Technical Field: This disclosure relates to microelectromechanical systems (MEMS) mirror arrays and methods of manufacturing the MEMS mirror arrays that reduces and/or constrains out-of-plane displacements caused by shock.
Background: A MEMS (microelectromechanical systems) device is a micro-sized mechanical structure having electrical circuitry and is fabricated using conventional integrated circuit (IC) fabrication methods. One type of MEMS device is a microscopic gimbaled mirror device. A gimbaled mirror device includes a mirror component, which is suspended off a substrate, and is able to pivot about a gimbal due to electrostatic actuation. Electrostatic actuation creates an electric field that causes the mirror component to pivot. By allowing the mirror component to pivot, the mirror component is capable of having an angular range of motion in which the mirror component can redirect light beams to varying positions.
An optical switch is a switching device that couples light beams from an input fiber to an output fiber. Typically, the light beams from an input fiber are collimated and directed toward a desired location such as an output fiber. A movable mirror (e.g., a gimbaled mirror) in a switch mirror array redirects the light beams to desired locations.
Inside the optical switch, the mirrors in the array may need to rotate 10 — 20 degrees or more to direct the light beams to the desired locations. The mirrors need sufficient space above and below to allow these rotations. However, having this much space above and below the mirrors allows the mirrors to also move linearly in the vertical (out-of-plane) direction. The mirror flexures are designed to prevent this undesired linear, out-of-plane motion under normal operating conditions. When the optical switch is being handled during shipment or installation, for example, the optical switch could be dropped or impacted with sufficient force to cause the mirrors to undergo large out-of-plane deflections. This may damage mirrors in the switch array resulting in them being inoperable.
What is needed are MEMS mirror arrays and methods of manufacturing the MEMS mirror arrays that reduces and/or constrains out-of-plane displacements caused by shock.
Disclosed are MEMS mirror arrays and methods of manufacturing the MEMS arrays that constrains out-of-plane displacement caused by shock which reduces the likelihood of damage. Also disclosed are MEMS mirror arrays and methods of manufacturing the arrays that constrains out-of-plane displacements while still allowing large angular rotations needed for optical switching.
One aspect of the disclosure provides a mirror array. The mirror array includes a lid, a base, and a movable mirror between the lid and the base. The movable mirror includes a stationary frame including a cavity, a movable frame in the cavity, and a central stage in the cavity. The mirror array also includes a first protrusion on the base. The first protrusion overlaps with the central stage in a first direction.
Implementations of the disclosure may include one or more of the following optional features. The central stage can include a bottom portion facing the first protrusion. Additionally, the first protrusion can be spaced apart from the bottom portion of the central stage by a predetermined distance. The predetermined distance between the first protrusion and the bottom portion of the central stage is between 3 μm and 15 μm.
Optionally, the mirror array further may include a second protrusion on the lid and a third protrusion on the lid. The second protrusion and the third protrusion can be configured to extend towards the base. The mirror array can also include a first stationary frame flexure and a second stationary frame flexure. The first stationary frame flexure and the second stationary frame flexure suspend the movable frame from the stationary frame. The second protrusion can be configured to overlap with the first stationary frame flexure in the first direction, and the third protrusion can be also configured to overlap with the second stationary frame flexure in the first direction. The second protrusion can also be positioned apart from the first stationary frame flexure by a predetermined distance. The predetermined distance between the second protrusion and the first stationary frame flexure is between 3 μm and 15 μm. The third protrusion can also be positioned apart from the second stationary frame flexure by a predetermined distance. The predetermined distance between the third protrusion and the secondary stationary frame flexure is also between 3 μm and 15 μm. The second protrusion and the third protrusion can be positioned so that the second protrusion and the third protrusion are non-overlapped with the central stage in the first direction.
The mirror array is further configurable to include a fourth protrusion on the base and a fifth protrusion on the base. The first protrusion can be positioned between the fourth protrusion and the fifth protrusion. Additionally, the fourth protrusion can be configured to support a first support member, while the fifth protrusion is configured to support a second support member. The central stage can also include a bottom portion extending towards the first protrusion, wherein the bottom portion is positioned between the first support member and the second support member.
Another aspect of the disclosure provides a mirror array. The mirror array includes a movable mirror and a lid wafer covering the movable mirror. The movable mirror also includes a stationary frame including a cavity, a movable frame in the cavity, and a central stage in the cavity. The movable frame can be suspended from the stationary frame by a first stationary frame flexure and a second stationary frame flexure. The mirror array can also include a first protrusion on the lid wafer. The first protrusion is extended towards the movable mirror.
Implementations of the disclosure may include one or more of the following optional features. The first protrusion can overlap with the first stationary frame flexure in a first direction. A gap can be provided between the first protrusion and the first stationary frame flexure that is between 3 μm and 15 μm. The mirror array can further include a second protrusion on the lid wafer. The second protrusion can be positioned to overlap with the second stationary frame flexure in the first direction. A gap can be provided between the second protrusion and the second stationary frame flexure that is between 3 μm and 15 μm.
