Rosemount Aerospace Limited

Carrier Corporation

Marcus Allen Childress

David Patrick Potasek

John Carl Christenson

Jim Golden

Brian Brent Naslund

Benjamin John Langemo

Nghia T Dinh

James C Golden

Dosi Dosev

Peter Mann-Lai Chong

A microelectromechanical systems (MEMS) device includes a MEMS device body connected to a first mooring portion and a second mooring portion. The MEMS device body further includes a first cantilever and a second cantilever and connected by a spring. The spring is in operable communication with the first cantilever and the second cantilever.

Piezoelectric MEMS device with cantilever structures

A method of testing sensors includes providing a test sheet that includes a plurality of sensor assemblies, a plurality of test pads, and traces extending from the sensor assemblies to the plurality of test pads. A sensor is positioned on each sensor assembly. Each sensor is connected to the sensor assembly with wire bonds. An enclosure is formed over the plurality of sensor assemblies. An electrical signal is detected from each of the plurality of sensor assemblies at the test pads.

Apparatus and method for packaging, handling or testing of sensors

A sensor is configured to attach to a main body and includes a sensor body, a transducer, a transmitter, and a power source. The sensor body is configured to provide a smooth transition with a surface of the main body. The transducer is positioned within the sensor body and is configured to provide a sensed output. The transmitter is positioned within the sensor body and is configured to transmit the sensed output. The power source is positioned within the sensor body and is configured to provide electrical power to the transducer and the transmitter.

Low profile pressure sensor on the body of a vehicle

A microelectromechanical systems die including a thermally conductive substrate including an outer surface, a plurality of low mass sensing structures disposed within the thermally conductive substrate to form a plurality of inter-structure spaces therebetween, each of the plurality of low mass sensing structures include a sensing structure proximal top surface, a sensing structure distal top surface, and a sensing structure width dimension.

MEMS die with sensing structures

A microelectromechanical systems die including a thermally conductive substrate, at least one insulator film disposed on the thermally conductive substrate, a sensor material disposed on the at least one insulator film, and a heater circumferentially disposed around the sensor material.

Gas detector with a thermally uniform MEMS die

Spring set configurations that include an advantageous combination of spring geometries are disclosed. Spring elements having curved and straight sections, orientation of spring element anchor points with respect to the common radius, orientation of spring element segments with respect to a specific axis, balance of the length of spring elements about the common radius, and mass balance about the common radius can be used to mitigate unwanted out of plane motion. The spring set provides planar motion while reducing undesired out of plane motion making MEMS devices substantially insensitive to the process-induced etch angle variations of the spring elements. The spring set can be used in a MEMS gyro device which maintains the desired resonant modes and consistently low quadrature error even with process variations in manufacturing causing undesirable etch angles.

MEMS gyros with quadrature reducing springs

A microstructure device has a microstructure (e.g., a circuit card assembly, a printed circuit board, etc.) defining a sensitive axis and one or more isolators configured and adapted to be compliant along the sensitive axis and to be rigid along one or more other axes.

Vibration isolated MEMS structures and methods of manufacture

A microstructure device package includes a package housing configured and adapted to house a microstructure device. A bracket is housed in the package housing. The bracket includes a bracket base with a first bracket arm and a second bracket arm each extending from the bracket base. A channel is defined between the first and second bracket arms. The first bracket aim defines a first mounting surface facing inward with respect to the channel. The second bracket aim defines a second mounting surface facing outward with respect to the channel. The second mounting surface of the bracket is mounted to the package housing. A microstructure device is mounted to the first mounting surface in the channel. The bracket is configured and adapted to isolate the microstructure device from packaging stress imparted from the package housing on the second mounting surface of the bracket.

Growing community of inventors

Farmington, MN, United States of America

Marcus Allen Childress