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1.发明公开公开(公告)号：US20230215281A1
公开(公告)日：2023-07-06
申请号：US17651525
申请日：2022-02-17
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Subhransu Sahoo , Kalimulla Khan , Raghu Shamasundar , Sreenivasan Govindillam , Richard Snyder
CPC classification number: G08G5/0039 , B64D45/00 , G08G5/0013 , G08G5/0021 , G08G5/0091 , H04W4/42 , B64D2045/0075
Abstract: Systems and methods for coordinating with a flight management system (FMS) on-board an aircraft to determine whether a flight plan (FP) change generated by an external device is valid. The method includes generating the FP change, which includes a deviation to the intended FP and a savings parameter associated with a parameter of the intended FP, responsive to weather data and aircraft state data; generating a lateral display showing the intended FP and an alphanumeric window with the FP change; transmitting the FP change to the FMS; receiving, from the FMS, a travel path and a calculated parameter for the travel path, generated by the FMS responsive to the FP change; determining whether the travel path realizes the savings parameter by comparing the calculated parameter to the savings parameter; and, displaying either a selectable graphical user interface (GUI) object to implement the FP change, or a warning based thereon.
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公开(公告)号：US11682308B2
公开(公告)日：2023-06-20
申请号：US17811938
申请日：2022-07-12
Applicant: Honeywell International Inc.
Inventor： Richard Snyder , Rajeev Mohan , Rajesh Chaubey , Ravish Udupa , Sharanabasappa Advani
CPC classification number: G08G5/0039 , G08G5/006 , G08G5/0013 , G08G5/0021 , G08G5/0026 , G08G5/0078 , G08G5/0082 , G08G5/0091 , G08G5/025
Abstract: A system and methods for enhancing operator situational awareness are disclosed. For example, one method includes monitoring a plurality of radio transmissions associated with a plurality of vehicles in a first traffic flow pattern, monitoring a second traffic flow pattern in a vicinity of a vehicle of the plurality of vehicles, monitoring at least one weather value for a destination site for the plurality of vehicles, proposing a destination approach for the vehicle in response to the monitoring, evaluating an impact of the proposed destination approach on an existing travel path for the vehicle, and generating a second travel path for the vehicle in response to the evaluating.
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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：US12183211B2
公开(公告)日：2024-12-31
申请号：US17398733
申请日：2021-08-10
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Steven Curtis Crouch , Santosh Mathan , Matthew Joseph , Bradley Bootz , Richard Snyder
IPC: G08G5/00
Abstract: Methods and apparatus are provided for performing determinations and actions as to a required time of arrival (RTA) for an aircraft during flight. In exemplary embodiments, data is received as to the RTA for the aircraft during flight. Also in exemplary embodiments, determinations are made, via a processor, as to one or more RTA limits for the aircraft based on the RTA. Also in exemplary embodiments, the RTA limits comprise one or both of the following: one or more limits for aircraft speed based on the RTA; and one or more limits for aircraft arrival time based on the RTA.
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Patent Agency Ranking
公开(公告)号：US20230249842A1
公开(公告)日：2023-08-10
申请号：US17656128
申请日：2022-03-23
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Rajesh Chaubey , Gregory Carlucci , Richard Snyder , Michael Jackson , Naresh Bandam , Roopa Niveditha Sundara Kulal , Ambika Sure
Abstract: Methods and systems are provided for assisting operation of a vehicle to satisfy a downpath energy constraint when a current energy state has deviated from a reference energy state according to a planned route of travel. One method involves identifying an intermediate energy constraint at an intermediate point en route to the downpath waypoint, determining a first segment for satisfying the intermediate energy constraint at the intermediate point from the current energy state using a first configuration, determining a second segment from the intermediate point that satisfies the requested energy constraint at the downpath waypoint using a different configuration, and providing graphical indicia of the recommended path including the first and second segments. The graphical indicia includes a first graphical indication of the first configuration associated with the first segment and a second graphical indication of the second configuration associated with the second segment.
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公开(公告)号：US11511881B2
公开(公告)日：2022-11-29
申请号：US16809247
申请日：2020-03-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Philip Toews , Robert Brownlee , John Beckwith , Richard Snyder , Rajeev Mohan , Lior Attias , Salvatore Bottiglieri , Daniel E. Lewis , Helen Edelson , Parker LeBlanc
Abstract: A system includes an aircraft avionics system and a portable computing device. The aircraft avionics system is configured to run one or more embedded avionics applications. The portable computing device is in operable communication with the aircraft avionics system and is configured to run one or more portable device applications. Each portable device application has resident therein a software development kit having libraries and utilities that enables the portable device application to: establish a secure connection with the aircraft avionics system, establish and maintain a required protocol with the embedded avionics application, and communicate with the embedded avionics application as specified by an application programming interface definition.
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公开(公告)号：US11417222B2
公开(公告)日：2022-08-16
申请号：US16945409
申请日：2020-07-31
Applicant: Honeywell International Inc.
Inventor： Richard Snyder , Rajeev Mohan , Rajesh Chaubey , Ravish Udupa , Sharanabasappa Advani
Abstract: A system and methods for enhancing operator situational awareness are disclosed. For example, one method includes monitoring a plurality of radio transmissions associated with a plurality of vehicles in a first traffic flow pattern, monitoring a second traffic flow pattern in a vicinity of a vehicle of the plurality of vehicles, monitoring at least one weather value for a destination site for the plurality of vehicles, proposing a destination approach for the vehicle in response to the monitoring, evaluating an impact of the proposed destination approach on an existing travel path for the vehicle, and generating a second travel path for the vehicle in response to the evaluating.
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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：US20190164433A1
公开(公告)日：2019-05-30
申请号：US15978832
申请日：2018-05-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Connor MacDowell , Todd Hammer , Rajeev Mohan , Partho Sarkar , Ravish Udupa , Richard Snyder
IPC: G08G5/00
Abstract: Systems are provided for providing distributed flight management capability for flight management systems (FMS) of a fleet of aircraft. The system comprises an FMS located on board and electronically integrated into the avionics system of each of the aircraft in the fleet. The system also has a digital twin FMS that contains identical software components and capabilities of the FMS. The digital twin FMS is located off board the aircraft and is in communication with each of the FMSs via a digital communications link. The digital twin FMS is configured to provide pre-flight planning for each aircraft that is dispatched to each FMS via the digital communications link.
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