Patent Application
20230382715
This application claims priority to French Patent Application No. 2205088, filed May 27, 2022, the entire content of which is incorporated herein by reference in its entirety.
The technical field of the invention is that of microelectromechanical systems (MEMS) or nanoelectromechanical systems (NEMS) devices. The invention more particularly relates to an electroacoustic transducer comprising a movable element and a back volume, the back volume being delimited in part by the movable element and subjected to a reference pressure. Such an electroacoustic transducer can be employed as a microphone or loudspeaker.
Microelectromechanical or nanoelectromechanical microphones represent a rapidly growing market, especially by virtue of the development of nomadic apparatuses, such as tablets, smartphones and other connected objects, in which they are gradually replacing electret microphones.
Microphones measure a rapid change in atmospheric pressure, also known as acoustic pressure. They therefore include at least one part in contact with the outside.
Most MEMS or NEMS microphones manufactured today are capacitive detection microphones. Patent applications FR3059659A1 and EP3975584A1 describe an example of a capacitive detection microphone comprising a movable element, capacitive detection means and a device for transmitting movement between the movable element and the capacitive detection means.
The movable element is capable of collecting the pressure variation. It may be formed by a rigid piston comprising a membrane and a membrane rigidifying structure. The membrane forms a separation between a cavity open to the external environment and a back volume of the microphone, also called the reference volume because a reference pressure prevails therein. Thus, a face of the membrane is subjected to the reference pressure and an opposite face to the membrane is subjected to the atmospheric pressure (whose variation is desired to be detected). The back volume is usually connected to the external environment by a narrow acoustic path. The reference pressure is then equal to the atmospheric pressure filtered out of its dynamic (high frequency) components which do not have time to equilibrate. The pressure difference between both faces of the membrane hence corresponds only to these high frequency variations (the sound), the atmospheric pressure and its slow variations being cancelled out.
This capacitive detection microphone, like other electroacoustic transducers with a membrane and a back volume, suffers from acoustic noise. This acoustic noise adds to the useful signal at the output of the microphone and deteriorates its performance.
Document US2017/325012A1 describes another electroacoustic transducer comprising a frame, an element movable relative to the frame and an internal cavity delimited by the movable element and walls belonging to the frame. The frame comprises a substrate and a lid. An internal surface of the lid is made of a thermally insulating material, in order to reduce the frequency of gas pressure fluctuations within the internal cavity, and thus reduce noise.
There is therefore a need to provide an electroacoustic transducer in which acoustic noise is reduced.
According to a first aspect of the invention, this need tends to be satisfied by providing an electroacoustic transducer comprising:
The first wall comprises at least one sealed cavity separated from the back volume by the first portion of the first structural layer, and a pressure lower than the reference pressure prevails in the at least one sealed cavity of the first wall.
The sealed cavity reduces heat exchange between the back volume and its boundaries, thereby reducing the associated acoustic noise (at a constant back volume). This alternatively allows to reduce the back volume, and hence the overall size of the microphone, for the same performance.
In an embodiment, the membrane is formed by a second portion of the first structural layer.
In an embodiment, the second wall comprises at least one sealed cavity, a pressure lower than the reference pressure prevails in the at least one sealed cavity of the second wall and the at least one sealed cavity of the second wall is located in the cap and separated from the back volume by a third structural layer with a thickness of less than 2 μm.
Further to the characteristics just discussed in the preceding paragraphs, the electroacoustic transducer according to the invention may have one or more complementary characteristics among the following, considered individually or according to any technically possible combinations:
A second aspect of the invention relates to a method for manufacturing an electroacoustic transducer comprising:
The substrate may be etched so as to delimit a transmission arm, the movable element being coupled to an end of the transmission arm, the first sacrificial layer serving as a stop layer in etching the substrate.
In an embodiment, the method further comprises, after the step of providing the stack and before the step of transferring the cap, the following steps of:
Beneficially, the first structural layer and the second structural layer are etched simultaneously so as to delimit the membrane and the rigidifying structure of the movable element.
In an embodiment of the method, the step of providing the stack comprises the following sub-steps of:
The manufacturing method may further comprise a step of providing the cap comprising the following sub-steps of:
The invention and its different applications will be better understood upon reading the following description and upon examining the accompanying figures.
