Honeywell International Inc.

Andrew Abeyta

Thomas D Judd

Harold Anthony Zulch, Iii

A system comprises a physical display unit and an aircraft system component. The aircraft system component is configured to output a first signal for display according to a first display format. The system also includes an abstraction component configured to generate a virtual display page according to the first protocol based on the signal received from the aircraft system component and to map the virtual display page into two or more modified pages. Each of the modified pages is configured according to a second display format and corresponds to a respective portion of the virtual display page. The abstraction component is further configured to output a second signal comprising a first of the two or more modified pages to the physical display unit for display according to the second display format. The abstraction component is configured to output a signal comprising a second modified page based on user input.

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Glendale, AZ, United States of America

Andrew Abeyta