The embodiments of the present invention relate to curved surface supported structures that can be used as hemispherical resonator gyroscopes.
Hemispherical resonator gyroscopes are known which are gyroscopes that detect angular velocity. This type of hemispherical resonator gyroscope 9 has a resonator 91 formed in a generally hemispherical shape, a stem 90 supporting the resonator 91, a plurality of electrodes 92 formed on the outside of the resonator 91 and disposed in an annular pattern, and a plurality of electrodes 93 formed on the inside of the resonator 91 and disposed in an annular pattern, as shown in
In the hemispherical resonator gyroscope 9, a plurality of electrodes 92 or 93 are used alternately in the circumferential direction as either sensing electrodes 92A, 93A or control electrodes 92B, 93B. The resonator 91 resonates by electrostatic attraction when a restraining voltage is applied to the control electrodes 92B, 93B. When angular velocity is input in this state, the resonance pattern of the resonator 91 rotates according to the angular velocity, and the angular velocity can be determined by measuring the capacitance between the resonator 91 and the sensing electrodes 92A, 93A. It may also be possible to use a plurality of electrodes 94 formed beneath the resonator 91 and disposed in an annular pattern (see
The Q-factor of the resonator and the relative positions of the electrodes determine the performance of such hemispherical resonator gyroscopes. In order to increase the Q-factor of the resonator to reduce noise and improve performance, quartz or synthetic glass with a low thermoelastic modulus is used for the resonator. The resonators are made by processing quartz or synthetic glass, both of which are difficult materials to work with and require high precision machining. Therefore, such a resonator manufacturing process requires mechanical polishing and cutting followed by final shape adjustment by laser machining, which makes the manufacturing cost very high.
In order to reduce the manufacturing cost of the resonators, manufacturing methods based on the MEMS (Micro Electro Mechanical Systems) process may be proposed. A known method for this kind of manufacturing is to process a quartz wafer into what is called a wine glass or bird bath shape by heating it to a deformable temperature and then suctioning or pressurizing it.
However, such methods require laser cutting and polishing when the resonator is separated, as well as bonding the resonator with adhesive or other means to a substrate on which electrodes are formed. As a result, the alignment accuracy is often inferior to that of semiconductor machines used in common MEMS processes, and the performance of the hemispherical resonator gyroscopes produced by this method may be deteriorated. Moreover, since this method is not a batch production process, the cost of manufacturing the hemispherical resonator gyroscopes will be high.
The problem that embodiments of the present invention seek to solve is to provide, at a lower cost, a technique that enables the manufacturing of curved surface supported structures that can be used as hemispherical resonator gyroscopes.
In order to solve the above-mentioned problem, the method for manufacturing a curved surface supported structure comprising an upper wafer and a lower wafer, the method comprising: forming an annular recess on an upper surface of the lower wafer by etching, and a stem having a tip higher than a radially-outer-surface a generally center of the recess by etching the radially-outer-surface, which is a plane located radially outer side of the recess; forming a plurality of first electrodes arranged on the radially-outer-surface; forming a sacrificial layer, which is an annular deposition pattern on the plurality of first electrodes; forming a plurality of second electrodes, which are arranged on a bottom surface of the upper wafer in correspondence with the plurality of first electrodes; bonding the upper wafer and the lower wafer with the sacrificial layer in between so that the plurality of first electrodes and the plurality of second electrodes are superimposed; separating a radially outer portion, which is located radially outer side of the upper wafer than the second electrodes by etching after the bonding; vacuum heating the upper wafer, the lower wafer, and the sacrificial layer are under a condition where a pressure in a cavity defined by the upper wafer, the lower wafer, and the sacrificial layer is different from an ambient pressure after the separating; and removing the sacrificial layer by etching, after the vacuum heating at the pressure different from the ambient pressure.
The embodiments of the present invention enable the manufacturing of curved surface supported structures that can be used as hemispherical resonator gyroscopes at a lower cost.
In the following, embodiments of the invention are described with reference to the drawings.
An outline of the method for manufacturing a curved surface supported structure of the present embodiment will be described.
