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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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公开(公告)号：US20230373653A1
公开(公告)日：2023-11-23
申请号：US17663911
申请日：2022-05-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Shobana Arumugam , Sripathi Ramachandra , Randy Moore
CPC classification number: B64D45/0005 , B64D45/04 , G05D1/0676 , G08G5/025
Abstract: An aircraft flap malfunction detection and landing assist system and method includes supplying flap status data, from a flap status data source, that indicates at least aircraft flap configuration and operability, supplying aircraft state data, from an aircraft state data source, that indicates at least aircraft weight, aircraft speed, and aircraft position, supplying weather data, from a weather data source, that indicates current weather at a landing runway, processing, in a processing system the flap status data to determine if at least one flap is inoperable and, upon determining that the at least one flap is inoperable, processing the flap status data, the aircraft state data, and the weather data to selectively generate, and command a display device to render, at least one of forward slip landing parameters or side slip landing parameters.
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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：US10290217B1
公开(公告)日：2019-05-14
申请号：US16008233
申请日：2018-06-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Sripathi Ramachandra , Patricia May Ververs , Thea L. Feyereisen , Karel Mundel , Mohammed Ibrahim Mohideen , Mark Pearson , Srikanth Desai
Abstract: Improved systems and methods for the evaluation of runway changes that analyze the effect of the runway change on relevant factors, and provide intuitive visual feedback of the analysis, are provided. The provided systems and methods depict the original runway and the new runway, side by side, in a pictorial representation. Additionally, a selectable group of relevant factors for each runway is determined. The pictorial representation is overlaid with one or more symbolic indicators that distinctly demark each of the factors, alphanumeric descriptors may also be displayed alongside the symbolic indicators. The provided systems and methods additionally generate a tabular display of the information and factors. The tabular display provides a side by side comparison of the old runway, the new runway, and the relevant factors.
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公开(公告)号：US11587447B2
公开(公告)日：2023-02-21
申请号：US17098561
申请日：2020-11-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Sripathi Ramachandra , Michael Jackson , Ryan Howe-Veenstra
Abstract: Systems and methods provide dynamically modifiable parameters in required time of arrival (RTA) speed regions of an assigned flight path of an aircraft. The system includes a vertical situation display (VSD) rendering thereon a vertical flight profile of the assigned flight path. A control module is coupled to the display system and configured to: demark the vertical flight profile with a plurality of RTA speed regions related to an initial speed profile; render an RTA speed band graphic having demarked sections vertically representing a speed minimum and speed maximum for an respective RTA speed region, the RTA speed band graphic representing a normalized speed range between zero and a maximum value for each respective RTA speed region. The control module accepts user modifications and updates the RTA speed band graphic and the current speed profile to reflect user input.
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Patent Agency Ranking
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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公开(公告)号：US10417919B1
公开(公告)日：2019-09-17
申请号：US16137010
申请日：2018-09-20
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Srihari Jayathirtha , Kalimulla Khan , Sripathi Ramachandra , Chavdar Kirov , Dinkar Mylaraswamy
Abstract: Systems and methods that optimize landing performance are provided. The system determines a number, N, of equipment configurations (a combination of a brake setting and a thrust reverser configuration) supported by the aircraft. The system determines a deceleration airspeed to achieve a target taxi speed and, for each of the N equipment configurations, determines a respective deceleration distance. In various embodiments, the system further updates the deceleration distances by one or more of a brake's condition, aircraft historical data, brake warranty and life cycle data, and environmental conditions. The deceleration distances are used to identify a number P of exit-ways that can be used at the runway. Total costs (including brake usage and fuel cost) for each of the P exit-ways is determined, and the equipment configuration that delivers the lowest total cost delivers the optimize landing performance.
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9.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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公开(公告)号：US11842651B2
公开(公告)日：2023-12-12
申请号：US16953444
申请日：2020-11-20
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Sripathi Ramachandra , Shobana Arumugam , Anil Kumar Songa , Mohammed Ibrahim Mohideen , Sabu Mathew , Ruben Carrillo
CPC classification number: G08G5/025 , G08G5/003 , G08G5/0021
Abstract: Methods and systems are provided for providing a runway awareness system for an aircrew of an aircraft. The method comprises receiving a first data stream that provides operational characteristics of a primary aviation parameter on approach to the runway. A second data stream is also received that provides operational characteristics of an alternative aviation parameter on approach to the runway. The first data stream and the second data stream are then displayed in a comparative layout format on a flight display for the aircrew of the aircraft during the approach to the runway.
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