Honeywell International Inc.

Anup Raje

David B Dwyer

Charles Dairman

Nayyar Azam Khan Rao

Justin Schassler

Robert E Flasher

Paramjit Kaur

Carol Rogers

Robert Pickell

Ratan Khatwa

Ivan Sandy Wyatt

Saravanakumar Gurusamy

Jan Bilek

Subash Samuthirapandian

William H Rogers

Zdenek Eichler

Melissa Ziarnick

Pamela Mannon

Fazurudheen A

Prithvi Krishnamurthy

Nirupam Karmakar

Don Moldenhauer

Ravi Kumar Harapanahalli

Rob Odgers

Systems and methods are disclosed for exchanging real-time data between vehicle systems by receiving, at a first source system, a request for data from a requestor and, based on determining that the first source system does not have all requested data, querying an operations center for missing data. Then, based on determining that the operations center does not have all missing data, the operations center is queried for a list comprising candidate source systems. Upon identifying a next source system from the list, the next source system is queried for missing data, and the next source system is removed from the list. Based on whether the next source system has all missing data, either all missing data is transmitted to the requestor, or, the process of finding and querying for the missing data is iteratively performed until all missing data is received or the list is empty.

Methods and systems for vehicle based internet of things

An apparatus and method for receiving and processing weather data and flight plan data is disclosed. The apparatus includes a first display, an input unit, and a processor. The processor is configured to receive flight plan data and weather data, and to determine, based on the weather data, which weather characteristics is located within a predetermined range of a predetermined flight altitude value. The processor is further configured to instruct the first display to display those weather data which are located within the predetermined range above and below the input flight altitude value together with the flight plan data, and to instruct the first display to additionally display at least one element of the group consisting of the elements: strategic information weather, uplink weather, weather information from external weather data provider, onboard weather radar information, notice to airmen, aeronautical information service data, terminal area forecast, air-traffic related information.

Display device for vertical presentation of forecast weather

A system and method are provided for displaying visual flight reference points and their associated flight data. This is achieved by coupling a processor to a display system and configured the processor to generate symbology graphically representative of the VRPs and their associated flight data. The display system then renders the VRP symbology and the flight data symbology proximate to the VRP symbology. In addition, the processor is configured to alter the symbology of the VRPs depending on the estimates elapsed time for each of the VRPs to become visible to the aircraft.

System and method for displaying visual flight reference points

An aircraft display system is provided and configured to render a cockpit display having a field-of-view. The system comprises a monitor and a processor coupled to the monitor and configured to generate a vertical situation display on the monitor. The vertical situation display includes at least one graphic indicative of a region of the terrain encompassed by the field-of-view.

System and method for indicating a perspective cockpit field-of-view on a vertical situation display

A flight deck communication and display system () for displaying a modified flight plan transmitted to an aircraft () is described including a processor () adapted to receive (i) data representative of a current aircraft flight plan () and (ii) a textual message representative of the modified flight plan () and operable, in response thereto, to supply a flight plan display command, and a modified flight plan display command, and comparing the textual clearance message with factors affecting aircraft safety to supply an alert message display command (). A display () coupled to receive the flight plan display command, the modified flight plan display command, the alert message display command is operable, in response thereto, to substantially simultaneously display () (i) an image representative of the current aircraft flight plan, (ii) the textual clearance message, (iii) the modified flight plan, and (iv) an alert message indicating whether there are any safety concerns related to the textual air traffic modified flight plan.

Flight deck communication and display system

A display system is provided that renders a horizontal situation indicator that includes required navigation performance (RNP) and estimated position uncertainty (EPU) values rendered non-numerically and in a fairly intuitive manner. A processor receives at least data representative of a desired course of the aircraft, data representative of the RNP for the aircraft, and data representative of the EPU for the aircraft. The processor renders, on a display device, a horizontal situation indicator that includes an aircraft symbol representative of a top-down view of the aircraft, an RNP boundary graphic representative of at least one RNP boundary for the aircraft, and an EPU graphic representative of the EPU for the aircraft. The aircraft symbol is rendered at a position that is representative of actual aircraft position relative to the desired course, and the RNP boundary graphic is rendered at a position relative to the rendered aircraft symbol and comprises a shaded region that shades a portion of the display device.

System for displaying required navigation performance on a horizontal situation indicator

A display system is provided that renders a horizontal situation indicator that includes required navigation performance (RNP) and estimated position uncertainty (EPU) values rendered non-numerically and in a fairly intuitive manner. A processor receives at least data representative of a desired course of the aircraft, data representative of the RNP for the aircraft, and data representative of the EPU for the aircraft. The processor renders, on a display device, a horizontal situation indicator that includes an aircraft symbol representative of a top-down view of the aircraft, an RNP boundary graphic representative of at least one RNP boundary for the aircraft, and an EPU graphic representative of the EPU for the aircraft. The aircraft symbol is rendered at a position that is representative of actual aircraft position relative to the desired course, and the RNP boundary graphic is rendered at a position relative to the rendered aircraft symbol.

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Karnataka, India

Anup Raje