As shown in
After the sacrificial layer depositing step and the second electrode forming step are performed, a bonding step is performed to bond the upper wafer and the lower wafer together by the sacrificial layer (S105), and a radially-outer-portion separating step is performed to separate the radially outer portion of the upper wafer (S106).
After the radially-outer-portion separating step is performed, an equal-pressure heating step (S107) and an unequal-pressure heating step (S108) are performed, in which a vacuum heating is performed by a vacuum heater equipped with a chamber, and then a sacrificial layer removing step (S109) is performed to remove the sacrificial layer, thereby manufacturing a curved surface supported structure which can be used as a hemispherical resonator gyroscope.
The stem forming step is described below.
The stem forming step is a step to form a stem 11 by forming an annular recess on the lower wafer 1, as shown in
The first electrode forming step is described below.
The first electrode forming step is a step to form a plurality of first electrodes 13 made of high-melting point metal on the radially-outer-surface 12 of the lower wafer 1, as shown in
The sacrificial layer depositing step is described below.
The sacrificial layer depositing step, as shown in
The second electrode forming step is described below.
The second electrode forming step is a step to form a plurality of second electrodes 23 on the upper wafer 2, as shown in
In this embodiment, each of the plurality of second electrodes 23, when superimposed on a corresponding first electrode 13, is assumed to be formed small enough to fit within the area of the first electrode 13, but alternatively the first electrodes 13 may be formed smaller than the second electrodes 23. Forming one of the first electrodes 13 or second electrodes 23 to fit within the area of the other, as described above, can minimize adverse effects caused by possible misalignments in the bonding step.
In the stem forming step, the radially-outer-surface 12 is etched so that the distance between the tip of the stem 11 and the radially-outer-surface 12 is greater than the distance of the combined thicknesses of the first electrode 13 and the second electrode 23. This creates a gap between the first electrodes 13 and the second electrodes 23 when they are superimposed in the bonding step, which will be described in detail later.
The bonding step is described below.
The bonding step is a step to bond the bottom surface of the upper wafer 2 and the top surface of the lower wafer 1 so that the plurality of first electrodes 13 and their corresponding plurality of second electrodes 23 are superimposed, as shown in
If the upper wafer 2 and the lower wafer 1 are made of Tempax glass or silicon, the upper wafer 2 and the lower wafer 1 may be bonded together using an anodic bonder instead of a double-sided aligner. Regardless of which method is used, this bonding step can keep alignment errors at the semiconductor process level (5 um or less).
The radially-outer-portion separating step is described below.
The radially-outer portion separating step is a step to separate the radially outer portion of the upper wafer 2 by etching, as shown in
The unequal-pressure heating step may deform the upper wafer 2 into a three-dimensional shape, as will be described in detail later, however, etching the flat upper wafer 2 prior to the unequal-pressure heating step allows the precision patterns of the semiconductor process to be applied and eliminates the need for expensive laser cutting and polishing steps.
Although the etching step may produce sharp-edged portions at the periphery of the upper wafer 2, such edges of the upper wafer 2 will be rounded when heat-treated by the equal-pressure and unequal-pressure heating steps. As a result, the curved surface supported structure manufactured by this manufacturing method has a high energy confinement effect when used as a hemispherical resonator gyroscope, resulting in an improved Q-factor.
The equal-pressure heating step and the unequal-pressure heating step are described below.
The equal-pressure heating step is a step in which the upper wafer 2 and the lower wafer 1 are vacuum heated until they soften, with the ambient pressure P2, which is the pressure in the chamber of the vacuum machine, generally equal to the cavity pressure P1. In the equal-pressure heating step, the temperature in the chamber should be 1200˜1400° C. if the material of the upper wafer 2 and the lower wafer 1 is quartz, and 500˜600° C. if the material is Tempax glass. The equal-pressure heating step fuses the stem 11 of the lower wafer 1 and the upper wafer 2 into one piece, and also fuses the deposition pattern 3 made of liquid glass to the lower wafer 1 and the upper wafer 2, thereby making the cavity C airtight. The equal-pressure heating step may be omitted from this manufacturing method, because the fusing of the lower wafer 1 to the upper wafer 2 and the fusing of the deposition pattern 3 to the lower wafer 1 and the upper wafer 2 may also be effected in the unequal-pressure heating step.
