Micromechanical system fabrication method using (111) single crystalline silicon

[0002] This is a continuation application of copending U.S. patent application Ser. No. 09/250,519 filed on Feb. 16, 1999, now U.S. Pat. No. 6,150,275.

[0003] 1. Field of the Invention

[0004] The present invention relates to a micromechanical system and more particularly to a micromechanical system fabrication method using (111) single crystalline silicon.

[0005] 2. Description of Related Art

[0006] A micromechanical system, also called micromachined system, is implemented by patterning and integrating particular portions of the system on a silicon substrate in a precise shape in micrometer scale using silicon fabrication processes. This is based upon semiconductor device fabrication techniques such as deposition of a thin film, etching, photolithography, and impurity diffusion and doping.

[0007] Micromechanical systems include the silicon accelerometers for sensing the acceleration of a moving body and the gyroscope for sensing the angular velocity of a rotating body.

[0008] Such micromechanical systems comprise of a moving parts and a stationary parts, which, when viewed on the cross section of the silicon substrate, are fabricated separated from the silicon substrate.

[0009] Conventionally the bulk micromachining method, in which a (100) single crystalline silicon or (110) single crystalline silicon is etched in an aqueous alkaline solution so as to fabricate a microstructure, and the surface micromachining method, in which polycrystalline silicon deposited on a silicon substrate is released at specified locations by a sacrificial layer etching technique, are used so as to fabricate a micromechanical system.

[0010] On the other hand, the present invention provides a micromachining method using (111) single crystalline silicon. In the present invention, micromachining method is also referred to as micromechanical system fabrication method.

[0011] FIG. 1 illustrates various planes of single crystalline silicon. FIG. 1 shows the (100), (110), and (111) planes in the single crystalline silicon, which has a cubic lattice structure.

[0012] Micromachining methods using the (100) single crystalline silicon or the (110) single crystalline silicon as the silicon substrate are conventionally well known. To use the (100) single crystalline silicon as the silicon substrate means to use a single crystalline silicon that is oriented in the direction of the (100) plane. This is implemented by using a silicon wafer that is cut from an ingot in the (100) plane during a wafer manufacturing process.

[0013] While the conventional micromachining methods using the (100) single crystalline silicon or the (110) single crystalline silicon are already well known, nothing about a micromachining method using (111) single crystalline silicon is known until now.

[0014] This is because studies on the crystallographic characteristics and the characteristics in fabrication steps with respect to the (111) single crystalline silicon, reflecting particular essential factors of a micromechanical system, different from the semiconductor device fabrication method, have not been actively conducted.

[0015] Accordingly, the present invention is directed to a method using the (111) single crystalline silicon to fabricate micromechanical systems that substantially obviates one or more of the limitations and disadvantages of the related art.

[0016] An objective of the present invention is to provide a micromechanical system fabrication method using (111) single crystalline silicon, wherein the crystallographic characteristics and characteristics in fabrication steps with respect to the (111) single crystalline silicon are utilized in fabricating a micromechanical system, thereby improving the micromachining technology.

[0017] Additional features and advantages of the invention will be set forth in the following description, and in part will be apparent from the description, or may be learned by practice of the invention. The objectives and other advantages of the invention will be realized and attained by the structure as illustrated in the written description and claims hereof, as well as the appended drawings.

[0018] To achieve these and other advantages, and in accordance with the purpose of the present invention as embodied and broadly described, a micromechanical system fabrication method using (111) single crystalline silicon, comprising: fabrication step, in which the (111) single crystalline silicon is utilized as a silicon substrate; reactive ion etching step, in which microstructures which have to be separated from the silicon substrate are patterned; and selective release-etching step, in which the microstructures are separated from the silicon substrate in an aqueous alkaline solution.

[0019] The step of reactive ion etching allows a thickness of the microstructures themselves and spacing between the silicon substrate and the microstructures separated from the silicon substrate to be defined and adjusted.

