A movable mass forming a seismic mass is formed starting from an epitaxial layer and is covered by a weighting region of tungsten which has high density. To manufacture the mass, buried conductive regions are formed in the substrate. Then, at the same time, a sacrificial region is formed in the zone where the movable mass is to be formed and oxide insulating regions are formed on the buried conductive regions so as to partially cover them. An epitaxial layer is then grown, using a nucleus region. A tungsten layer is deposited and defined and, using a silicon carbide layer as mask, the suspended structure is defined. Finally, the sacrificial region is removed, forming an air gap.
|
1. A process for manufacturing an accelerometric and gyroscopic integrated sensor, comprising the steps of:
forming a sacrificial region on in a substrate of semiconductor material;
growing an epitaxial layer on said substrate and said sacrificial region; and
removing selective portions of said epitaxial layer and said sacrificial region to form a movable mass surrounded at the sides and separated from fixed regions by trenches and separated from said substrate by an air gap, the movable mass supported by anchorage zones only at the sides; and
forming a weighting region of tungsten at said movable mass.
0. 14. A process for manufacturing an accelerometric and gyroscopic integrated sensor, comprising the steps of:
forming a sacrificial region in a substrate of semiconductor material;
growing an epitaxial layer on said substrate and said sacrificial region; and
removing selective portions of said epitaxial layer and said sacrificial region to form a movable mass surrounded at the sides and separated from fixed regions by trenches and separated from said substrate by an air gap, the movable mass supported by anchorage zones only at the sides; and
forming a weighting region of a metal at said movable mass.
0. 16. A method for producing an integrated sensor comprising the steps of:
forming a sacrificial support layer in a semiconductor substrate;
forming an epitaxial layer in the sacrificial support layer and on the semiconductor substrate;
depositing a metal layer on the epitaxial layer;
removing the sacrificial support layer; and
forming a movable mass from portions of the epitaxial layer and the metal layer by forming trenches to separate the movable mass from fixed regions of the epitaxial layer and weighting region and separated from said substrate by an air gap, the movable mass thereby supported by anchorage zones only at the sides.
10. A method for producing an integrated sensor comprising the steps of:
forming a sacrificial support layer on in a semiconductor substrate;
forming an epitaxial layer on the sacrificial support layer and on the semiconductor substrate;
depositing a tungsten layer weighting region on the epitaxial layer;
removing the sacrificial support layer; and
forming a movable mass from portions of the epitaxial layer and tungsten layers the weighting region by forming trenches to separate the movable mass from fixed regions of the epitaxial layer and tungsten layers weighting region and separated from said substrate by an air gap, the movable mass thereby supported by anchorage zones only at the sides.
0. 18. A process for manufacturing an accelerometric and gyroscopic integrated sensor, comprising the steps of:
forming a sacrificial region on a substrate of semiconductor material;
growing an epitaxial layer on said substrate and said sacrificial region;
removing selective portions of said epitaxial layer and said sacrificial region to form a movable mass surrounded at the sides and separated from fixed regions by trenches and separated from said substrate by an air gap, the movable mass supported by anchorage zones only at the sides; and
forming a weighting region at said movable mass,
wherein a step of forming a nucleus region of non-single-crystal semiconductor material on said sacrificial region is carried out before said step of growing an epitaxial layer and wherein said step of growing an epitaxial layer comprises the step of growing a multi-crystal region on said nucleus region and growing a single-crystal region on said substrate, and wherein said suspended mass is formed in said multi-crystal region and wherein the process comprises the step of forming electronic components in said single-crystal region.
2. The process according to
3. The process according to
4. The process according to
5. The process according to
6. The process according to
forming electronic components in said epitaxial layer;
depositing a dielectric layer over said electronic components; and
forming contact openings in said dielectric layer, and wherein said step of defining said tungsten layer further comprises the step of forming tungsten contact electrodes for said electronic components and for said accelerometric and gyroscopic sensor.
7. The process according to
8. The process according to
9. The process according to
11. The method of
12. The method of
forming a protective layer on the tungsten layer weighting region;
masking a pattern on the protective layer; and
etching trenches through the protective layer, tungsten, and epitaxial layers layer, and the weighting region.
13. The method of
forming electronic components in the epitaxial layer;
depositing a dielectric layer over the components; and
forming contact openings in the dielectric layer.
0. 15. The process according to
0. 17. The process according to
0. 19. The process according to
0. 20. The process of
|
This application is a divisional of pending U.S. patent application Ser. No. 09/126,625, filed Jul. 30, 1998.