Further characteristics and benefits of the invention will become clearer from the description thereof given below, by way of indicating and in no way limiting purposes, with reference to the appended figures, of which:
For more clarity, identical or similar elements are marked with identical reference signs throughout the figures.
In common to these three embodiments, the electroacoustic transducer 1 comprises a frame 10, an element 11 movable relative to the frame 10 and a first so-called internal cavity 12 where a reference pressure prevails.
The movable element 11, hereinafter referred to as piston, comprises a membrane 111 and a rigidifying structure 112 for rigidifying the membrane 111.
The membrane 111 of the piston 11, also referred to as a thin layer, is able to move or deform under the effect of a pressure difference between its two faces. It separates the first cavity 12 from a second cavity 13. In the case of an electroacoustic transducer of the microphone or loudspeaker type, the second cavity 13 is open to the external environment, that is the air. One face of the membrane 111 is therefore subjected to the reference pressure and an opposite face of the membrane 111 is subjected to atmospheric pressure.
The first cavity 12 is commonly referred to as the back volume (referring to its position behind the piston). This back volume 12 may be connected to the second cavity 13 through an acoustic path, for example located at the periphery of the piston 11 as represented in
Alternatively, the back volume 12 can be sealed. The reference pressure is then decorrelated from the atmospheric pressure.
When the membrane 111 moves as a result of the pressure differential, the back volume 12 is compressed or stretched, its pressure changes. In other words, part of the pressure change is transmitted to the back volume 12 via the membrane 111. The pressure changes cause temperature changes within the back volume 12, which in turn cause heat dissipation at the boundaries of the back volume 12. It is this thermal dissipation that causes the acoustic noise experienced by the electroacoustic transducer.
The larger the back volume 12, the less sensitive the electroacoustic transducer 1 is to temperature variations in the back volume 12. A good compromise between sensitivity to temperature variations and overall size of the electroacoustic transducer 1 can be obtained for a back volume 12 of between 1 mm3 and 100 mm3.
The back volume 12 is delimited by the mobile element 11 and by walls belonging to the frame 10. The back volume 12 is especially delimited by a first wall 101 located as an extension of the membrane 111 and by a second wall 102 arranged facing the membrane 111. In other words, the first wall 101 and the membrane 111 are located on a same side of the back volume 12 and the second wall 102 is located on the opposite side.
In order to reduce acoustic noise generated by heat dissipation during temperature variations in the back volume 12, at least one of the walls delimiting the back volume 12 comprises at least one sealed cavity 103a, 103b. Each sealed cavity 103a, 103b is filled with a gas or a gas mixture, for example air, which exerts a (strictly) lower pressure on the walls of the sealed cavity 103a, 103b than the reference pressure. In other words, a pressure (strictly) lower than the reference pressure prevails in the sealed cavity 103a, 103b.
Each sealed cavity 103a or 103b within a wall of the back volume 12 reduces heat dissipation through that wall. In other words, the sealed cavity 103a, 103b improves thermal insulation of the wall. This results in a decrease in acoustic noise at the output of the electroacoustic transducer.
The lower the pressure in the sealed cavity 103a, 103b, the lower the heat dissipation. The pressure in the sealed cavity 103a, 103b is beneficially less than 1000 Pa (10 mBar).
The pressure prevailing in the sealed cavity 103a, 103b may be very low, in order to achieve a near-vacuum configuration. It is then less than or equal to 100 Pa (1 mbar).
In an embodiment, the sealed cavity 103a, 103b extends parallel to at least one of the surfaces of the back volume 12.
A wall delimiting the back volume 12 may comprise a single sealed cavity 103a, 103b within which pillars 104a, 104b (also referred to as columns) are arranged. These pillars 104a, 104b improve mechanical strength of the wall. They have a width l which is beneficially between 500 nm and 50 μm. The width l, also called critical dimension, is the smallest dimension of the pillars 104a, 104b in a plane parallel to the faces of the membrane 111. Such a width offers a good compromise between mechanical strength of the wall (at the reference pressure) and thermal conduction.
