摘要:
A MEMS device includes a mass system capable of undergoing oscillatory drive motion along a drive axis and oscillatory sense motion along a sense axis perpendicular to the drive axis. A quadrature correction unit includes a fixed electrode and a movable electrode coupled to the movable mass system, each being lengthwise oriented along the drive axis. The movable electrode is spaced apart from the fixed electrode by a gap having an initial width. At least one of the fixed and movable electrodes includes an extrusion region extending toward the other of the fixed and movable electrodes. The movable electrode undergoes oscillatory motion with the mass system such that the extrusion region is periodically spaced apart from the other of the fixed and movable electrodes by a gap exhibiting a second width that is less than the first width thereby enabling capacitance enhancement between the electrodes.
摘要:
This document discusses, among other things, a cap wafer and a via wafer configured to encapsulate a single proof-mass 3-axis gyroscope formed in an x-y plane of a device layer. The single proof-mass 3-axis gyroscope can include a main proof-mass section suspended about a single, central anchor, the main proof-mass section including a radial portion extending outward towards an edge of the 3-axis gyroscope sensor, a central suspension system configured to suspend the 3-axis gyroscope from the single, central anchor, and a drive electrode including a moving portion and a stationary portion, the moving portion coupled to the radial portion, wherein the drive electrode and the central suspension system are configured to oscillate the 3-axis gyroscope about a z-axis normal to the x-y plane at a drive frequency.
摘要:
This document discusses, among other things, a cap wafer and a via wafer configured to encapsulate a single proof-mass 3-axis gyroscope formed in an x-y plane of a device layer. The single proof-mass 3-axis gyroscope can include a main proof-mass section suspended about a single, central anchor, the main proof-mass section including a radial portion extending outward towards an edge of the 3-axis gyroscope sensor, a central suspension system configured to suspend the 3-axis gyroscope from the single, central anchor, and a drive electrode including a moving portion and a stationary portion, the moving portion coupled to the radial portion, wherein the drive electrode and the central suspension system are configured to oscillate the 3-axis gyroscope about a z-axis normal to the x-y plane at a drive frequency.
摘要:
An out-of-plane thermal buckle-beam microelectrical mechanical actuator is formed on a planar substrate of semiconductor material (e.g., silicon). The actuator includes first and second anchors secured to the substrate and multiple elongated thermal buckle beams that are secured between the anchors. The buckle beams are formed of semiconductor material, such as polysilicon. In one implementation, the buckling beams are coupled together by a pivot frame that includes a frame base secured to each buckle beam and at least one pivot arm that is coupled to the frame base at one end and includes a free end that pivots out-of-plane when the actuator is activated. A cyclic current source directs cyclic electrical current through the thermal buckle beams via the anchors to impart thermal expansion of the buckle beams and hence a cyclic buckling motion of them out of the plane (i.e., away from) the substrate. In one implementation, the actuator has a characteristic resonant deflection frequency range and the cyclic current is of a first frequency within the resonant deflection frequency range.
摘要:
The present invention easily achieves an accurate control structure for limiting displacement of a weight (310; 310B). An SOI substrate with a trilaminar structure including a silicon layer (10), a silicon oxide layer (20), and a silicon layer (30) is prepared, and slits (S1-S4) are opened by applying induced coupling plasma etching which can selectively remove only silicon from the upper side. Then, the same etching is applied from the lower side to form grooves (G1, G2), whereby the silicon layer (30) is separated into a weight (310; 310B) and a pedestal (330; 330B). Next, the structure is immersed in an etchant which can selectively remove only silicon oxide, whereby the vicinities of exposed portions of the silicon oxide layer (20) are removed to form joint layers. A glass substrate (400) is joined to the bottom surface of the pedestal (330; 330B). Piezo resistor elements (Rx1-Rx4, Ry1-Ry4, Rz1-Rz4) are formed on the upper surface of the silicon layer (100) to detect bending. The degree of freedom of upward displacements of the weight (310; 310B) is accurately set based on the thickness of the joint layer (200; 200B).
