General Electric Company

Lockheed Martin Corporation

Nuovo Pignone Tecnologie Srl

Joseph Alfred Iannotti

Christopher James Kapusta

Yongjae Lee

Marco Francesco Aimi

Christopher Fred Keimel

Glen Peter Koste

Selaka Bandara Bulumulla

David Richard Esler

William P Kornrumpf

Kevin Matthew Durocher

Glenn Scott Claydon

Matthew Christian Nielsen

Richard Louis Frey

Glenn A Forman

Steven Y Go

Eric William Fiveland

William Chester Platt

Robert John Filkins

Samhita Dasgupta

Todd Ryan Tolliver

William Joseph Taft

Joleyn Eileen Brewer

Filippo Gerbi

Douglas Scott Jacobs

Brandon Wayne Miller

Arthur William Sibbach

Stanton Earl Weaver, Jr

Richard J Saia

Arun Virupaksha Gowda

Rick C Stevens

Ronald Dean Watkins

Thomas K F Foo

William Edward Burdick, Jr

Kevin J Thorson

Anthony Wykeham Jacomb-Hood

Erich Alois Krammer

Fraser Robb

Aaron Jay Knobloch

Trang Thuy Thai

Donald Paul Cunningham

Steven William Wik

Nancy Cecelia Stoffel

David Cecil Hays

Charles John Kryzak

Brendon Matthew Leeker

Oliver Charles Boomhower

Mahesh Raveendranatha Panicker

Alessio Capanni

Robert Edward Goeller

Brian Scott Leininger

William Gregg Hawkins

Maxine Marie Gibeau

James Patrick Carneal

Olga B Spahn

Kevin Dufel

Bradley Alan Bauer

William D Cowan

Daryl J Dagel

Mudassar Ali Muhammad

Jason Case

Donald Cunningham

Oliver Charles Boomhoower

Richard Joseph Saia

Fliippo Gerbi

The present disclosure is generally related to a fault isolation sensor system for use with determining whether a potential fault is more likely to be on a rotor side or a stator side. The measurement signals are transmitted from the rotor antenna to the stator antenna, and then from the stator antenna to a controller. The controller is configured to monitor the measurement signals. If the measurement signal is outside of a predetermined range or past a predetermined threshold, then the stator antenna can be interrogated with an interrogation signal with a reflected signal being compared with the interrogation signal and a ratio thereof being used to identify the potential side of the fault.

Fault isolation sensor system and methods

A method for measuring shaft deflection in a turbomachine includes communicating one or more signals from a controller to a plurality of sensing devices positioned on a shaft of a turbomachine across an airgap defined between a rotating antenna positioned around the shaft and a stationary antenna aligned with the rotating antenna in a radial direction to excite the plurality of sensing devices; receiving a parameter of the shaft in a plurality of circumferentially spaced locations from the excited plurality of sensing devices; determining a magnitude of a deflection in the shaft as a function of the parameter of the shaft in the plurality of circumferentially spaced locations; and adjusting a startup sequence or a motoring sequence of the turbomachine based on the magnitude of the deflection.

System and method for reducing motoring time in a turbomachine based on shaft deflection

A system includes a sensor comprising a sensor bonding layer disposed on a surface of the sensor, wherein the sensor bonding layer is a metallic alloy. An inlay includes a planar outer surface, wherein the inlay may be disposed on a curved surface of a structure. A structure bonding layer may be disposed on the planar outer surface of the inlay, wherein the structure bonding layer is a metallic alloy. The sensor bonding layer is coupled to the structure bonding layer via a metallic joint, and the sensor is configured to sense data of the structure through the metallic joint, the structure bonding layer, and the sensor bonding layer. The inlay comprises at least one of a modulus of elasticity, a shape, a thickness, and a size configured to reduce strain transmitted to the sensor.

Sensor system and method

A method for providing overspeed protection for a gas turbine engine having an engine shaft includes monitoring, via an overspeed protection system, a torque of the engine shaft. The method also includes determining, via the overspeed protection system, at least one additional condition of the engine shaft. Further, the method includes determining, via the overspeed protection system, an overspeed condition of the gas turbine engine when the torque of the engine shaft drops below a torque threshold and the at least one additional condition of the engine shaft is indicative of the gas turbine engine being in an operational state. Thus, the overspeed condition is indicative of an above normal rotational speed of the engine shaft. In addition, the method includes initiating a shutdown procedure for the gas turbine engine in response to the determined overspeed condition to reduce the rotational speed of the engine shaft.

Electronic overspeed protection system and method

A method includes obtaining an active feature layer having a first surface bearing one or more active feature areas. A first capacitor plate of a first capacitor is formed on an interior surface of a cap. A second capacitor plate of the first capacitor is formed on an exterior surface of the cap. The first capacitor plate of the first capacitor overlays and is spaced apart from the second capacitor plate of the first capacitor along a direction that is orthogonal to the exterior surface of the cap to form the first capacitor. The cap is coupled with the first surface of the active feature layer such that the second capacitor plate of the first capacitor is in electrical communication with at least a first active feature of the active feature layer. The cap is bonded with the passive layer substrate.

