elements <NUM> therefore have elasticity and robustness characteristics linked to the used semiconductor material (here silicon) and to the thickness of the second semiconductor layer <NUM>, similarly to the transmission elastic elements <NUM>. The bearing structures <NUM> of the fast actuation arms <NUM> are also formed by the second semiconductor layer <NUM> and here have a thickness equal to the respective transmission elastic elements <NUM>.

<FIG> shows a cross-section of the device <NUM> taken through the third slow actuation arm 12C (but the same section is applicable for the other slow actuation arms 12A, 12B and 12D and therefore <FIG> and the following description refer to a generic slow actuation arm <NUM>). As noted, the slow actuation arm <NUM>, coupled between the respective transmission elastic element <NUM> (not visible in <FIG>) and the external frame <NUM>', is formed by the bearing structure <NUM> and by the piezoelectric structure <NUM>. Since the slow actuation arms <NUM> are of material different from the semiconductor material of the transmission elastic elements <NUM> and of the torsional elastic elements <NUM>, they may be designed in a dedicated manner; in particular, the use of a polymeric material allows an optimal stiffness value to be set, on the basis of the characteristics of the material and by a suitable choice of its thickness.

In a possible embodiment of the device <NUM>, the thickness of the first semiconductor layer <NUM> may be comprised between <NUM> and <NUM>, for example <NUM>; the thickness of the second semiconductor layer <NUM> may be comprised between <NUM> and <NUM>, for example <NUM>; and the thickness of the bearing structure <NUM> may be comprised between <NUM> and <NUM>, for example <NUM>.

<FIG> shows a possible implementation of the piezoelectric structure <NUM>, not to scale (in general, the layers of the piezoelectric structure <NUM> are much thinner than the bearing structure <NUM> and have a small impact on the stiffness thereof; in any case, the overall stiffness of the slow actuation arms <NUM> may be designed considering the entire structure, in a manner obvious to the person skilled in the art).

The piezoelectric structure <NUM> may be provided in a known manner and comprise in particular PZT - Lead Zirconate Titanate.

In detail, with reference to <FIG>, the piezoelectric structure <NUM> here comprises:.

The third dielectric region <NUM> is surrounded by a soft region <NUM>, of polymeric material, which forms the bearing structure <NUM>.

First and second contacts 57A, 57B are formed through the second or the third dielectric regions <NUM>, <NUM> and are connected to conductive lines (a track <NUM> shown partially) and to metal regions, not shown, in a first metallization level of the device for the electrical connection of the electrode regions <NUM>, <NUM>, as discussed above.

As noted, the end sides of the soft region <NUM> visible in <FIG> are superimposed on the transmission elastic element <NUM> and on the frame <NUM>'.

<FIG> also shows oxide regions <NUM> interposed between the first and the second semiconductor layers <NUM>, <NUM>, for the reasons explained below.

As described in detail in aforementioned <CIT>, during the operation of the device <NUM>, the application of a biasing voltage to the piezoelectric structure <NUM> of the first/third slow actuation arm 12A/12C, having a positive value with respect to the bias of the piezoelectric structure <NUM> of the second/fourth slow actuation arm 12B/12D, causes a rotation of the internal frame <NUM> and of the tiltable structure <NUM>, coupled thereto, in a first direction around the first rotation axis SA (with consequent torsional deformation of the torsional elastic elements 16A, 16B).

Correspondingly, the application of a biasing voltage to the piezoelectric structure <NUM> of the second/fourth slow actuation arm 12B/12D, having a positive value with respect to the bias of the piezoelectric structure <NUM> of the first/third slow actuation arm 12A/12C, causes a corresponding rotation of the internal frame <NUM> and of the tiltable structure <NUM> in a second direction, opposite to the first, around the same first rotation axis SA.

During the rotation around the first rotation axis SA, the tiltable structure <NUM> is integrally coupled to the internal frame <NUM> (due to the stiffness of the suspension elastic elements 9A, 9B with respect to this movement), so rotate therewith and cause the desired movement of the reflecting surface <NUM>' with respect to the first rotation axis SA. In other words, the suspension elastic elements 9A, 9B do not undergo deformations due to the rotation of the internal frame <NUM> around the first rotation axis SA.

In this step, the bearing structures <NUM> of the slow actuation arms 12A, 12B, and 12C, 12D may easily deform and require a low deformation force, due to the lower stiffness, compared to the respective transmission elastic elements <NUM>. They are therefore capable of generating the desired rotational movement with high efficiency.

Conversely, the transmission elastic elements <NUM> have a high stiffness with respect to movements out of the horizontal plane XY (along the orthogonal axis z). They therefore transfer this rotation movement with high efficiency.

