Rosemount Aerospace Limited

Goodrich Corporation

Other

United Technologies Corporation

Rohr, Inc.

Odd Harald Steen Eriksen

Shuwen Guo

Kimiko Childress

Christopher Sanden

Chuang-Chia Lin

Alexander Spivak

Anita Fink

Lawrence Joseph Stang

David Patrick Potasek

Saeed Fahimi

Weibin Zhang

Charles Little

Robert Stuelke

Alexander Grichener

Charles Robin Hood

Felix Goldenberg

Brian Snyder

Jon A Cox

Yosief Abraha

Joe Mctighe

Mark Jefferson Kranz

Dave Lopes

Kimiko J Childress

Christopher M Sanden

Alan Leingang

Dennis Roertson

A differential pressure sensor includes a body having a first end, a second end, and a wall. The first end and second end include isolator diaphragms connected to external first and second process fluid inlets. A MEMS pressure sensor including a pressure sensing diaphragm inside the cylinder has first and second sides coupled to the first and second isolator diaphragms by first and second fill fluid volumes. Sensor elements on the diaphragm are configured to provide, via associated sensor circuitry, an indication of deflection due to pressure differences between the first and second fill volumes. Electrical and fill fluid connections to the differential pressure sensor are made through radial connections in the wall of the body.

Compact or miniature high temperature differential pressure sensor capsule

A method for forming a pressure sensor includes forming a base of a sapphire material, the base including a cavity formed therein; forming a sapphire membrane on top of the base and over the cavity; forming a lower electrode on top of the membrane; forming a piezoelectric material layer on an upper surface of the lower electrode, the piezoelectric material layer being formed of aluminum nitride (AIN); and forming at least one upper electrode on an upper surface of the piezoelectric material layer.

High temperature flexural mode piezoelectric dynamic pressure sensor

A pressure sensor assembly includes a pressure sensor having a pressure sensing transducer connected to a plurality of electrode pins via a plurality of electrode pads disposed on the transducer, an inner casing configured to hold the pressure sensing transducer including a plurality of inner casing electrode pin channels having the electrode pins disposed therein. The pressure sensor further includes an outer casing holding the inner casing therein having a capsule header with a plurality of capsule header electrode pin channels defined therein which can include a ceramic seal disposed therein such that the capsule header electrode pin channels engage the electrode pins in an insulating sealed relationship. The outer casing further includes an isolator plate including an isolator plate fluid port defined therein and a pressure isolator disposed on the isolator plate and configured to deflect in response to a change in ambient pressure. The pressure sensor includes a pressure transmitting fluid disposed in the fluid volume.

High temperature pressure sensor

A sensor for monitoring loads in a landing gear torque linkage includes a main pin having an axial interior bore defined therein. The main pin is configured and adapted to engage a torque link to a strut lug of a landing gear strut. A core pin is mounted axially within an interior bore of the main pin and is spaced radially inwardly from the interior bore for relative displacement with respect to the main pin. A capacitor is included having an inner capacitor plate mounted to the core pin. An outer capacitor plate is mounted to the main pin. Relative displacement of the core pin and the main pin due to loads acting on the torque link and strut lug results in relative displacement of the inner and outer capacitor plates. Signals can thereby be produced indicative of the loads acting on the torque link.

Capacitive sensors for monitoring loads

A capacitive strain sensor for sensing strain of a structure. The sensor includes a first section attached to the structure at a first location and a second section attached to the structure at a second location. The first section includes a capacitor plate electrically isolated from the structure and the second section includes two electrically isolated capacitive plates, both of the plates being electrically isolated from the structure. A flexible connector connects the first section to the second section. The capacitor plate of the first section is separated from the two capacitive plates of the second section by at least one capacitive gap. When strain is experienced by the structure, a change occurs in the capacitive gap due to relative motion between the first and second sections.

Sensor for measuring large mechanical strains with fine adjustment device

A capacitive strain sensor for sensing strain of a structure. The sensor includes a first section attached to the structure at a first location and a second section attached to the structure at a second location. The first section includes a capacitor plate electrically isolated from the structure and the second section includes two electrically isolated capacitive plates, both of the plates being electrically isolated from the structure. A flexible connector connects the first section to the second section. The capacitor plate of the first section is separated from the two capacitive plates of the second section by at least one capacitive gap. When strain is experienced by the structure, a change occurs in the capacitive gap due to relative motion between the first and second sections. The first section includes a core and the second section includes a ring that receives the core.

Sensor for measuring large mechanical strains in shear or lateral translation

A method for forming a transducer including the step of providing a semiconductor-on-insulator wafer including first and second semiconductor layers separated by an electrically insulating layer, wherein the first layer is formed or provided by hydrogen ion delamination of a starting wafer. The method further includes doping the first layer to form a piezoresistive film and etching the piezoresistive film to form at least one piezoresistor. The method also includes depositing or growing a metallization layer on the semiconductor-on-insulator wafer, the metallization layer including an electrical connection portion that is located on or is electrically coupled to the piezoresistor. The method includes removing at least part of the second semiconductor layer to form a diaphragm, with the at least part of the piezoresistor being located on the diaphragm, and joining the wafer to a package by melting a high temperature braze material or a glass frit material.

Method for forming a transducer

A strain sensor device for measuring loads on aircraft landing gear. This is done by measuring strains in the lower end of the strut, by which we infer the loading in the entire landing gear structure. These strains can be very large (as high as 10,000 microstrain) and can be imposed in numerous random directions and levels. The present invention includes a removable sensor assembly. An electromechanical means is presented that can accommodate large strains, be firmly attached to the strut, and provide good accuracy and resolution.