Alternatively, the wall may comprise several sealed cavities 103a, 103b separated from each other by partition walls whose width 1 is beneficially between 500 nm and 50 μm. The different sealed cavities 103a or 103b within the same wall may have identical shape and dimensions.
The number of pillars 104a, 104b (or partition walls) per unit area depends on the compromise between mechanical strength of the wall and thermal conductivity.
In order to significantly reduce heat dissipation, the sealed cavity or cavities 103a, 103b extend into at least one of the first and second walls 101-102. These walls, referred to as the main walls, are those with the largest surface areas.
Thus, in the embodiment represented in
In these three embodiments, the frame 10 comprises a support 21, a first portion 23a of a first structural layer 23 disposed on the support 21 and a cap 30 disposed on the first portion 23a of the first structural layer 23. In an embodiment, the support 21 is formed by a first substrate (for example made of silicon) and the cap 30 comprises a second substrate 31 (for example made of silicon).
The frame 10 may further comprise a second structural layer 25 disposed between the first portion 23a of the first structural layer 23 and the cap 30.
The sealed cavity 103a of the first wall 101 is, in the embodiments of
Beneficially, the first structural layer 23 has a thickness of 2 μm or less. Thus, the first wall 101 has a low thermal inertia. The membrane 111 of the piston 11 is in an embodiment formed by a second portion 23b of the first structural layer 23.
In the embodiments of
The electroacoustic transducer 1 may be a capacitive detection microphone. In addition to the piston 11, the electroacoustic transducer 1 then comprises capacitive detection means and a device for transmitting movement between the movable element and the capacitive detection means.
The piston 11 is connected to the movement transmitting device in a first zone of the microphone, herein the second cavity 13.
The capacitive detection means make it possible to measure the displacement of the piston 11 and thus the variation in atmospheric pressure. They are disposed in a second zone of the microphone, sealingly isolated from the first zone 13 and not represented in the figures. They comprise a movable electrode and at least one fixed electrode arranged facing the movable electrode. The electrodes form the plates of a capacitor whose capacitance varies according to the displacement of the piston 11. The second zone is in an embodiment a controlled atmosphere chamber in order to reduce the phenomena of viscous friction and the associated acoustic noise. By “controlled atmosphere chamber”, it is meant a chamber under reduced pressure, typically less than 1000 Pa (10 mbar), and in an embodiment under vacuum (<100 Pa or 1 mbar).
The transmission device comprises at least one first transmission arm 14 extending into the first zone 13 and at least one second transmission arm extending into the second zone. The piston 11 is coupled to a first end of the first transmission arm 14, while the movable electrode of the capacitive detection means is coupled to an end of the second transmission arm. The first and second transmission arms are connected at their second end through a pivot hinge. This pivot hinge allows rotation of the transmission arms relative to the microphone frame 10 and simultaneously ensure sealing of the first and second zones.
The steps S1 to S5, illustrated in
Thus, with reference to
The substrate 21 serves especially to produce the first transmission arm 14 and a part of the frame (the support). It initially has a thickness which may be between 500 μm and 700 μm. The substrate 21 is in an embodiment a so-called “bulk” semiconductor substrate, for example made of silicon.
Then, in step S2 of
Beneficially, the first sacrificial layer 22 is deposited so as to completely fill the first and second cavities 210a-210b of the substrate 21. For example, the first sacrificial layer 22 is formed by plasma enhanced chemical vapour deposition (or PECVD) and then annealing. This deposition operation is followed by a planarisation operation, for example by chemical mechanical polishing (CMP), in order to obtain a planar surface with the reference surface R of the substrate 21.
The first sacrificial layer 22 is intended to disappear in part upon making the transducer. This layer is especially useful for delimiting the first transmission arm 14. It can also serve as a lower air gap in the capacitive detection zone of the transducer (not represented in the figures). It may also serve to mechanically connect the substrate 21 and the first structural layer 23. The first sacrificial layer 22 may be made of a dielectric material, for example a silicon nitride or a silicon oxide, for example silicon dioxide (SiO2). Its thickness is for example between 100 nm and 10 μm.
Step S3 of
The first portion 22a of the first sacrificial layer 22 is in an embodiment etched selectively with respect to the substrate 21. The pillars 104a or partition walls are then formed solely from the material of the first sacrificial layer 22.