[0020] In the step of selective release-etching, the etch is selectively performed with respect to {100} planes and {110} planes, thus preventing the microstructures from being damaged, and the microstructures are readily separated from the silicon substrate due to slow etching characteristics of {111} planes that are left after the selective release-etching step in an aqueous alkaline solution.

[0021] The step of reactive ion etching comprises: a first reactive ion etching step of defining the thickness of the microstructures themselves; and a second reactive ion etching step of defining the spacing between the microstructures and the silicon substrate.

[0022] The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention.

[0023] In the drawings:

[0024] FIG. 1 illustrates planes of single crystalline silicon;

[0025] FIGS. 2a, 2b, 2cshow {111} planes of (111) single crystalline silicon and their normal directions;

[0026] FIG. 3 is a plan view of a pattern fabricated in accordance with a micromechanical system fabrication method according to the present invention;

[0027] FIGS. 4a, 4b, 4c, 4d, 4e, 4f, 4g, 4h, 4ishow steps for fabrication of the pattern depicted in FIG. 3;

[0028] FIG. 5 is a scanning electron microscopic photograph of a microbridge fabricated in accordance with a micromechanical system fabrication method according to the present invention; and

[0029] FIG. 6 illustrates a comb drive fabricated in accordance with a micromechanical system fabrication method according to the present invention.

[0030] Reference will now be made in detail to the preferred embodiments of the present invention, examples of which are illustrated in the accompanying drawings.

[0031] With reference to the accompanying drawings, the present invention will now be described in detail.

[0032] Primarily, crystalline characteristics of the (111) single crystalline silicon are reviewed.

[0033] FIG. 2ashows two equilateral triangles surrounded by the {111} planes. FIG. 2bshows a cross sectional view taken along line A-A′ showing other {111} planes. FIG. 2cshows a cross sectional view taken along line B-B′ showing remaining {111} planes.

[0034] As shown in FIGS. 2band 2c, the {111} planes slant against a [111] normal direction of the (111) planes at an angle of ±19.47°.

[0035] Because of this crystallographic orientation characteristic, when selectively etching the {100} planes and {110} planes with an aqueous alkaline solution and separating a microstructure from a silicon substrate in the micromechanical system fabrication method according to the present invention, the {111} planes which have been left after the etching step slant against the direction [111] at the angle of ±19.47°.

[0036] FIG. 3 is a plan view of a pattern fabricated in accordance with the micromechanical system fabrication method according to the present invention. FIGS. 4ato 4iare cross sectional views taken along line C-C′ in FIG. 3 and show pattern fabrication steps.

[0037] FIG. 3 also shows the {111} planes of the (111) single crystalline silicon and their normal directions. Especially, dotted lines in FIG. 3 indicate normal directions of the {111} planes left after the wet etching step using an aqueous alkaline solution (see FIG. 4i).

[0038] To fabricate the pattern depicted in FIG. 3, a buffer oxide layer, a nitride layer, and a mask oxide layer are formed on a (111) single crystalline silicon substrate as shown in FIG. 4a.

[0039] Photolithography etching process (FIG. 4b) is then carried out on the buffer oxide layer, nitride layer, and mask oxide layer. After patterning as shown in FIG. 4c, the photoresist layer is removed (FIG. 4d).

[0040] Subsequently, a reactive ion etching (RIE) process is carried out on the (111) silicon substrate (FIG. 4e). The etch is performed vertically on the silicon substrate as shown in FIG. 4eand an etched depth can be readily adjusted within the range from a sub-micrometer up to 500 μm in the RIE process. In FIG. 4e, the etched depth on the silicon substrate corresponds to a thickness of a microstructure itself that will be finally separated from the silicon substrate in the micromechanical system. In other words, since the etched depth in the silicon substrate can be adjusted by using the RIE process, the thickness of the microstructure itself separated from the silicon substrate can be easily controlled within the range from the sub-micrometer up to 500 μm in this micromechanical system.