As described in aforementioned <CIT>, the rotation of the tiltable structure <NUM> around the second rotation axis FA occurs by applying a biasing voltage to the piezoelectric structure <NUM> of at least one of the first and the second fast actuation arms 17A, 17B (with phase-opposition bias when both arms are actuated). This rotation generally occurs at the resonance frequency of the tiltable structure <NUM>.

In this case, in fact, the force along the vertical axis Z generated by biasing the piezoelectric structures <NUM> of the first/second fast actuation arm 17A, 17B is transmitted to the internal frame <NUM>, with torsional deformation of the suspension elastic elements 9A, 9B.

During this rotation, the transmission elastic elements <NUM>, compliant with respect to torsion around rotation axes parallel to the first rotation axis SA, only minimally transfer their deformation to the slow actuation arms <NUM> which are therefore practically not affected by the rotation of the tiltable structure <NUM> around the second rotation axis FA.

The device <NUM> may be manufactured as described hereinbelow, with reference to <FIG>, taken along section plane VII-VII of <FIG>.

With reference to <FIG>, a semiconductor wafer <NUM> comprises a substrate <NUM> of semiconductor material, here of monocrystalline silicon, intended to form the first semiconductor layer <NUM> of <FIG>.

A barrier layer <NUM>, for example of silicon oxide, is formed, for example deposited, on the substrate <NUM>.

Then, <FIG>, the barrier layer <NUM> is patterned, using standard photolithography steps, to form barrier regions 102A, forming, inter alia, the oxide regions <NUM> of <FIG>.

In <FIG>, a bearing layer <NUM> of semiconductor material, here silicon, intended to form the second semiconductor layer <NUM>, is epitaxially grown and planarized. A first dielectric layer <NUM>, a first electrode layer <NUM>, a piezoelectric layer <NUM> and a second electrode layer <NUM>, are formed, in sequence, on the bearing layer <NUM>.

In <FIG>, the layers <NUM>-<NUM> are patterned, using standard photolithography steps; in particular, here, the second electrode layer <NUM> and the piezoelectric layer <NUM> are first etched, in an aligned manner; then the first electrode layer <NUM> and subsequently the first dielectric layer <NUM> are etched, thus forming, respectively, the top electrode region <NUM>, the piezoelectric region <NUM>, the bottom electrode region <NUM> and the first dielectric region <NUM> of <FIG>, completing the piezoelectric stack <NUM>.

In <FIG>, a second dielectric layer is deposited and patterned, so as to form the second dielectric region <NUM>; the second dielectric region <NUM> has openings <NUM> which reach the top electrode region <NUM> and the bottom electrode region <NUM>.

Then metal connection material (for example aluminum) is deposited and patterned, forming the first contacts 57A and the conductive tracks <NUM> coupled thereto.

In <FIG>, a third dielectric layer is deposited and patterned, so as to form the third dielectric region <NUM> and openings <NUM> which reach the conductive tracks <NUM>. Subsequently, the second contacts 57B (one visible) are formed, in a similar manner to the first contacts 57A. The piezoelectric structure <NUM> is thus formed.

In <FIG>, a reflecting layer (e.g. of aluminum or gold, depending on whether the projection is in the visible or in the infrared) is deposited and patterned to form the reflecting surface <NUM>'.

Then, <FIG>, a polymeric layer is deposited and patterned, forming the soft region <NUM>.

Subsequently, <FIG>, the wafer <NUM> is flipped over and thinned, so as to reduce the thickness of the substrate <NUM> to the desired value for the first layer <NUM>, for example variable between <NUM> and <NUM>. Thinning may be performed according to any suitable technique, for example by grinding and polishing.

In <FIG>, the wafer <NUM> is etched from the back in a masked manner, for example by a dry etching, such as DRIE - Deep Reactive Ion Etching, so as to remove both the substrate <NUM> and the bearing layer <NUM>, where the barrier regions 102A are not present, stopping on the first dielectric region <NUM> at the slow actuation arms 12A-12D (being defined), and so as to remove only the substrate <NUM>, where are the barrier regions 102A.

In this manner, the fixed structure <NUM>', the internal frame <NUM>, the tiltable structure <NUM> and the support elements 5A, 5B (the latter, not visible in <FIG>), formed by both the semiconductor layers <NUM> and <NUM>, are defined. Furthermore, the transmission elastic elements 14A-14D, the torsional elastic elements 16A, 16B and the bearing structures <NUM> of the fast actuation arms 17A, 17B (not visible in <FIG>), formed by the sole second semiconductor layer <NUM>, are defined. In this step, the slow actuation arms 12A-12D are also freed. Precisely, under the slow actuation arms 12A-12D, both the first and the second semiconductor layers <NUM>, <NUM> are removed.

In this manner, the cavity <NUM> is also formed.

Then, <FIG>, the barrier regions 102A are removed where exposed, by an oxide removal etching. In particular, the barrier regions 102A are removed below the slow actuation arms 12A-12D. The remaining portions of the barrier regions 102A thus form the oxide regions <NUM>.