Wafer level stacked structures having integrated passive features

A measuring system is disclosed. The measuring system includes a surface acoustic wave (SAW) device including a piezoelectric substrate and a first and second electrode disposed on a surface of the piezoelectric substrate, and a measuring device communicatively coupled to the first electrode via a first probe and the second electrode via a second probe and configured to apply an electrical signal to the first and second electrode to generate an incident bulk acoustic wave within the piezoelectric substrate, detect at least a first reflected bulk acoustic wave and a second reflected bulk acoustic wave at the first and second electrode, and calculate a thickness between a first interface corresponding to the first reflected bulk acoustic wave and a second interface corresponding to the second reflected bulk acoustic wave based on a time elapsed between detecting the first and second reflected bulk acoustic waves.

Systems and methods for measuring properties using bulk acoustic waves

An electronics package is disclosed. The electronics package includes a first radio frequency (RF) substrate layer, a second RF substrate layer, and a plurality of conductive layers disposed adjacent to at least one of the first RF substrate layer and the second RF substrate layer and including an inner conductive layer disposed between and adjacent to both the first RF substrate layer and the second RF substrate layer. The inner conductive layer bonds the first RF substrate layer to the second RF substrate layer. The electronics package also includes a plurality of conductive interconnects extending through the first RF substrate layer and the second RF substrate layer and electrically coupled between at least two of the plurality of conductive layers.

Systems and methods for hybrid glass and organic packaging for radio frequency electronics

A sensor system for monitoring a condition of a piston rod includes an interrogator system having a first coil winding coupled to a housing and radially spaced from the piston rod such that a gap is defined between the first coil winding and the piston rod. A second coil winding is coupled to the piston rod and is inductively coupled to the first coil winding. The second coil winding is configured to communicate with the first coil winding through a range of linear movement of the piston rod relative to the housing. A sensor is coupled to the second coil winding. The sensor is configured to measure a characteristic associated with the piston rod and generate a current in the second coil winding to transmit, via the inductive coupling with the first coil winding, an electrical output signal associated with the characteristic to the interrogator system.

Systems and methods for piston rod monitoring

A system includes a structure bonding layer and a sensor. The structure bonding layer is disposed on a structure. The structure bonding layer is a metallic alloy. The sensor includes a non-metallic wafer and a sensor bonding layer disposed on a surface of the non-metallic wafer. The sensor bonding layer is a metallic alloy. The sensor bonding layer is coupled to the structure bonding layer via a metallic joint, and the sensor is configured to sense data of the structure through the metallic joint, the structure bonding layer, and the sensor bonding layer.

A sensor system includes a rotor antenna, a radio frequency (RF) sensor, a stator antenna, and one or more processors. The rotor antenna and the RF sensor are configured to be disposed on a shaft of a rotor assembly and are conductively connected to each other. The RF sensor generates measurement signals. The stator antenna is mounted to a stator member of the rotor assembly and positioned radially outward from the rotor antenna. The stator antenna is wirelessly connected to the rotor antenna across an air gap. The one or more processors are communicatively connected to the stator antenna and are configured to monitor one or more electrical characteristics of the measurement signals that are received by the stator antenna from the rotor antenna over time as the shaft rotates and to determine rotational speed of the shaft based on recurrent variations in the one or more electrical characteristics.

Sensor system for a rotor assembly

A beam former module includes a package base and an interconnect structure formed within the package base. The beam former module also includes a first true time delay (TTD) module attached to the package base. The first TTD module includes a plurality of switching elements configured to define a signal transmission path between a signal input and a signal output of the first TTD module by selectively activating a plurality of time delay lines. The signal input and the signal output of the first TTD module are electrically coupled to the interconnect structure. In some embodiments, the interconnect structure includes at least one TTD meander line and at least one of the time delay lines of the first TTD module is electrically coupled to the at least one TTD meander line.

True time delay beam former module and method of making the same

A sensor system includes a rotor antenna, a radio frequency (RF) sensor, a stator antenna, and one or more frequency selective structures. The rotor antenna and the RF sensor are disposed on an outer surface of a shaft and are conductively connected to each other. The RF sensor generates measurement signals as the shaft rotates. The stator antenna is mounted separate from the shaft and positioned radially outward from the rotor antenna. The stator antenna wirelessly receives the measurement signals from the rotor antenna across an air gap. The one or more frequency selective structures are disposed on the outer surface of the shaft and configured to dissipate electromagnetic current that is conducted along the shaft to alleviate interference of the measurement signals.

Rotor assembly sensor system with interference isolation

A monitoring system for monitoring environmental conditions for rotary members includes a plurality of stationary reader antennas positioned proximate rotary members. A first sensor is coupled to a first rotary member and a second sensor is coupled to a second rotary member. Each sensor is configured to generate environmental condition data. A key phasor is coupled to a third rotary member and configured to generate key phasor data. The monitoring system also includes a data integrator communicatively coupled to each stationary reader antenna and configured to determine measurement values for the first and second environmental condition based on raw data from each stationary reader antennas and data from the key phasor.

Wireless monitoring system for rotary machines

Growing community of inventors

Glenville, NY, United States of America

Joseph Alfred Iannotti