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    Multiple flight data reference for a specific selection on a vertical and lateral display
    2.
    发明授权
    Multiple flight data reference for a specific selection on a vertical and lateral display 有权

    公开(公告)号：US10706726B2

    公开(公告)日：2020-07-07

    申请号：US15912942

    申请日：2018-03-06

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Sripathi Ramachandra ,  Mark Pearson ,  Greg Carlucci ,  Richard Snyder ,  Balaji Srinivasan

    IPC: G08G5/00 ,  G01C23/00

    Abstract: Methods and systems for a flight display system are provided. The method includes: commanding a vertical situation display (VSD) and a lateral navigation display (ND) to render, concurrently, a viewing segment of a flight plan. The method includes receiving a user input selecting a section of the viewing segment, the user input being received on only one of the VSD and the ND. The method continues by commanding, concurrently, the VSD and the ND to visually distinguish the section, and to demark the section on the VSD with starting points and ending points. The method identifies a flight parameter, and for the flight parameter, includes (a) determining which display, among the VSD and the ND, is appropriate for the rendering of flight parameter information; (b) generating flight parameter information based on (a); and (c) overlaying the flight parameter information on the appropriate display.

    Flight deck multifunction control display unit
    4.
    再颁专利
    Flight deck multifunction control display unit 有权

    公开(公告)号：USRE49067E1

    公开(公告)日：2022-05-10

    申请号：US16425179

    申请日：2019-05-29

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Sue McCullough ,  Mark Pearson ,  Phillip Toews ,  Charles Dairman ,  Shane Lai ,  Hariharan Saptharishi ,  Venkat Ramana Mummadi

    IPC: G10L15/00 ,  G06F3/16 ,  G06F3/01 ,  G10L15/22 ,  G06F3/041 ,  G10L15/26 ,  B64D43/00

    Abstract: Systems and methods for controlling a flight deck multifunction control display unit are disclosed. In various embodiments, the systems may comprise a flight management system or other MCDU driven devices, a command database that stores a plurality of voice commands and a plurality of multifunction control display unit commands. In various embodiments, each voice command is associated with one of the plurality of multifunction control display unit commands. The systems may further comprise a pilot voice interface configured to receive a voice command from a pilot and transmit the voice command to the multifunction control display unit. The multifunction control display unit can receive the voice command from the pilot voice interface and, in response, access the command database to identify a multifunction control display unit command in the command database that is associated with the voice command.

    SYSTEMS AND METHODS FOR PROVIDING USER-MANIPULATED PRIMARY FLIGHT DISPLAY (PFD) DATA ONBOARD AN AIRCRAFT
    7.
    发明申请
    SYSTEMS AND METHODS FOR PROVIDING USER-MANIPULATED PRIMARY FLIGHT DISPLAY (PFD) DATA ONBOARD AN AIRCRAFT 审中-公开

    公开(公告)号：US20190220152A1

    公开(公告)日：2019-07-18

    申请号：US15874066

    申请日：2018-01-18

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Sripathi Ramachandra ,  Mark Pearson ,  PraveenKumar Ayyathurai

    IPC: G06F3/0481 ,  G06F3/0484 ,  G06F3/0485 ,  G06F3/0488 ,  B64D43/00

    Abstract: A method for providing flight data onboard an aircraft is provided. The method obtains avionics data, by a processor communicatively coupled to a display device onboard the aircraft; presents a graphical user interface (GUI), by the display device, wherein the GUI comprises at least a speed tape graphical element and an altitude tape graphical element; receives user input manipulations via a user interface communicatively coupled to the processor; executes the user input manipulations for the altitude tape graphical element or the speed tape graphical element, to generate a revised altitude tape graphical element or a revised speed tape graphical element; generates a revised GUI comprising the revised altitude tape graphical element or the revised speed tape graphical element; and presents the revised GUI, via the display device.

    CUSTOM SEARCH QUERIES FOR FLIGHT DATA
    8.
    发明申请
    CUSTOM SEARCH QUERIES FOR FLIGHT DATA 审中-公开

    公开(公告)号：US20200035109A1

    公开(公告)日：2020-01-30

    申请号：US16043854

    申请日：2018-07-24

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Sripathi Ramachandra ,  Mark Pearson ,  Greg Carlucci ,  Richard Snyder

    IPC: G08G5/00 ,  G06F17/30 ,  B64D43/00

    Abstract: Systems and methods of searching stored flight plan information using a custom search query including at least one aircraft parameter condition or environmental parameter condition. The systems and method include receiving, using a user interface module, a custom search query comprising an aircraft parameter condition or an environmental condition; searching, using a processor module, stored flight plan information for instances in the stored flight plan information that satisfy the aircraft parameter condition or environmental condition; and displaying, using a display module, the instances in the stored flight plan information that satisfy the aircraft parameter condition or environmental condition.

    System and method of providing clipboard cut and paste operations in an avionics touchscreen system
    9.
    发明授权
    System and method of providing clipboard cut and paste operations in an avionics touchscreen system 有权

    公开(公告)号：US10131444B1

    公开(公告)日：2018-11-20

    申请号：US15689171

    申请日：2017-08-29

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Philip Toews ,  Todd Wisner ,  Mark Pearson ,  Susan McCullough

    IPC: B64D43/00 ,  G06F3/0488 ,  G06F3/041 ,  G06F3/0482

    Abstract: A keyboard module configured for use in an avionics touchscreen system is disclosed. The keyboard module is configured to display, via a visual display in the avionics touchscreen system and responsive to a selection of an application program generated widget for focus via a touchscreen surface in the avionics touchscreen system, a virtual keyboard. The virtual keyboard includes a text box widget configured to display clip data stored in clipboard memory provided by the avionics touchscreen system, a copy widget configured to cause data in a first widget provided by the application program that is in focus to be copied to the clipboard memory, and a paste widget configured to cause the clip data in the clipboard memory and displayed in the text box widget to be pasted to a second widget provided by the application program that is in focus.

    ENGINE RELIGHT VISUALIZATION METHODS AND SYSTEMS
    10.
    发明申请
    ENGINE RELIGHT VISUALIZATION METHODS AND SYSTEMS 有权

    公开(公告)号：US20210018333A1

    公开(公告)日：2021-01-21

    申请号：US16512151

    申请日：2019-07-15

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Sripathi Ramachandra ,  Greg Carlucci ,  Karel Mundel ,  Richard Snyder ,  Mark Pearson ,  Udipi Ranga Ananthram ,  PraveenKumar Ayyathurai ,  Samrat Kar

    IPC: G01C23/00 ,  G06F3/0484 ,  G06F3/14 ,  B64D43/02

    Abstract: Methods and systems are provided for presenting an energy state associated with an aircraft with respect to an operating envelope region for a procedure to restart an engine of the aircraft. One method involves providing a graphical user interface display having a first reference axis corresponding to a first energy state parameter and a second reference axis corresponding to a second energy state parameter different from the first energy state parameter, providing a graphical representation of an operating envelope region associated with a procedure for starting an engine of the aircraft with respect to the first and second reference axes, obtaining current values for the first and second energy state parameters for the aircraft, and providing a graphical representation of the aircraft positioned with respect to the first and second reference axes based on the current values for the first and second energy state parameters.

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