The mirror array is further configurable to include a base wafer and a third protrusion on the base wafer. The third protrusion can also overlap with the central stage in the first direction. The third protrusion can also be spaced apart from a bottom portion of the central stage by a predetermined distance, such as 3 μm and 15 μm.
Both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the disclosed embodiments, as claimed.
All publications, patents, and patent applications mentioned in this specification are herein incorporated by reference to the same extent as if each individual publication, patent, or patent application was specifically and individually indicated to be incorporated by reference.
U.S. Pat. No. 5,501,893 A issued Mar. 26, 1996 to Laermer et al.;
U.S. Pat. No. 5,635,739 A issued Jun. 3, 1997 to Grieff et al.;
U.S. Pat. No. 5,696,619 A issued Dec. 9, 1997 to Knipe et al.;
U.S Pat. No. 6,430,333 B1 issued Aug. 6, 2002 to Little et al.;
U.S Pat. No. 6,664,706 B1 issued Dec. 16, 2003 to Hung et al.;
U.S Pat. No. 6,914,711B2 issued Jul. 5, 2005 to Novotny et al.;
U.S. Pat. No. 7,092,141 B2 issued Aug. 15, 2006 to Kim et al.;
U.S. Pat. No. 7,261,826 B2 issued Aug. 28, 2007 to Adams et al.;
U.S. Pat. No. 7,330,297 B2 issued Feb. 12, 2008 to Noh et al. and
BEHIN, et al., Magnetically Actuated Micromirrors for FiberOptic Switching, 1998, Dec. 31.
The novel features of the invention are set forth with particularity in the appended claims. A better understanding of the features and advantages of the present invention will be obtained by reference to the following detailed description that sets forth illustrative embodiments, in which the principles of the invention are utilized, and the accompanying drawings of which:
A second blade 116 is coupled on end of stage 102 opposite the location of the first blade 112, with a pair of second flanking blades 118, 118′ coupled to moveable frame 104 on opposite ends of second blade 116. Second blade 116 moves relative to second flanking blades 118, 118′. In order to provide the desired motion of stage 102 and to resist unwanted rotations, actuation voltages are applied concurrently with respect to first blade 112 and second blade 116. For example, the range of motion for the stage 102 is between +15 degrees and −15 degrees, approximately. When the potential difference is applied between the second blade 116 and one of second flanking blades 118, 118′, an attraction is generated between the blades resulting in the rotation of stage 102 in a manner similar to that discussed above with respect to the first blade 112. The use of actuation mechanisms in tandem on each end of stage 102 minimizes or reduces undesired twisting of the stage 102 to provide for more uniform rotation.
A similar actuation mechanism structure may be used for rotation of moveable frame 104. For example, a first side blade 122 is coupled to moveable frame 104 and first side flanking blades 124, 124′are coupled to stationary frame 140 (stationary frame 214 in
Moveable frame 104 is pivotally coupled to the stationary frame 140 such that first side blade 122 is configured to move relative to first side flanking blades 124, 124′. When a potential difference is applied between the first side blade 122 and one of the first side flanking blades 124, 124′, an attraction is generated between the blades causing moveable frame 104 to pivot in a manner similar to that discussed above in relation to stage 102. As shown, the moveable frame 104 is suspended from the stationary frame 140 by mirror flexure 152 (e.g., spring, first stationary frame flexure) and a second mirror flexure 154 (e.g., spring, second stationary frame flexure).
Second side blade 126 is coupled on the opposite end of moveable frame 104, with second side flanking blades 128, 128′ coupled to stationary frame 140 on opposite ends of second side blade 126. Second side blade 126 moves relative to second side flanking blades 128, 128′. When the potential difference is applied between second side blade 126 and one of second side flanking blades 128, 128′, an attraction is generated between the blades facilitating the rotation of moveable frame 104. The use of actuation mechanisms in tandem on each end of moveable frame 104 minimizes or reduces undesired twisting of the frame to provide for more uniform rotation. For example, the range of motion for the movable frame 104 is between +20 degrees and −20 degrees, approximately.
Alternatively, a stage 102 or moveable frame 104 may only have an actuation mechanism structure on a single end. For another embodiment, actuator 100 may have other actuation mechanism structures without departing from the scope of the disclosure.
For one embodiment, a plurality of elongated members 130 can be provided (e.g., elongated member 130) which are coupled to the undersurface of stage 102 to stiffen the stage 102 and minimize or reduce top surface distortions. In addition, the elongated members 130 on stage 102 may be used to remove etch depth variations across the device. Elongated member 130 may be constructed similar to that of blades discussed herein.
