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    Systems and methods for providing or requesting avionics simulation data using API adapter
    1.
    发明授权
    Systems and methods for providing or requesting avionics simulation data using API adapter 有权

    公开(公告)号：US10798189B1

    公开(公告)日：2020-10-06

    申请号：US16385253

    申请日：2019-04-16

    Applicant: Honeywell International Inc.

    Inventor： Mahesh Sivaratri ,  Raghu Shamasundar ,  Rajeev Mohan ,  Sushma Bidrupane ,  Soumitri Swain ,  Mythili Belle

    IPC: G09B9/02 ,  H04L29/08 ,  G09B9/08 ,  H04L29/06

    Abstract: Systems and methods are disclosed for providing or requesting data for simulating avionics systems. For example, a method for providing data for simulating avionics systems may include: receiving, from a client device, a first message requesting information usable by the client device to simulate a functionality of an avionics system, the first message being in a web services data format; converting the first message to an avionics protocol data format to obtain a first converted message; providing the first converted message to a server application; receiving, from the server application, a second message including the requested information, the second message being in the avionics protocol data format; converting the second message to the web services data format to obtain a second converted message; and providing, to the client device, the second converted message.

    METHODS, AND SYSTEMS FOR ENABLING EFFECTIVE MODELING OF LANDING GEAR FOR ENERGY MANAGEMENT
    2.
    发明申请
    METHODS, AND SYSTEMS FOR ENABLING EFFECTIVE MODELING OF LANDING GEAR FOR ENERGY MANAGEMENT 有权

    公开(公告)号：US20220266989A1

    公开(公告)日：2022-08-25

    申请号：US17225387

    申请日：2021-04-08

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Ambika Sure ,  Chethan N ,  Rajesh Chaubey ,  Roopa Niveditha Sundara Kulal ,  Soumitri Swain ,  Sripathi Ramachandra

    IPC: B64C25/26 ,  B64D43/00

    Abstract: Methods and systems are provided for guiding or otherwise assisting energy management of an aircraft en route to a runway. A method to optimize managing energy of an aircraft in a landing trajectory when deploying landing gear, the system including evaluating an energy state for the aircraft for a set of flight trajectories including a lateral and a vertical trajectory for a flight path in an approach phase to a runway; identifying at least one energy state for the aircraft based on a set of formulated computations based on an altitude and speed of a vertical aircraft profile on the flight path in the approach phase; and assessing in an envelope region a landing gear extension to manage the excess energy at a prediction location in the flight path; and deploy the landing gear responsive to an assessed change in the aircraft energy state in route to the runway.

    System and method for modifying multiple request datalink messages in avionics system
    3.
    发明授权
    System and method for modifying multiple request datalink messages in avionics system 有权

    公开(公告)号：US10771558B2

    公开(公告)日：2020-09-08

    申请号：US15483735

    申请日：2017-04-10

    Applicant: Honeywell International Inc.

    Inventor： Raghu Shamasundar ,  Thomas D. Judd ,  Soumitri Swain

    IPC: G06F3/048 ,  G08G5/00 ,  H04L29/08 ,  G01C23/00

    Abstract: Systems and methods for modifying multiple element request datalink messages in avionics system are provided. A method includes generating a plurality of downlink message element information at a verify screen displayed by a display. The method further allows for the changing of at least one downlink message element information of the plurality of downlink message element information within the verify screen. Moreover, the method concatenates the plurality of downlink message element information after the changing of the at least one element information in preparation of generating a concatenating downlink message element information message to be downlinked.

    System and method to revise vertical profile of a flight plan
    5.
    发明授权
    System and method to revise vertical profile of a flight plan 有权

    公开(公告)号：US10467912B2

    公开(公告)日：2019-11-05

    申请号：US15458653

    申请日：2017-03-14

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Sue McCullough ,  Mahesh Sivaratri ,  Sujith Kalarickal ,  Kalimulla Khan ,  John R ,  Soumitri Swain

    IPC: G06F3/048 ,  G08G5/00 ,  G06F3/0484 ,  G06F3/0488 ,  G06F3/0485

    Abstract: A vehicular situation display including a user interface, a display, and a processor is provided to modify a vertical profile of a flight plan. The processor may generate vertical profile display data on the display based, receive a request to edit the vertical profile, expand the vertical profile display data on the display, generate a first movable reference line corresponding to one of an altitude, a distance and a time, receive, from the user interface, a flight plan change request to change an altitude, distance or time of the flight plan, the altitude, distance or time corresponding to the first movable reference line, generate a preview of an updated flight plan, and transmit the approval of the displayed updated flight plan to a flight management system, the flight management system configured to update the flight plan of the aircraft based upon the command to change the flight plan.

    SYSTEM AND METHOD FOR MODIFYING MULTIPLE REQUEST DATALINK MESSAGES IN AVIONICS SYSTEM
    6.
    发明申请
    SYSTEM AND METHOD FOR MODIFYING MULTIPLE REQUEST DATALINK MESSAGES IN AVIONICS SYSTEM 审中-公开

    公开(公告)号：US20180292954A1

    公开(公告)日：2018-10-11

    申请号：US15483735

    申请日：2017-04-10

    Applicant: Honeywell International Inc.

    Inventor： Raghu Shamasundar ,  Thomas D. Judd ,  Soumitri Swain

    IPC: G06F3/0482 ,  H04L29/08 ,  H04B1/3822 ,  G06F3/0483

    Abstract: Systems and methods for modifying multiple element request datalink messages in avionics system are provided. A method includes generating a plurality of downlink message element information at a verify screen displayed by a display. The method further allows for the changing of at least one downlink message element information of the plurality of downlink message element information within the verify screen. Moreover, the method concatenates the plurality of downlink message element information after the changing of the at least one element information in preparation of generating a concatenating downlink message element information message to be downlinked.

    SYSTEM AND METHOD TO REVISE VERTICAL PROFILE OF A FLIGHT PLAN
    7.
    发明申请
    SYSTEM AND METHOD TO REVISE VERTICAL PROFILE OF A FLIGHT PLAN 审中-公开

    公开(公告)号：US20180268721A1

    公开(公告)日：2018-09-20

    申请号：US15458653

    申请日：2017-03-14

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Sue McCullough ,  Mahesh Sivaratri ,  Sujith Kalarickal ,  Kalimulla Khan ,  John R ,  Soumitri Swain

    IPC: G08G5/00 ,  G06F3/0484 ,  G06F3/0488 ,  G06F3/0485

    Abstract: A vehicular situation display including a user interface, a display, and a processor is provided to modify a vertical profile of a flight plan. The processor may generate vertical profile display data on the display based, receive a request to edit the vertical profile, expand the vertical profile display data on the display, generate a first movable reference line corresponding to one of an altitude, a distance and a time, receive, from the user interface, a flight plan change request to change an altitude, distance or time of the flight plan, the altitude, distance or time corresponding to the first movable reference line, generate a preview of an updated flight plan, and transmit the approval of the displayed updated flight plan to a flight management system, the flight management system configured to update the flight plan of the aircraft based upon the command to change the flight plan.

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