Furthermore, a cap wafer <NUM>, previously processed to form the recess <NUM>, is attached to the first wafer <NUM>, forming a composite wafer <NUM>.

To this end, the bonding region <NUM>, for example of oxide, may be arranged between the fixed structure <NUM> and the portion of the cap wafer <NUM> surrounding the recess <NUM>.

After dicing the composite wafer <NUM>, in a known manner, the device <NUM> of <FIG> is obtained.

<FIG> shows a device <NUM> wherein the soft region <NUM> is arranged at the bottom of the piezoelectric stack <NUM>.

In this case, the manufacturing process differs from what has been shown in <FIG> and described above in that the soft region <NUM> is deposited directly above the second semiconductor layer <NUM>, after growing the latter (after the step of <FIG>) and defined before forming the stack of layers <NUM>-<NUM> of <FIG>.

The device <NUM>, <NUM> may be modified so as to include an additional layer to modulate the stiffness of the slow actuation arms 12A-12D.

For example, <FIG> shows a device <NUM> having an additional layer <NUM> above the soft region <NUM>.

The additional layer <NUM> is typically a layer having a stiffness (Young's modulus) greater than the polymeric material of the soft region <NUM>, for example <NUM> times greater, with a thickness comprised between <NUM> and <NUM>.

For example, the additional layer <NUM> is a material chosen from silicon oxide, silicon nitride, metal or the like and has a stiffness comparable to that of the polymeric material or intermediate between the polymeric material of the soft region <NUM> and the silicon of the transmission elastic elements 14A-14D.

In this manner, the total stiffness of the slow actuation arms 12A-12D may be chosen on the basis of the best trade-off between stiffness and robustness, also here independently of the stiffness and robustness of the respective transmission elastic elements 14A-14D.

As indicated above, the mirror device described here allows the elastic characteristics of the actuation arms to be optimized so as to improve the efficiency in driving the movement of the tiltable structure <NUM>. In this manner, with the same dimensions, geometry and other design considerations, the present device affords a greater rotation angle of the tiltable structure <NUM> (and therefore of the reflecting structure <NUM>'), with a gain, in some cases, of <NUM>%.

Alternatively, for a same rotation angle, the slow actuation arms 12A-12D may be shorter, with a reduction of the total dimensions of the device <NUM> and in some cases allowing an area reduction in the die <NUM>' of about <NUM>%.

The Applicant has also assessed the robustness obtainable with the present device.

In particular, taking into account that the robustness Rshock depends on the frequency of the first spurious mode fspur: <MAT> it has been verified that the present device provides a robustness improvement of <NUM>% with respect to equal devices, having slow actuation arms 12A-12D of silicon, even if optimized.

Finally, it is clear that modifications and variations may be made to the mirror device and the manufacturing process thereof, described and illustrated herein, without thereby departing from the scope of the present invention, as defined in the attached claims. For example, the different embodiments described may be combined to provide further solutions.

Furthermore, the sequence of manufacturing steps is only indicative, and some steps may be carried out before or after others, differently from what has been described. For example, the reflecting surface <NUM>' may be formed before or after forming the piezoelectric stack <NUM> and/or the soft region <NUM>, or even after bonding the wafers <NUM>, <NUM>. Similarly, the piezoelectric stack <NUM> and the soft region <NUM> might be formed after bonding the wafers <NUM>, <NUM>.

Although the Figures refer to biaxial mirror devices, the invention may be applied to monoaxial micromirrors.

Claim 1:
A micro-electro-mechanical mirror device (<NUM>), comprising:
a fixed structure (<NUM>) defining an external frame (<NUM>') delimiting a cavity (<NUM>);
a tiltable structure (<NUM>) extending into the cavity;
a reflecting surface (<NUM>') carried by the tiltable structure and having a main extension in a horizontal plane (XY);
an actuation structure (<NUM>), coupled between the tiltable structure (<NUM>) and the fixed structure (<NUM>),
wherein the actuation structure (<NUM>) comprises at least one first pair of actuation arms (12A, 12B) configured to cause the rotation of the tiltable structure (<NUM>) around a first rotation axis (SA) parallel to the horizontal plane (XY), the actuation arms of the first pair of actuation arms (12A, 12B) being elastically coupled to the tiltable structure (<NUM>) through respective coupling elastic elements (14A, 14B) and each comprising a bearing structure (<NUM>) and a piezoelectric structure (<NUM>),
characterized in that the bearing structure (<NUM>) of each actuation arm of the first pair of actuation arms (12A, 12B) comprises a soft region (<NUM>) of a first material and the coupling elastic elements (14A, 14B) comprise a bearing layer (<NUM>) of a second material, the second material having greater stiffness than the first material.