A micromechanical apparatus includes a substrate, a movable element disposed in a reference plane in an undeflected state, a transmission structure having a first transmission side coupled to the substrate, and a second transmission side coupled to the movable element, and an actuator configured to provide a force along a force direction parallel to the reference plane and apply the same to the first transmission side. The transmission structure is configured to transfer the force along the force direction to a movement of the movable element out of the reference plane.

A micro-electrical-mechanical system (MEMS) assembly includes a stationary stage, a rigid stage, at least one flexure configured to slidably couple the stationary stage and the rigid stage, at least one flexible electrode coupled and essentially orthogonal to one of the stationary stage and the rigid stage, and at least one rigid electrode coupled and essentially orthogonal to the other of the stationary stage and the rigid stage.

A micro-electrical-mechanical system (MEMS) cantilever assembly includes an intermediary cantilever portion, a main cantilever arm configured to couple a moveable portion of a micro-electrical-mechanical system (MEMS) and the intermediary cantilever portion, and a plurality of intermediary links configured to couple the intermediary cantilever portion to a portion of the micro-electrical-mechanical system (MEMS).

A micro-electrical-mechanical system (MEMS) assembly includes a micro-electrical-mechanical system (MEMS) actuator configured to be coupled, on a lower surface, to a printed circuit board, an image sensor assembly coupled to an upper surface of the micro-electrical-mechanical system (MEMS) actuator, and a holder assembly coupled to and positioned with respect to the micro-electrical-mechanical system (MEMS) actuator.

A method of manufacturing a micro-electrical-mechanical system (MEMS) assembly includes mounting a micro-electrical-mechanical system (MEMS) actuator to a metal plate. An image sensor assembly is mounted to the micro-electrical-mechanical system (MEMS) actuator. The image sensor assembly is electrically coupled to the micro-electrical-mechanical system (MEMS) actuator, thus forming a micro-electrical-mechanical system (MEMS) subassembly.

A micro-electrical-mechanical system (MEMS) actuator includes a first set of actuation fingers, a second set of actuation fingers, and a first spanning structure configured to couple at least two fingers of the first set of actuation fingers while spanning at least one finger of the second set of actuation fingers.

INVENTION #7

A micro-electrical-mechanical system (MEMS) device includes one or more slidable connection assemblies for releasably coupling the micro-electrical-mechanical system (MEMS) device to a wafer from which the micro-electrical-mechanical system (MEMS) device was made.

A micro-electrical-mechanical system (MEMS) actuator includes: a MEMS actuation core, and a multi-piece MEMS electrical connector assembly electrically coupled to the MEMS actuation core and configured to be electrically coupled to a printed circuit board, wherein the multi-piece MEMS electrical connector includes: a plurality of subcomponents, and a plurality of coupling assemblies configured to couple the plurality of subcomponents together.

Methods for fabricating microelectronic packages and microelectronic packages having split gyroscope structures are provided. In one embodiment, the microelectronic package includes a first Microelectromechanical Systems (MEMS) die having a first MEMS gyroscope structure thereon. The microelectronic package further includes a second MEMS die, which has a second MEMS gyroscope structure thereon and which is positioned in a stacked relationship with the first MEMS die. The first and second MEMS gyroscope structures overlap as taken along a first axis orthogonal to a principal axis of the first MEMS die.

Systems and methods are described herein for detecting and measuring inertial parameters, such as acceleration. In particular, the systems and methods relate to vibratory inertial sensors implementing time-domain sensing techniques. Within a composite mass sensor system, a sense mass may oscillate at a frequency different from its actuation frequency, allowing flexibility when integrating the sensor into drive systems without sacrificing sensitivity.