The unequal-pressure heating step is a step in which the upper wafer 2 and the lower wafer 1 are vacuum heated to the point of softening while the ambient pressure P2 is made different from the cavity pressure P1, that is, the ambient pressure P2 is made lower than the cavity pressure P1 or the ambient pressure P2 is made higher than the cavity pressure P1. In the unequal-pressure heating step, the temperature in the chamber should be 1400 to 1700° C. if the material of the upper wafer 2 and the lower wafer 1 is quartz, and 600 to 700° C. if the material is Tempax glass.
When the ambient pressure P2 is lower than the cavity pressure P1 in the unequal-pressure heating step, the cavity C expands to deform a part of the upper wafer 2 to form an annular convex surface 21A having a curved surface projecting upward along an annulus as shown in
Alternatively, when the ambient pressure P2 is higher than the cavity pressure P1 in the unequal-pressure heating step, the cavity C contracts to deform a part of the upper wafer 2 to form an annular concave surface 21B having a curved surface projecting downward along an annulus as shown in
In either the unequal-pressure heating step in which the ambient pressure P2 is lower than the cavity pressure P1, or the unequal-pressure heating step in which the ambient pressure P2 is higher than the cavity pressure P1, the thickness, height, curvature, etc. of the annular convex surface 21A or the annular concave surface 21B can be made as desired by adjusting the pressure difference between the cavity pressure P1 and the ambient pressure P2, the temperature in the chamber during vacuum heating, the lifting time of the lifting mechanism in the vacuum heater, etc.
In the unequal-pressure heating step, the composition of the liquid glass that forms the deposition pattern 3 becomes closer to that of quartz, which improves the air tightness in cavity C, but its chemical resistance becomes worse compared to that of the materials of the upper wafer 2 and the lower wafer 1.
The sacrificial layer removing step is described below.
The sacrificial layer removing step is a step to remove the deposition pattern 3 formed with liquid glass by etching. The deposition pattern 3, which is denatured by vacuum heating, has a faster etch rate than the other portions and can be selectively removed by etching. Alternatively, chemicals that etches only the liquid glass forming the deposition pattern 3 may be used in the sacrificial layer removing step.
The sacrificial layer removing step produces a curved surface supported structure 4A having an upwardly projecting annular convex surface 21A, as shown in
With the manufacturing methods described above, the curved surface supported structures 4A and 4B, which can be used as hemispherical resonator gyroscopes, can be manufactured using existing low-cost processes. In this manufacturing method, an annular convex surface 21A or an annular concave surface 21B, a stem 11, respectively, having a three-dimensional structure, first electrodes 13 and second electrodes 23 are integrally formed. Therefore, no mechanical alignment is required in the manufacturing steps, and when the curved surface supported structures 4A or 4B are used as hemispherical resonator gyroscopes, performance degrading phenomena caused by misalignment such as drift are prevented.
In the description of this embodiment, while the plurality of first electrodes 13 and the plurality of second electrodes 23 are assumed to be arranged in an annular pattern, the plurality of first electrodes 13 may be arranged on the radially-outer-surface 12, and the plurality of second electrodes 23 may be arranged on the bottom surface of the upper wafer 2, corresponding to the plurality of first electrodes 13.
The embodiments of the present invention have been presented by way of example only, and are not intended to limit the scope of the invention. The novel embodiments described herein may be embodied in a variety of other forms; furthermore, various omissions, substitutions and changes may be made without departing from the spirit of the invention. The embodiments and modifications are included in the scope or spirit of the present invention and in the appended claims and their equivalents.
Number | Date | Country | Kind |
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2021-073086 | Apr 2021 | JP | national |
Filing Document | Filing Date | Country | Kind |
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PCT/JP2022/014314 | 3/25/2022 | WO |