Patent application number | Description | Published |
20100036607 | Apparatus and Method to Indicate Course Deviation Instrument Saturation - An apparatus and method to maintain traditional navigational deviation presentation in a manner that is consistent with existing training and safety methodology, but eliminates confusion generated when a navigation needle is placed in a fully pegged position by positively indicating that a needle is off-scale and not representing an actual accurate deviation. | 02-11-2010 |
20120001773 | AVIONICS DEVICE, SYSTEMS AND METHODS OF DISPLAY - The present general inventive concept relates to methods and systems to select and display information on an avionics display screen. The systems and methods allow for the selection and display of information using knobs to highlight and select the desired information for display, eliminating the need for a cursor function. The systems and methods also provide for multiple pages and/or multiple windows or “tiles” within these pages and/or windows simultaneously on a single screen of a display, with each window, page, and/or tile being fully controlled independently when selected. The present general inventive concept also relates to systems and methods to provide multiple cues on an electronic display system altitude tape to a pilot in advance and impending approach to a predefined altitude. The present general inventive concept also relates to systems and methods to employ variable resolution topographical data based on display range for an avionics navigation display. | 01-05-2012 |
20120001774 | ELECTRONIC AVIONICS SYSTEMS AND METHODS - The present general inventive concept relates to a system of method having an electronic flight display that meets the FAR 23.1311(b) regulatory requirement for redundant backup instruments in the cockpit. The present general inventive concept also provides a system and method to detect failures, obstructions, or improper operation of the aircraft pitot pressure sensing system using a combination of dissimilar sensor data that is independent from each other, e.g., allocated from different sources and employed for different purposes on different displays, and displays information on an avionics display screen. | 01-05-2012 |
20130314258 | ELECTRONIC AVIONICS SYSTEMS AND METHODS - The present general inventive concept relates to a system of method having an electronic flight display that meets the FAR 23.1311(b) regulatory requirement for redundant backup instruments in the cockpit. The present general inventive concept also provides a system and method to detect failures, obstructions, or improper operation of the aircraft pitot pressure sensing system using a combination of dissimilar sensor data that is independent from each other, e.g., allocated from different sources and employed for different purposes on different displays, and displays information on an avionics display screen. | 11-28-2013 |
20140277856 | AVIONICS DEVICE, SYSTEMS AND METHODS OF DISPLAY - The present general inventive concept relates to methods and systems to select and display information on an avionics display screen. The systems and methods allow for the selection and display of information using knobs to highlight and select the desired information for display, eliminating the need for a cursor function. The systems and methods also provide for multiple pages and/or multiple windows or “tiles” within these pages and/or windows simultaneously on a single screen of a display, with each window, page, and/or tile being fully controlled independently when selected. The present general inventive concept also relates to systems and methods to provide multiple cues on an electronic display system altitude tape to a pilot in advance and impending approach to a predefined altitude. The present general inventive concept also relates to systems and methods to employ variable resolution topographical data based on display range for an avionics navigation display. | 09-18-2014 |
20150019862 | AVIONICS GATEWAY INTERFACE, SYSTEMS AND METHODS - Systems and methods are provided for FAA-certified avionics devices to safely interface with non-certified mobile telecommunications devices before, during, and after flight. Data transmitted to the certified devices do not affect functionality of the certified device unless and until a user acknowledges and/or confirms the data on the certified device. Thus, the integrity of the certified device is maintained. | 01-15-2015 |
20150074424 | AVIONICS GATEWAY INTERFACE, SYSTEMS AND METHODS - Systems and methods are provided for FAA-certified avionics devices to safely interface with non-certified mobile telecommunications devices before, during, and after flight. Data transmitted to the certified devices do not affect functionality of the certified device unless and until a user acknowledges and/or confirms the data on the certified device. Thus, the integrity of the certified device is maintained. | 03-12-2015 |
20160118788 | AIRBORNE POWER SYSTEM DISCONNECT SYSTEM AND METHOD - An system and method to automatically disconnect a retrofit electrical unit from an electrical system in the event of an emergency situation and maintain power to the retrofit electrical unit. | 04-28-2016 |