[0041] As illustrated above, the thickness of the microstructures are determined through the above first RIE step, and then a passivation step of overlaying protective films of the nitride layer and oxide layer is carried out (FIG. 4f). Subsequently, an other RIE process is performed with respect to the nitride layer and oxide layer as shown in FIG. 4g.

[0042] The second RIE process is also vertically carried out on the (111) silicon substrate (FIG. 4h). At this time, the etch is also performed vertically on the silicon substrate as shown in FIG. 4h, and the etched depth can be readily adjusted within the range from a sub-micrometer up to 500 μm in the RIE process. The etched depth shown in FIG. 4hcorresponds to the spacing between the silicon substrate and the microstructures that will be finally separated from the silicon substrate in this micromechanical system. In other words, the etched depth on the silicon substrate can be controlled by using the RIE technique, thereby easily adjusting the spacing between the silicon substrate and the microstructures separated from the silicon substrate within the range from the sub-micrometer up to 500 μm in the micromechanical system.

[0043] As illustrated above, after the spacing between the silicon substrate and the microstructures is determined through the second RIE step, a wet etching step is carried out using an aqueous alkaline solution (FIG. 4i). The microstructures are separated from the silicon substrate through this step, so this step can be defined as a release-etching step. In this release-etching step using an aqueous alkaline solution, the {100} planes and the {110} planes are selectively etched, but the {111} planes is not etched.

[0044] Therefore, the microstructures that have been formed with the (111) single crystalline silicon are not damaged during the release-etching step. More specifically, the etching process does not damage a bottom surface of the microstructure.

[0045] Additionally, the {111} planes of the silicon substrate, which are left after the release-etching step, are not rough as shown in FIG. 4i. The {111} planes left after the release-etching step slant against the [111] direction at an angle of ±19.47°, but this does not influence the microstructures separated from the silicon substrate. Since the etch is vertically carried out in the first RIE step as shown in FIG. 4e, the side surfaces of the microstructures are patterned to be vertical.

[0046] Such selective release-etching process also has an advantage of allowing the microstructure to be readily separated from the silicon substrate without additional etched holes.

[0047] FIG. 5 is a scanning electron microscopic photograph of a microbridge fabricated in accordance with the micromechanical system fabrication method according to the present invention. The microbridge shown in FIG. 5 is formed to be 55 μm in length, 20 μm in width, and 4 μm in thickness. The spacing between the microbridge and the silicon substrate is 2 μm. The microbridge shown in FIG. 5 is formed by carrying out the RIE process on the (111) single crystalline silicon, so the side surfaces of the micro bridge are formed to be vertical.

[0048] The micromechanical system fabrication method using the (111) single crystalline silicon according to the present invention as illustrated above can be applied for various microstructures. FIG. 6 illustrates a comb drive fabricated in accordance with the micromechanical system fabrication method. In this comb drive structure, a moving beam in the form of tooth of a comb moves between tooth of a stationary beam that is also made in the form of tooth of a comb. Such movement of the moving beam causes change of spacing between the moving beam and the stationary beam. Based upon the change of the spacing between the two beams, change of capacitance of a plate capacitor composed of the moving and stationary beams can be sensed. According to the micromechanical system fabrication method using the (111) single crystalline silicon of the present invention, the side surfaces of microstructures such as the moving parts or the stationary parts can be formed to be vertical by using the RIE technique. Furthermore, the microstructures can be readily separated from the silicon substrate by employing the selective release-etching technique using slow etching {111} planes as the etch stop in an aqueous alkaline solution. In addition, the etched depth can be arbitrarily defined during the RIE step, thereby arbitrarily defining the thickness of the microstructures and the spacing between the microstructures and the silicon substrate.

[0049] It will be apparent to those skilled in the art that various modifications and variations can be made in the micromechanical system fabrication method using (111) single crystalline silicon of the present invention without deviating from the spirit or scope of the invention. Thus, it is intended that the present invention covers the modifications and variations of this invention provided they come within the scope of the appended claims and their equivalents.