The pillars 104a or partition walls may have different shapes. For example, the pillars 104a are cylinders with a round, square or octagonal cross-section. The partition walls are, for example, lines parallel to each other. The partition walls may also form a grid (lines extending in two intersecting, in an embodiment perpendicular, directions), each mesh of the grid hence corresponding to a cavity 103a.
The method for manufacturing then comprises a step of transferring the first structural layer 23 onto the first portion 22a of the first sacrificial layer 22 (pillars 104a or partition walls) and onto the second portion 22b of the first sacrificial layer 22, so as to close the cavity(ies) 103a in a tight manner (
Thus, in step S4 of
And then, in step S5 of
The transfer substrate 40 is in an embodiment a multilayer SOI type structure successively comprising a support layer 41 (typically silicon), a buried oxide layer 42 (typically SiO2) and a thin film of silicon forming the first structural layer 23. The transfer substrate 40 is thinned by successively removing the support layer 41 and the buried oxide layer 42.
The first structural layer 23 especially serves to produce the membrane 111 of the piston 11. It may also serve to produce the movable electrode of the capacitive detection means. It has a thickness less than that of the substrate 21, in an embodiment between 100 nm and 10 μm, and in an embodiment less than or equal to 2 μm.
The method for manufacturing continues with steps S6 to S12 described below in connection with
In step S6 of
The second sacrificial layer 24 may be first deposited to fully cover the first structural layer 23 and then partially etched, for example through a resin mask formed by photolithographically, to form the first and second portions 24a-24b. The etching of the second sacrificial layer 24 is in an embodiment selective with respect to the first structural layer 23. The second sacrificial layer 24 is beneficially formed from the same dielectric material as the first sacrificial layer 22, for example a silicon oxide. Its thickness may be between 100 nm and 10 μm.
The second sacrificial layer 24 may serve as an upper air gap for capacitive detection.
In step S7 of
Before step S7 of forming the second structural layer 25, the method for manufacturing may comprise a so-called step of opening the first structural layer 23 and the second portion 22b of the first sacrificial layer 22. This opening step consists of forming a well 26 that extends through the first structural layer 23 and the second portion 22b of the first sacrificial layer 22 to the substrate 21. This well 26 is formed by successively etching the first structural layer 23 and the second portion 22b of the first sacrificial layer 22, in an embodiment through the second portion 24b of the second sacrificial layer 24. The well 26 allows the material of the second structural layer 25 (for example silicon) to grow from the substrate 21 to the first structural layer 23, forming a pillar that passes through the second portion 22b of the first sacrificial layer 22. This pillar will provide connection between the membrane 111 of the piston 11 (formed in the first structural layer 23) and the first transmission arm 14 (formed in the substrate 21).
And then, in a step S8 represented by
In contrast, between the first and second portions 24a-24b of the second sacrificial layer 24, etching of the second structural layer 25 to delimit the periphery (or external contour) of the rigidifying structure 112 opens onto the first structural layer 23. Since etching of the second structural layer 25 is not selective with respect to the first structural layer 23 (but only with respect to the first and second sacrificial layers 22, 24), the first structural layer 23 is etched together with the second structural layer 25 down to the second portion 22b of the first sacrificial layer 22.
Thus, at the bottom of the trench corresponding to the periphery of the rigidifying structure 112, the first structural layer 23 has been etched and the second portion 22b of the first sacrificial layer 22 is exposed.
At the end of step S8, the first structural layer 23 comprises a first portion 23a and a second portion 23b separated from each other. The first portion 23a of the first structural layer 23 (on the left in
The etching technique used in step S8 of
The etching of the first structural layer 23 beneficially opens onto the second portion 22b of the first sacrificial layer 22.
Alternatively, the second structural layer 25 and the first structural layer 23 may be etched separately, using different etching chemistries, when both layers are made of different materials.
With reference to
Etching of the second sacrificial layer 24 is in an embodiment isotropic etching selective with respect to the substrate 21, the first structural layer 23 and the second structural layer 25. The second sacrificial layer 24 is in an embodiment etched chemically, for example by immersing the stack in a hydrofluoric acid (HF) bath in the liquid or vapour phase (in the case of a silicon oxide layer) for a controlled time.