The invention relates to a process for manufacturing high-sensitivity accelerometric and gyroscopic integrated sensors and a sensor thus produced.
As is known, using electromechanical microstructures of semiconductor material, the manufacture of which utilizes microelectronics techniques, has recently been proposed for producing accelerometers and gyroscopes. These silicon micro-machining techniques make it possible to produce different types of angular velocity and acceleration sensors. In particular, at the present lime prototypes operating according to the piezoelectric, piezoresistive, capacitive, threshold, resonant and tunnel effect principles have been proposed.
Reference will be made below to an accelerometric sensor of differential capacitive type, i.e. one in which acceleration induces the movement of a seismic mass which constitutes the electrode common to two coupled capacitors by varying the two capacitances in opposite directions. This effect is known as differential variation of capacitance.
Historically, integrated micro-structures have been manufactured by preferably using the “bulk micro-machining” technique in which a wafer of single-crystal silicon is machined on both faces. This technique is, however, incompatible with the process steps for producing components of a circuit which processes a signal picked up by a sensitive element, as required at present.
It has been proposed to use the technique of “surface micro-machining” in which the sensitive element is made of multi-crystal silicon and suspended structures are formed by depositing and successively removing sacrificial layers. This technique is compatible with the current integrated circuit manufacturing processes and is therefore preferred at present. The integrated micro-structures produced with this technique are, however, relatively insensitive to acceleration and angular velocity. In fact, having a mass of the order of a few tenths of a microgram, they suffer the effects of thermodynamic noise caused by the Brownian movement of the particles of the fluid in which they are immersed (see, for example, the article by T. B. Gabrielson entitled “Mechanical-Thermal Noise in Micromachined Acoustic and Vibration Sensors”, IEEE Transactions on Electron Devices, vol. 40, No. 5, May 1993). The upper limit to the mass obtainable with these structures is imposed by genuinely technological reasons; the deposition of very thick films involves extremely long wafer machining times and renders the surface of the wafer unsuitable for the successive operations such as lapping the wafers.
A technique for machining the epitaxial layer (epitaxial micro-machining) is also known, which produces micro-structures with inertial masses that are higher and hence more sensitive, but not yet at a sufficient value for practical applications.
An object of the invention is to improve a process for manufacturing an accelerometric and gyroscopic sensor according to a technique of “epitaxial micro-machining” so as to increase its sensitivity further than the prior art.
An embodiment of the invention provides a process for manufacturing a high-sensitivity accelerometric and gyroscopic integrated sensor including forming a sacrificial region on a substrate of semiconductor material, growing an epitaxial layer that includes tungsten on the substrate and the sacrificial region, and then removing selective portions of the epitaxial layer and the sacrificial region to form a movable mass. The moveable mass formed is surrounded at the sides and separated from fixed regions by trenches, and separated from the substrate by an air gap.
It also provides for an accelerometric integrated sensor, having a substrate and an epitaxial layer of semiconductor material, whereby the epitaxial layer includes tungsten and forms a movable mass which is surrounded at sides by a fixed mass. The movable mass is separated from the substrate by a gap from below and from the fixed mass by trenches at the sides, and is supported by the fixed mass through anchorage portions.
For an understanding of the invention, a number of preferred embodiments will now be described, purely by way of non-exhaustive example, with reference to the accompanying drawings.
An embodiment of a capacitive-type accelerometric or gyroscopic sensor according to a first embodiment of the process will now be described with reference to
Shown in
Through suitable masking steps, portions of the layers 5, 6 are then removed in the sensor zone 7 where the buried contacts of the sensor and of the silicon nitride layer 6 are to be formed in the circuitry and from an interconnection area 10, obtaining the structure of FIG. 3. In
An amorphous or multi-crystal silicon layer 12 is then deposited, as shown in FIG. 4. By means of a phototechnique and plasma etching step, the amorphous or multi-crystal silicon layer 12 is removed, except in the sensor zone 7, forming a silicon region 12′ representing the nucleus for a successive epitaxial growth step. By means of chemical etching, the pad oxide layer 5 is then removed where exposed and epitaxial growth takes place with formation of a “pseudo-epitaxial”, P-type layer 13. In the sensor zone 7, the layer 13 has a multi-crystal structure (multi-crystal region 13′) and a single-crystal structure elsewhere (single-crystal region 13″). A wafer 14 as shown in
The pseudo-epitaxial layer 13 is then doped with doping ions suitable for determining an N-type conductivity to form deep regions. In particular, as shown in
The electronic components of the circuitry are then formed by means of standard steps. In the example shown, an N-type collector well 15 is formed, extending from the surface 16 of the pseudo-epitaxial layer 13 as far as the substrate 1. An NPN transistor 23, having an N+-type collector contact region 20, a P-type base region 21 and an N+-type emitter region 22 is formed in the collector well 15.
