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1.发明授权公开(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
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.
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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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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
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.
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Patent Agency Ranking
公开(公告)号：US11385072B2
公开(公告)日：2022-07-12
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 , G06F3/04847 , G06F3/0482
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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公开(公告)号：US20200051441A1
公开(公告)日：2020-02-13
申请号：US16100763
申请日：2018-08-10
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Sripathi Ramachandra , Greg Carlucci , Richard Snyder , Mohammed Ibrahim Mohideen , Mark Pearson , Hyden Lopez , Christopher Raj Mariadoss
Abstract: An aircraft and a method for operating the same are provided. The aircraft, for example, may include, but is not limited to, a flight management system, a vertical situation display, and a processor configured to determine a first variable, a second variable and a third variable, determine flight plan data for the first, second and third variables, generate display data for the vertical situation display, the display data including the scale of the first second and third variables and a vector corresponding to the flight plan data of the first variable and second variable scaled to the first scale and the second scale, wherein the scale of the third variable is non-linear and varies based upon the flight plan data corresponding to the third variable relative to the vector, and output the generated display data to the vertical situation display for display on the vertical situation display.
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公开(公告)号：US11328610B2
公开(公告)日：2022-05-10
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 , G06F16/9537 , 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.
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公开(公告)号：US11043130B2
公开(公告)日：2021-06-22
申请号：US16100763
申请日：2018-08-10
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Sripathi Ramachandra , Greg Carlucci , Richard Snyder , Mohammed Ibrahim Mohideen , Mark Pearson , Hyden Lopez , Christopher Raj Mariadoss
Abstract: An aircraft and a method for operating the same may include, but is not limited to, a flight management system, a vertical situation display, and a processor configured to determine a first variable, a second variable and a third variable, determine flight plan data for the first, second and third variables, generate display data for the vertical situation display, the display data including the scale of the first second and third variables and a vector corresponding to the flight plan data of the first variable and second variable scaled to the first scale and the second scale, wherein the scale of the third variable is non-linear and varies based upon the flight plan data corresponding to the third variable relative to the vector, and output the generated display data to the vertical situation display for display on the vertical situation display.
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8.发明申请公开(公告)号：US20190279514A1
公开(公告)日：2019-09-12
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
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.
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