For one embodiment, actuator 100 may be fabricated on a wafer level using semiconductor fabrication techniques, as discussed below. For such an embodiment, stationary frame 140 may be formed from a substrate, for example, constructed from silicon. Where all blades are directly driven by different control voltages, actuator 100 may use four voltages, plus a ground. With this arrangement, the number of conductive paths on a substrate quickly becomes very large as multiple actuators are combined to form an array. The low voltages required by the blade actuators discussed herein may allow for control circuitry to be fabricated into the substrate so that only control signals need be routed, rather than separate lines for each blade. This results in a significant reduction in lead count. Lower voltages may also reduce the necessity for spacing between leads to avoid arcing and cross-talk.
The trenches 210 are filled with a dielectric material, which for one embodiment is silicon dioxide. The filled trenches 210 provide the electrical isolation between blades after the mirror is released. A dielectric layer 203 also remains on the surface of the device wafer 220′ and is planarized after the fill process to ease subsequent lithographic patterning and eliminate surface discontinuities. Structure release is accomplished at the upper surface (topside) of the device wafer 220′ using dry etching, which punctures through a plurality of trenches 226 to suspend the movable elements of the mirror 213 and the frame 227. Support webbing 234 (also referred as support member) is also provided. As shown, the bottom portion of the central stage 220 is between the support webbings 234. A base wafer 212 is bonded to the device wafer 220′ to protect the blades after release. A hermetic seal 204 can surround the entire mirror array. The hermetic seal 204 can be formed by the frit material between the base wafer 212 and the device wafer 220′.
A coating of photoresist material 720 (also referred as photoresist layer) is deposited on the hard mask layer 702 and the base wafer 700 as shown in
As shown in
As shown, the mirror array 800 also includes a second protrusion (mechanical stop 1012) on the lid (lid wafer 802), and a third protrusion (mechanical stop 1012) on the lid (lid wafer 802). The second protrusion (mechanical stop 1012) and the third protrusion (mechanical stop 1012) extend towards the base (base wafer 700). As shown, the mirror array 800 also includes a first stationary frame flexure (mirror's flexure 152) and a second stationary frame flexure (mirror's flexure 154). The first stationary frame flexure (mirror's flexure 152) and the second stationary frame flexure (mirror's flexure 154) suspend the movable frame 227 from the stationary frame 214. As shown, the second protrusion (mechanical stop 1012) overlaps with the first stationary frame flexure (mirror's flexure 152) in the first direction, and the third protrusion (mechanical stop 1012) overlaps with the second stationary frame flexure (mirror's flexure 154) in the first direction. As shown, the second protrusion (mechanical stop 1012) is apart from the first stationary frame flexure (mirror's flexure 152) by a predetermined distance (e.g., distance between 3 μm and 15 μm). As shown, the third protrusion (mechanical stop 1012) is apart from the second stationary frame flexure (mirror's flexure 154) by a predetermined distance (e.g., distance between 3 μm and 15 μm). As shown, the second protrusion (mechanical stop 1012) and the third protrusion (mechanical stop 1012) are non-overlapped with the central stage 220 in the first direction.
As shown, the mirror array 800 also includes a fourth protrusion (support anchor 430) and a fifth protrusion (support anchor 430) on the base (base wafer 700). As shown, the fourth protrusion (support anchor 430) and the fifth protrusion (support anchor 430) are formed from the base (base wafer 700). However, the fourth protrusion (support anchor 430) and the fifth protrusion (support anchor 430) may be formed from a (separate) layer on the base (base wafer 700). As shown, the first protrusion (support anchor 430) is between the fourth protrusion (support anchor 430) and the fifth protrusion (support anchor 430). As shown, the fourth protrusion (support anchor 430) is configured to support a first support member (support webbing 234), and the fifth protrusion (support anchor 430) is configured to support a second support member (support webbing 234). As shown, the central stage 220 includes a bottom portion extending towards the first protrusion (mechanical stop 502). As shown, the bottom portion of the central stage 220 is between the first support member (support webbing 234) and the second support member (support webbing 234).
As shown in
While preferred embodiments of the present invention have been shown and described herein, it will be obvious to those skilled in the art that such embodiments are provided by way of example only. Numerous variations, changes, and substitutions will now occur to those skilled in the art without departing from the invention. It should be understood that various alternatives to the embodiments of the invention described herein may be employed in practicing the invention. It is intended that the claims define the scope of the invention and that methods and structures within the scope of these claims and their equivalents be covered thereby.
This application claims the benefit of U.S. Provisional Application No. 63/263,373, filed Nov. 1, 2021, entitled VERTICAL MECHANICAL STOPS TO PREVENT LARGE OUT-OF-PLANE DISPLACEMENTS OF A MICRO-MIRROR which application is incorporated herein in its entirety by reference.
Number | Date | Country | |
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63263373 | Nov 2021 | US |