Honeywell International Inc.

Ametek Rotron

Matthew Clark

Dean Eivind Johnson

Myles Koshiol

George Goblish

Alan Bruce Touchberry

Terry Dean Stark

Steven P Ecklund

Bruce A Seiber

Stephen Matthew Baker

Craig A Galbrecht

Emily Hart

Robert B Hanson, Ii

Basil Issac

Mark Edward Petersen

Leslie W Yoho

Dean Kei Naritoku

James Mitchell Coker, Iii

Jackson Karl Harwell

Gordon Allen Seppanen

Peter Pronovost

Taylor Ann Peake

Issac Basil

George L Goblish

A system and method for securely displaying patient data within a plurality of display windows of a display is provided. Additionally, the system is configured to reduce the amount of data transferred between the various computing devices in order to reduce strain on a network. The system generally comprises a first computing device having a first user interface, second computing device having a second user interface, processor operably connected to said first computing device and said second computing device, display operably connected to said processor, and non-transitory computer-readable medium coupled to said processor and having instructions stored thereon. The display is configured to receive image data from the first computing device and second computing device and present said image data via a display user interface, wherein said image data pertains to a plurality of application windows of the first user interface and second user interface.

System and method for decreasing data transfer between computing devices

An in-flight contact charging system includes a charging contact, a power receiver, and a recharging controller connected to the charging contact. The charging contact is mounted on a support. The power receiver is mounted on an aerial vehicle containing an electrical load. The power receiver connects to the electrical load. The recharging controller can detect contact between the charging contact and the power receiver; transmit electricity to the charging contact; detect a spike in battery impedance; and discontinue transmission of electricity to the charging contact. The system enables a drone to rapidly recharge its battery while in flight by making brief contact between the charging contact and the power receiver. This system keeps the drone airborne, does not waste energy, and is comparatively cheap to build and maintain.

In-flight contact charging system

Disclosed is a three phase Vienna converter for converting three phase AC to DC, with active power factor control. Further the control electronics is galvanically isolated from the neutral of the input three phase supply and also from the center terminal of the two series connected output DC filter capacitors. The control circuit is built completely with analog devices to meet stringent electromagnetic interference standards. The converter is capable of operating over a wide range of voltages and frequencies of the input supply voltage.

Control circuit and control method for a three phase Vienna converter

A ring laser gyroscope comprises a laser block that includes a resonant internal cavity defined by a plurality of surfaces of an optical closed loop pathway, and a plurality of electrodes coupled to the laser block. The electrodes are configured to generate a pair of counter-propagating laser beams from a lasing gas in the optical closed loop pathway. The ring laser gyroscope also includes a field reducer shield comprising an electrically conductive material, with the field reducer shield located completely within the laser block. The field reducer shield is configured to modify an electric field generated by the plurality of electrodes to substantially prevent ions in the laser block from migrating toward the plurality of surfaces of the optical closed loop pathway.

Ring laser gyroscope with ion migration field reducer shield

A partially-insulated cathode for exciting plasma in a plasma chamber is provided. The partially-insulated cathode includes a conductive structure enclosing a cavity having a cavity surface and an insulating material contiguously covering a portion of the cavity surface from the cavity opening up to an insulation height that is less than a cavity height. Cross-sections of the cavity in X-Y planes have at least one respective cavity-width. A cavity opening has a diameter less than a minimum cavity-width of the at least one cavity-width.

Partially insulated cathode

A ring laser gyroscope configured to reduce alignment shifts in at least one critical alignment of the ring laser gyroscope is provided. The ring laser gyroscope includes reflective components configured to direct clockwise optical beams and counter-clockwise optical beams in at least one lasing plane; at least one ring-laser-gyro mounting feature having at least one respective through hole; and at least one minimally-threaded screw positioned in the at least one respective through hole. An unthreaded section of the minimally-threaded screw is contactlessly encased in the at least one respective through hole. A threaded-end of the at least one minimally-threaded screw is threaded in a respective at least one threaded hole in a gyro frame, the gyro frame spanning a reference mounting plane.

Minimally-threaded screw to reduce alignment shifts

A temperature sensor package includes a temperature sensor having a first side and a second side, wherein the first side of the temperature sensor includes an active region configured for coupling with a target area for temperature measurement of an object. The temperature sensor package further includes a circuit board having a first side and a second side, the first side of the circuit board coupled to the second side of the temperature sensor, wherein the circuit board provides thermal insulation between the active region of the temperature sensor and an environment on the second side of the circuit board.

Temperature sensor attachment facilitating thermal conductivity to a measurement point and insulation from a surrounding environment

An apparatus includes a sheet of circuit board material, at least one electrically conductive trace positioned on the sheet of circuit board material, and at least one electrically conductive contact pad positioned on the sheet of circuit board material and coupled to the at least one electrically conductive trace. The apparatus further includes at least one deformation point configured to absorb stresses developed in the sheet of circuit board material when the sheet of circuit board material experiences resistance to expansion or compression caused by connection to an object resisting expansion or compression.

Mitigation of block bending in a ring laser gyroscope caused by thermal expansion or compression of a circuit board

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Blaine, MN, United States of America

Matthew Clark