A dielectric layer 24 for opening the contacts, e.g., BPSG (boron phosphorus silicon glass) is then deposited on the surface 16 of the wafer 14. Then, by a suitable masking and selective removal step, the contacts are opened in the circuitry area and on the deep region 18, and a part of the dielectric layer 24 is removed from the sensor zone 7. An adhesive layer 25 (of titanium nitride for example) is then deposited, to facilitate the adhesion of the next layer to the silicon of the wafer 14. A tungsten layer 26 is deposited by CVD (Chemical Vapor Deposition) at a thickness of 1 μm thick, for example, obtaining the intermediate structure of FIG. 6. The nucleus silicon region 12′ has been omitted in FIG. 6.
The tungsten layer 26 is then shaped, by means of known photo-lithographic steps, so as to form contacts 26a of the circuitry and 26b of the sensor and a weighting region 26c over the well 19, as shown in
A silicon carbide layer 31, intended to form a mask for the subsequent step of excavation of the pseudo-epitaxial layer 13 and precisely of the multi-crystal region 13′, is then deposited and defined. Excavations are carried out to release the movable mass of the accelerometer, to separate the fixed and movable electrodes and to insulate the regions at different potential. Thus a trench 33a which separates the fixed part from the movable part and the fixed mass from the surrounding portion of the well 19 is formed. A trench 33b (see
Finally, the sacrificial region 8 is removed by etching in, e.g., hydrofluoric acid, and the zone previously occupied by this region 8 forms an air gap 38 which at the bottom separates the movable mass from the rest of the wafer. The movable mass is then etched and supported by the chip only at the anchorage zones. With a subsequent etching in plasma, the silicon carbide layer 31 is removed from all areas of the wafer. The final structure is thus obtained which is shown in
As will be noted, the movable mass 40 is H-shaped and the transverse walls 34 define the movable electrodes of the capacitive sensor. The moveable electrodes are interleaved in a comb-like manner with the transverse walls 35 defining the fixed electrodes and are separated from its central element. The structure is therefore equivalent to a capacitor formed by two capacitors in series, each formed by a plurality of elementary capacitors connected in parallel.
In per se known manner, through the deep regions 18 and the buried conductive regions 2, 2′, 2″, and 3, the movable electrodes 34 and the fixed electrodes 35 are biased at different voltages so that when the movable mass 40 is subjected to acceleration, the consequent change of distance between the movable electrodes and the fixed ones may be detected as a variation of capacitance.
Manufacturing the movable mass 40 in a semiconductor material having a tungsten weighting region 26c, as described, gives the sensor high sensitivity. In fact, tungsten has high density (19.3 g/cm3) with respect to multi-crystal or amorphous silicon (2.33 g/cm3). Consequently, a tungsten layer 1 μm thick is virtually equivalent, from the point of view of the mechanical properties, to a 10 μm polysilicon layer. On the other hand, the deposition by CVD of a tungsten layer of the indicated thickness can easily be achieved with the conventional integrated microelectronics machining techniques.
The sensor obtained in this way thus has high sensitivity, yet benefits from the advantages typical of epitaxial machining technology and permits the integration of the sensor together with the integrated signal processing circuit.
The manufacturing process is simple to implement, using steps typical of microelectronics and forms the metallic circuit interconnection regions and the weighting regions of the movable structure at the same time. The process is also readily controllable and repeatable.
According to a different embodiment of the invention, the buried oxide regions 8 and 9 are grown in recesses previously formed in the substrate 1, after the buried conductive regions 2, 3 have been formed. In detail, shown in
According to a further embodiment which is not shown, the sacrificial and buried oxide regions may be obtained by depositing and shaping an oxide layer.
Finally it will be clear that numerous modifications and variations may be introduced to the process and sensor described and illustrated herein, all coming within the scope of the inventive concept as defined in the accompanying claims. In particular, the components of the circuitry integrated with the sensor may be either bipolar or MOS; the conductivity of the conductive regions may be the opposite of that shown and the protective and/or adhesive materials may be replaced by others which are equivalent as regards the functions desired, as well as other changes and variations.