摘要:
The invention relates to a miniature kinetic energy harvester (1) for generating electrical energy, comprising: —a support (2), —a first element (3) having walls (32-35) surrounding at least one cavity (31), —at least one spring (4) mounted between the first element (3) and the support (2), the spring (4) being arranged so that the first element (3) may be brought into oscillation relative to the support (2) according to at least one direction (X) of oscillation, —a transducer (5) arranged between the first element (3) and the support (2) for converting oscillation of the first element (3) relative to the support (2) into an electrical signal, —at least one second element (7) housed within the cavity (31) and mounted to freely move within the cavity (31) relative to the first element (3) so as to impact the walls (32-35) of the cavity (31) when the harvester (1) is subjected to vibrations.
摘要:
This document discusses, among other things, a cap wafer and a via wafer configured to encapsulate a single proof-mass 3-axis gyroscope formed in an x-y plane of a device layer. The single proof-mass 3-axis gyroscope can include a main proof-mass section suspended about a single, central anchor, the main proof-mass section including a radial portion extending outward towards an edge of the 3-axis gyroscope sensor, a central suspension system configured to suspend the 3-axis gyroscope from the single, central anchor, and a drive electrode including a moving portion and a stationary portion, the moving portion coupled to the radial portion, wherein the drive electrode and the central suspension system are configured to oscillate the 3-axis gyroscope about a z-axis normal to the x-y plane at a drive frequency.
摘要:
This document discusses, among other things, a cap wafer and a via wafer configured to encapsulate a single proof-mass 3-axis gyroscope formed in an x-y plane of a device layer. The single proof-mass 3-axis gyroscope can include a main proof-mass section suspended about a single, central anchor, the main proof-mass section including a radial portion extending outward towards an edge of the 3-axis gyroscope sensor, a central suspension system configured to suspend the 3-axis gyroscope from the single, central anchor, and a drive electrode including a moving portion and a stationary portion, the moving portion coupled to the radial portion, wherein the drive electrode and the central suspension system are configured to oscillate the 3-axis gyroscope about a z-axis normal to the x-y plane at a drive frequency.
摘要:
A system and method are disclosed which constrain a microcomponent that is totally released from a substrate for handling of such totally released microcomponent. A preferred embodiment provides a system and method which constrain a totally released microcomponent to a base (e.g., another microcomponent or a substrate ). For example, a preferred embodiment provides constraining members that work to constrain a microcomponent to a substrate as such microcomponent is totally released from such substrate. Accordingly, such constraining members may aid in preserving the microcomponent with its substrate during the release of such microcomponent from its substrate during fabrication. Additionally, a preferred embodiment provides constraining members that are suitable for constraining a totally released microcomponent to a base for post-fabrication handling of the microcomponent. To further aid in post-fabrication handling of totally released microcomponents, a preferred embodiment may be implemented as a "pallet" having one or more microcomponents constrained thereto. Moreover, constraining members of a preferred embodiment enable the totally released microcomponent to be removed from such constraints when desired, but prevents the totally released microcomponent from inadvertently escaping such constraints. For instance, in one embodiment, the constraining members are implemented as moveable members that can be moved to unconstrain the totally released microcomponent from its base.
摘要:
This document discusses, among other things, a cap wafer and a via wafer configured to encapsulate a single proof-mass 3-axis gyroscope formed in an x-y plane of a device layer. The single proof-mass 3-axis gyroscope can include a main proof-mass section suspended about a single, central anchor, the main proof-mass section including a radial portion extending outward towards an edge of the 3-axis gyroscope sensor, a central suspension system configured to suspend the 3-axis gyroscope from the single, central anchor, and a drive electrode including a moving portion and a stationary portion, the moving portion coupled to the radial portion, wherein the drive electrode and the central suspension system are configured to oscillate the 3-axis gyroscope about a z-axis normal to the x-y plane at a drive frequency.