Nxp Usa, Inc.

Jun Tang

Andrew C McNeil

Aaron A Geisberger

Chad S Dawson

Jerome Romain Enjalbert

Margaret Leslie Kniffin

Joel Cameron Beckwith

Kajal Rahimian Kordestani

A microelectromechanical systems (MEMS) accelerometer comprises a compliant spring structure with a first beam, a second beam, and a rigid structure. One end of the first beam and one end of the second beam are coupled to the rigid structure and a proof mass is coupled to another end of the second beam. Further, a spring anchor is coupled to another end of the first beam. In response to the proof mass moving, an extension coupled to the rigid structure moves in an opposite direction to motion of the proof mass to contact the proof mass and stop the movement of the proof mass.

Accelerometer having an over travel stop with a stop gap less than a minimum etch size

A sensor system includes a transducer for sensing a physical stimulus along at least two orthogonal axes and an excitation circuit. The transducer includes a movable mass configured to react to the physical stimulus and multiple differential electrode pairs of electrodes. Each of the electrode pairs is configured to detect displacement of the movable mass along one of the orthogonal axes. The excitation circuit is connectable to the electrodes in various electrode connection configurations, with different polarity schemes, that enable excitation and sampling of each of the orthogonal axes during every sensing period. For each sensing period, a composite output signal is produced that includes the combined information sensed along each of the orthogonal axes. The individual sense signals for each orthogonal axis may be extracted from the composite output signals.

Inertial sensor sampling with combined sense axes

An inertial sensor includes a movable mass spaced apart from a surface of the substrate. The movable mass is adapted for motion about a rotational axis positioned between first and second ends of the movable mass in response to a first force imposed upon the movable mass in a first direction that is perpendicular to the surface of the substrate. The inertial sensor further includes a damping system configured to limit motion of the movable mass in a second direction perpendicular to the first direction. The damping system includes a first damping structure coupled to the movable mass, a second damping structure adjacent to the first damping structure, the first and second damping structures being spaced apart from the surface of the substrate, and a spring structure interconnected between the movable mass and the second damping structure.

Inertial sensor with integrated damping structures

A single axis inertial sensor includes a proof mass spaced apart from a surface of a substrate. The proof mass has first, second, third, and fourth sections. The third section diagonally opposes the first section relative to a center point of the proof mass and the fourth section diagonally opposes the second section relative to the center point. A first mass of the first and third sections is greater than a second mass of the second and fourth sections. A first lever structure is connected to the first and second sections, a second lever structure is connected to the second and third sections, a third lever structure is connected to the third and fourth sections, and a fourth lever structure is connected to the fourth and first sections. The lever structures enable translational motion of the proof mass in response to Z-axis linear acceleration forces imposed on the sensor.

Single axis inertial sensor with suppressed parasitic modes

An inertial sensor includes a proof mass spaced apart from a surface of a substrate. The proof mass has a first section and a second section, where the first section has a first mass that is greater than a second mass of the second section. An anchor is coupled to the surface of the substrate and a spring system is interconnected between the anchor and the first and second sections of the proof mass. The spring system enables translational motion of the first and second sections of the proof mass in response to linear acceleration forces imposed on the inertial sensor in any of three orthogonal directions.

Three-axis inertial sensor for detecting linear acceleration forces

An inertial sensor includes first and second movable elements suspended from a substrate and interconnected by a beam. The second movable element is positioned laterally adjacent to the first movable element, and each of the movable elements has a mass that is asymmetric relative to a rotational axis. A first spring system couples the first movable element to the substrate and a second spring system couples the second movable element to the substrate. The spring systems and the beam enable the movable elements to move together in response to force imposed upon the movable elements. In particular, the first and second movable elements can undergo in-plane torsion motion in response to force, such as acceleration, imposed in a sense direction. Additionally, damping structures may be integrated into the first and second movable elements to effectively increase a damping ratio of the device resulting from the in-plane torsion motion.

Multi-axis inertial sensor with dual mass and integrated damping structure

A MEMS device comprises a substrate, a proof mass spaced apart from a surface of the substrate, and an over-travel stop structure. The over-travel stop structure includes a lateral stop structure and a cap coupled to the lateral stop structure. The MEMS device is fabricated to include relatively small gap sections and relatively large gap regions separating the lateral stop structure from the proof mass. The larger gap regions are covered by the cap and the smaller gap sections are exposed from the gap. During fabrication, removal of particles from the smaller gap sections is facilitated by their exposure from the cap and removal of particles from the larger gap regions underlying the cap is facilitated by their larger size. The lateral stop structure may be cross-shaped to limit deflection of the proof mass along two in-plane axes. The cap limits deflection of the proof mass along an out-of-plane axis.

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Gilbert, AZ, United States of America

Jun Tang