Ferrera, Marco, Ferrari, Paolo, Vigna, Benedetto, Montanini, Pietro
Patent | Priority | Assignee | Title |
8007167, | Sep 30 2005 | Silicon Laboratories Inc | Integrated electronic sensor |
8357958, | Apr 02 2004 | Silicon Laboratories Inc | Integrated CMOS porous sensor |
8497531, | Apr 02 2004 | Silicon Laboratories Inc | Integrated MOS gas or humidity sensor having a wireless transceiver |
8507954, | Apr 02 2004 | Silicon Laboratories Inc | Integrated CMOS porous sensor having sensor electrodes formed with the interconnect conductors of a MOS circuit |
8507955, | Apr 02 2004 | Silicon Laboratories Inc | Sensor device having MOS circuits, a gas or humidity sensor and a temperature sensor |
8648395, | Apr 02 2004 | Silicon Laboratories Inc | Integrated CMOS porous sensor |
8669131, | Sep 30 2011 | Silicon Laboratories Inc | Methods and materials for forming gas sensor structures |
8691609, | Sep 30 2011 | Silicon Laboratories Inc | Gas sensor materials and methods for preparation thereof |
8852513, | Sep 30 2011 | Silicon Laboratories Inc | Systems and methods for packaging integrated circuit gas sensor systems |
9164052, | Sep 30 2011 | Silicon Laboratories Inc | Integrated gas sensor |
Patent | Priority | Assignee | Title |
4699006, | Mar 19 1984 | The Charles Stark Draper Laboratory, Inc. | Vibratory digital integrating accelerometer |
4783237, | Dec 01 1983 | Harry E., Aine; Barry, Block | Solid state transducer and method of making same |
5016072, | Jan 13 1988 | The Charles Stark Draper Laboratory, Inc. | Semiconductor chip gyroscopic transducer |
5395802, | Mar 31 1992 | Nissan Motor Co., Ltd. | Process for making semiconductor acceleration sensor having anti-etching layer |
5417111, | Aug 17 1990 | Analog Devices, Inc. | Monolithic chip containing integrated circuitry and suspended microstructure |
5591910, | Jun 03 1994 | Texas Instruments Incorporated | Accelerometer |
5616514, | Jun 03 1993 | Robert Bosch GmbH | Method of fabricating a micromechanical sensor |
5747353, | Apr 16 1996 | National Semiconductor Corporation | Method of making surface micro-machined accelerometer using silicon-on-insulator technology |
5830777, | Oct 31 1994 | Kabushiki Kaisha Tokai Rika Denki Seisakusho | Method of manufacturing a capacitance type acceleration sensor |
6020215, | Jan 31 1994 | Canon Kabushiki Kaisha | Process for manufacturing microstructure |
6090638, | Jul 10 1997 | STMICROELECTRONICS S R L | Process for manufacturing high-sensitivity capacitive and resonant integrated sensors, particularly accelerometers and gyroscopes, and sensors made therefrom |
6133059, | Sep 21 1993 | Infineon Technologies AG | Integrated micromechanical sensor device and process for producing it |
6199874, | May 26 1993 | GEFUS SBIC II, L P | Microelectromechanical accelerometer for automotive applications |
DE4318466, |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Feb 05 2003 | STMicroelectronics S.r.l. | (assignment on the face of the patent) | / |
Date | Maintenance Fee Events |
Jul 25 2012 | M1553: Payment of Maintenance Fee, 12th Year, Large Entity. |
Date | Maintenance Schedule |
Oct 26 2013 | 4 years fee payment window open |
Apr 26 2014 | 6 months grace period start (w surcharge) |
Oct 26 2014 | patent expiry (for year 4) |
Oct 26 2016 | 2 years to revive unintentionally abandoned end. (for year 4) |
Oct 26 2017 | 8 years fee payment window open |
Apr 26 2018 | 6 months grace period start (w surcharge) |
Oct 26 2018 | patent expiry (for year 8) |
Oct 26 2020 | 2 years to revive unintentionally abandoned end. (for year 8) |
Oct 26 2021 | 12 years fee payment window open |
Apr 26 2022 | 6 months grace period start (w surcharge) |
Oct 26 2022 | patent expiry (for year 12) |
Oct 26 2024 | 2 years to revive unintentionally abandoned end. (for year 12) |