In contrast, part of the first sacrificial layer 22 (more particularly of the second portion 22b) located vertically aligned with the periphery of the rigidifying structure 112 is etched at the same time as the second sacrificial layer 24, thereby forming a cavity 22′ in the first sacrificial layer 22. The etching can be controlled in time so that this cavity 22′ is of low extension.
The etching of the sacrificial layers 22 and 24 may also serve to release the movable electrode from the capacitive detection means (before it is enclosed in the controlled atmosphere chamber).
With reference to
The assembly formed by the stack of layers 21-25 and the cap 30 may then be flipped over, to facilitate subsequent etching of the substrate 21. After this flipping, the substrate 21 is beneficially thinned, for example by DRIE etching or by grinding and then CMP, and in an embodiment to a thickness of between 30 μm and 300 μm, that is the desired thickness for the first transmission arm 14.
Step S11 of
As illustrated in
Finally, in step S12 (cf.
The etching of the first sacrificial layer 22 is in an embodiment an isotropic etching selective with respect to the substrate 21, the first structural layer 23 and the second structural layer 25. The first sacrificial layer 22 is in an embodiment etched chemically, for example by immersing the assembly in a hydrofluoric acid (HF) bath in the liquid or vapour phase (in the case of a silicon oxide layer) for a controlled time.
In a first step S21 represented in
Then, in a second step illustrated in
Like the step of transferring the first structural layer 23 described in connection with
The transfer substrate 40′ is thinned down to the third structural layer 32 at least facing the cavity 104b. One or more portions of the transfer substrate 40′ may be kept around the sealed cavity 104b, in order to increase the back volume 12. In the case of a multi-layer structure SOI, thinning S23 the transfer substrate 40′ may be carried out in two successive operations illustrated by
More generally, the manufacturing method of
To obtain the electroacoustic transducer 1 according to
To obtain the electroacoustic transducer 1 according to
The stack 20 used as a starting point for this alternative method comprises successively the substrate 21, the first sacrificial layer 22 and the first structural layer 23, but no sealed cavities 103a provided within the first sacrificial layer 22 (see
The alternative method then does not include any of the steps S1-S5 aiming at forming the sealed cavity 103a (of the first wall 101), but merely a step of providing the stack 20. The second sacrificial layer 24 may not comprise the first portion 24a and the second structural layer 25 may not be etched out of the piston (although this is useful for enlarging the back volume 12).
The piston 11 may be devoid of a rigidifying structure 112. Steps S6 (forming the second sacrificial layer 24), S7 (forming the second structural layer 25), S8 (etching the second structural layer 25) and S9 (removing the second sacrificial layer 24) may then not be implemented.
Thus, more generally, the method for manufacturing an electroacoustic transducer according to an aspect of the invention comprises the following steps of:
The method manufacturing has been further described using a capacitive detection microphone as an example, one face of which is subjected to atmospheric pressure and the other face subjected to a reference pressure. The manufacturing method is, however, applicable to other types of microphone and other types of electroacoustic transducer, especially a loudspeaker (sound emitter) or an ultrasound emitter.
More generally, a microphone comprises in the second zone (controlled atmosphere chamber) means for measuring movement of the transmission device and/or force applied to the transmission device. These measurement means comprise for example a vibrating beam (resonating beam microphone).
In the case of a loudspeaker or ultrasonic transmitter, an actuator (for example capacitive actuator) replaces the measurement means in the second zone. The actuator moves the first end of the second transmission arm. This movement is transmitted by the transmission device to the piston 11 secured to the first end of the first transmission arm 14. The movement of the membrane 111 of the piston 11 enables the emission of sound (or ultrasound).
It will be appreciated that the various embodiments described previously are combinable according to any technically permissible combinations.
The articles “a” and “an” may be employed in connection with various elements and components of compositions, processes or structures described herein. This is merely for convenience and to give a general sense of the compositions, processes or structures. Such a description includes “one or at least one” of the elements or components. Moreover, as used herein, the singular articles also include a description of a plurality of elements or components, unless it is apparent from a specific context that the plural is excluded.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2205088 | May 2022 | FR | national |
