Rosemount Aerospace Limited

Goodrich Corporation

Christopher Sanden

Odd Harald Steen Eriksen

Chuang-Chia Lin

Alexander Spivak

Greg Allen Seidel

Scott Darrell Isebrand

Cuong Tho Huynh

James Joseph Mctighe

Alexander Grichener

Felix Goldenberg

Brian Snyder

Alan F Leingang

Odd Harald Steep Eriksen

Harald Eriksen

Dennis Robertson

Joe Mctighe

Dave Lopes

Odd Harald Eriksen

A probe head for an air data probe includes a ceramic body and a heater embedded within the ceramic body.

Ceramic probe head for an air data probe with and embedded heater

A pressure sensor includes a MEMS pressure transducer with a pressure sensing diaphragm and sensor elements, an isolator diaphragm spaced apart from the pressure sensing diaphragm, and a ceramic header body. The ceramic header body has an electrical conductor and transducer aperture with the MEMS pressure transducer supported therein. The isolator diaphragm is coupled to the to the MEMS pressure transducer by a fluid and is sealably fixed to the ceramic body. The ceramic header body bounds the fluid and the electrical conductor electrically connects the MEMS pressure transducer with the external environment. Differential pressure sensors and methods of making pressure sensors are also described.

Differential MEMS pressure sensors with a ceramic header body and methods of making differential MEMS pressure sensors

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

Health and usage monitoring systems for aircraft hoist systems are described herein. In some embodiments, a health and usage monitoring system comprises a capacitive load cell and a processing unit for communication with the capacitive load cell, the capacitive load cell comprising a load receiving surface and a capacitive assembly coupled to the load receiving surface, the capacitive assembly comprising parallel electrically conductive plates separated by a reversibly deformable spacer construction wherein the parallel plates comprise aligned apertures providing a passageway through the capacitive assembly for the hoist system cable.

Hoist health and usage monitoring system and components thereof

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 sensor for monitoring external loads acting on a pin assembly includes a pin having an axial interior bore defined therein and having a length defined from a first end to an opposed second end thereof. A core pin is mounted axially within the interior bore of the pin spaced radially inwardly from the interior bore for relative displacement with respect to the pin. A capacitor is provided having an inner capacitor plate mounted to the core pin, and an outer capacitor plate mounted to the pin, such that relative displacement of the core and the pin due to external loading on the pin results in relative displacement of the inner and outer capacitor plates. The capacitor is configured and adapted to be connected to an electrical circuit to produce signals indicative of external loading on the pin based on relative displacement of the inner and outer capacitor plates.

Capacitive sensors for monitoring load bearing on pins

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 force balanced mass flow meter is disclosed that includes a cylindrical sensor housing having an interior bore, an impeller body supported for axial rotation within the interior bore of the sensor housing, and including structure for converting fluid inertia into flow induced torque when fluid flows relative to the impeller body, a proximity sensor for measuring a rotation angle of the impeller body relative to the sensor housing, an electromagnet for generating a magnetic field about the sensor housing to prevent rotation of the impeller body, electronics for determining electrical values from the proximity sensor when fluid flows relative to the impeller body and a controller for controlling current supplied to the electromagnet in response to electrical values determined from the proximity sensor, to generate a magnetic field sufficient to prevent impeller rotation.

Growing community of inventors

Bloomington, MN, United States of America

Christopher Sanden