Systems and methods for mounting landing gear strain sensors

A system for monitoring landing gear position. An example rotation position sensor includes a hub mount that locks within a shaft of a joint, a first sensor attached to the hub mount, and a second sensor attached to the rotatably attached part that does not rotate. The hub mount includes a nut that has a partially tapered surface and a threaded cavity. The nut is secured within the shaft. The hub mount also includes a mounting unit that has a partially tapered surface that is in opposition to the partially tapered surface of the nut. A fastener secures the hub mount to the nut. In one example, the first sensor includes a magnetometer and the second sensor includes magnet(s). In another example, the first sensor includes inductor sensor(s) and the second sensor includes device(s) that causes a change in an inductance value of the inductor sensor(s) as the joint rotates.

Systems and methods for measuring angular motion

An inertial measurement system having a triangular cupola shaped base structure with three mutually orthogonal sides and a bottom surface surrounding a hollow core. The bottom surface includes an aperture providing access to the hollow core. An inertial module is mounted on each of the sides and includes a gyroscopic rotational rate sensor and a linear accelerometer connected to a circuit board. The inertial measurement system also includes a motherboard and a plurality of metallization elements. The metallization elements extend from the bottom surface to the sides of the base structure and conductively connect the inertial module to the motherboard. The inertial measurement system may also include a non-conductive adhesive underfill positioned between the inertial module and the base structure.

Integrated inertial measurement system and methods of constructing the same

A transducer for use in a harsh environment including a substrate and a transducer die directly coupled to the substrate by a bond frame positioned between the substrate and the transducer die. The transducer die includes a transducer element which provides an output signal related to a physical characteristic to be measured, or which receives an input signal and responsively provides a physical output. The transducer further includes a connecting component electrically coupled to the transducer element at a connection location that is fluidly isolated from the transducer element or the surrounding environment by the bond frame. The bond frame is made of materials and the connecting component is electrically coupled to the transducer element by the same materials of the bond frame, and the connecting component is electrically isolated from the bond frame.

Transducer with fluidly isolated connection

A harsh environment transducer including a substrate having a first surface and a second surface, wherein the second surface is in communication with the environment. The transducer includes a device layer sensor means located on the substrate for measuring a parameter associated with the environment. The sensor means including a single crystal semiconductor material having a thickness of less than about 0.5 microns. The transducer further includes an output contact located on the substrate and in electrical communication with the sensor means. The transducer includes a package having an internal package space and a port for communication with the environment. The package receives the substrate in the internal package space such that the first surface of the substrate is substantially isolated from the environment and the second surface of the substrate is substantially exposed to the environment through the port. The transducer further includes a connecting component coupled to the package and a wire electrically connecting the connecting component and the output contact such that an output of the sensor means can be communicated. An external surface of the wire is substantially platinum, and an external surface of at least one of the output contact and the connecting component is substantially platinum.

High temperature resistant solid state pressure sensor

A Coriolis effect device includes a housing defining an interior chamber having a central axis, an inlet, an outlet, a leading disc and a trailing disc. Each disc is supported for oscillatory movement within the interior chamber of the housing. The leading disc defines a leading flow path in fluid communication with the inlet and interior chamber, wherein a portion of the leading flow path extends radially with respect to the central axis. The trailing disc is axially spaced from the leading disc. The trailing disc defines a trailing flow path in fluid communication with the interior chamber and the outlet, wherein a portion of the trailing flow path extends radially with respect to the central axis. A phase difference between leading and trailing oscillating signals picked up from the disc movement can be used to determine a mass flow rate of fluid passing from the inlet to the outlet.

Coriolis effect mass flow meter and gyroscope

A method for forming a transducer including the step of providing a semiconductor-on-insulator wafer including first and second semiconductor layers separated by an electrically insulating layer. The method further includes depositing or growing a piezoelectric film or piezoresistive film on the wafer, depositing or growing an electrically conductive material on the piezoelectric or piezoresistive film to form at least one electrode, and depositing or growing a bonding layer including an electrical connection portion that is located on or is electrically coupled to the electrode. The method further includes the step of providing a ceramic substrate having a bonding layer located thereon, the bonding layer including an electrical connection portion and being patterned in a manner to generally match the bonding layer of the semiconductor-on-insulator wafer. The method also includes causing the bonding layer of the semiconductor-on-insulator wafer and the bonding layer of the substrate to bond together to thereby mechanically and electrically couple the semiconductor-on-insulator wafer and the substrate to form the transducer, wherein the electrical connection portions of the bonding layers of the semiconductor-on-insulator wafer and the substrate are fluidly isolated from the surrounding environment by the bonding layers.

Method for making a transducer

A method for bonding two components together including the steps of providing a first component, providing a second component, and locating a first eutectic bonding material between the first and second component. The first eutectic bonding material includes at least one of germanium, tin, or silicon. The method further includes the step of locating a second eutectic bonding material between the first and second component and adjacent to the first eutectic bonding material. The second eutectic bonding material includes gold. The method further includes the step of heating the first and second eutectic bonding materials to a temperature above a eutectic temperature of an alloy of the first and second eutectic bonding materials to allow a hypoeutectic alloy to form out of the first and second eutectic bonding materials. The method includes the further step of cooling the hypoeutectic alloy to form a solid solution alloy bonding the first and second components together.

Growing community of inventors

Minneapolis, MN, United States of America

Odd Harald Steen Eriksen