Spectralux Corporation

Universal Avionics Systems Corporation

Frank E Hummel

David E Hiney

Patrick Gerald Krohn

Joachim Laurenz Naimer

James A Reynolds

Douglas W Daman

Bryan L Sammons

Steinarr Bragason

Andy R Hill

Thomas Ogle Shafer

John Russell Jorgensen

Tony Monroe Bragg

Justin Grimes

James Dooley

Ronald Abeel

David Zeitouni

Timothy Hong

Drew Johnson

Paul Newby

Brian DeHart

An interface device configured to interface with one or more aircraft avionics data systems and an antenna. The interface device includes a radio and at least one computing device that are housed inside an enclosure. The radio is connected to the antenna. The radio is configured to transmit outgoing messages and to receive incoming messages via the antenna. The at least one computing device is configured to send the outgoing messages to the radio for transmission by the radio via the antenna and to receive the incoming messages from the radio. The radio may be a very high frequency ('VHF') transceiver.

Aviation datalink communications management unit

A control panel or display device that includes a light source, a controller, an illuminated element, a light conductor, and a light sensor. The controller generates a control signal instructing the light source when to generate light. The light conductor conducts light generated by the light source to the illuminated element to illuminate it. The light conductor receives ambient light through the illuminated element when the light source is not generating light. The light sensor receives the ambient light from the light conductor, generates a sensor signal based on the received ambient light, and sends the sensor signal to the controller. The controller determines a brightness level based at least in part on the sensor signal and encodes the brightness level in the control signal. Brightness of the light generated by the light source is based at least in part on the brightness level encoded in the control signal.

Lighted control panel and illuminated display with embedded lighting control

A user interface for an avionics interface device. The interface includes a display, selectable keys, and three annunciations. The keys include alphanumeric, functional, and line select keys. The functional keys are positioned above the display. The alphanumeric keys are positioned below the display. First and second portions of the line select keys are positioned along left and right side portions, respectively, of the display. All of the functional keys are separate and spaced apart from all of the alphanumeric keys. Pressing a line select key selects a line of the display that is positioned next to and aligned with the line select key. The annunciations identify a state of the avionics interface device. First and second annunciations indicate the device is configured to communicate with a Controller-Pilot Data Link Communications system and an Aircraft Communications Addressing and Reporting System, respectively. A third annunciation indicates the device has encountered a failure.

Aircraft avionics data input panel

A monitoring system for alerting operators of aircraft or other vehicles when they are approaching a geographical feature of interest, such as a runway, taxiway or other aircraft. The system includes a database having at least one geo-referenced chart, a processor, a positioning system configured to identify a number of aircraft or other vehicle operational parameters and transmit that data to the processor, and a display unit configured to display the present position of the aircraft on the geo-referenced chart. After receiving the operational parameters, the processor identifies a virtual containment zone centered about the aircraft or vehicle. The processor further monitors the position of the aircraft or other vehicle relative to any geographical features of interest and determines whether at least a portion of a geographical feature is located within the containment area. If such a condition is detected, a notification is generated and presented to the operator who may respond accordingly.

Aircraft-centered ground maneuvering monitoring and alerting system

A monitoring system for alerting pilots of aircraft or operators of vehicles when the aircraft or vehicle is approaching a geographical feature of interest, such as a runway, includes a database including at least one geo-referenced chart; a processor; a positioning system configured to identify at least one of the position, heading, track and velocity of the vehicle, and transmit such data to the processor; and a display unit configured to display the present position of the aircraft on the at least one geo-referenced chart. After receiving the position, heading, track and/or velocity data, the processor determines whether the aircraft has entered a containment area associated with a geographical feature of interest, and if so, provides a visible notification to the pilot or operator, which may comprise a change in display of the geographical feature of interest.

Aircraft ground maneuvering monitoring system

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Woodinville, WA, United States of America

Frank E Hummel