公开(公告)号：US12125393B2

公开(公告)日：2024-10-22

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

IPC: G08G5/00 ,  B64D45/00 ,  H04W4/42

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.

公开(公告)号：US12122530B2

公开(公告)日：2024-10-22

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

IPC: B64D43/00 ,  B64C13/16 ,  G08G5/00

CPC classification number: B64D43/00 ,  B64C13/16 ,  G08G5/003

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.

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.

公开(公告)号：US20190149404A1

公开(公告)日：2019-05-16

申请号：US15884835

申请日：2018-01-31

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Phillip Toews ,  Rajeev Mohan ,  Ravish Udupa ,  Richard Snyder ,  Robert Brownlee ,  Brian Walter ,  Daniel E. Lewis

IPC: H04L12/24 ,  H04L29/08 ,  G08G5/00

Abstract: Methods for providing a flight management service in a cloud computing environment, the method includes: receiving, an object request by a server from a mobile device wherein the server is located in the cloud computing environment including: at least a flight management system (FMS) connected to a stateless object; processing, by the connected FMS hosted by the server, the object request generating a resource object for a particular flight plan wherein the resource object includes a data set; storing, by the connected FMS, the data set at the stateless object in the cloud environment; and sending, by the server, an object response from the connected FMS to the mobile device, for accessing the data set of the stateless object for the particular flight plan.

公开(公告)号：US11527164B2

公开(公告)日：2022-12-13

申请号：US16997357

申请日：2020-08-19

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sivakumar Kanagarajan ,  Richard Snyder ,  Joshua Gavroy ,  Chunyu Sheng ,  Ivan Wyatt

IPC: G08G5/00 ,  B64D43/00

Abstract: Human-machine interface for required time of arrival (RTA) constraint negotiation. Embodiments present critical RTA information and results of associated data calculations to the pilot in a concise and informative manner using a dialogue box with intuitive graphical displays. Embodiments present critical RTA information to assist a pilot in negotiating the RTA constraint with air traffic controllers, accepting the clearance, and having confidence in the system that it will achieve the defined RTA constraint.

公开(公告)号：US20210390863A1

公开(公告)日：2021-12-16

申请号：US16997357

申请日：2020-08-19

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sivakumar Kanagarajan ,  Richard Snyder ,  Joshua Gavroy ,  Chunyu Sheng ,  Ivan Wyatt

IPC: G08G5/00 ,  B64D43/00

Abstract: Human-machine interface for required time of arrival (RTA) constraint negotiation. Embodiments present critical RTA information and results of associated data calculations to the pilot in a concise and informative manner using a dialogue box with intuitive graphical displays. Embodiments present critical RTA information to assist a pilot in negotiating the RTA constraint with air traffic controllers, accepting the clearance, and having confidence in the system that it will achieve the defined RTA constraint.

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.

公开(公告)号：US10854093B2

公开(公告)日：2020-12-01

申请号：US15867666

申请日：2018-01-10

Applicant: Honeywell International Inc.

Inventor： Richard Snyder ,  Rajeev Mohan ,  Rajesh Chaubey ,  Ravish Udupa ,  Sharanabasappa Advani

IPC: G08G5/00 ,  G08G5/02 ,  G06F17/00

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.

公开(公告)号：US10755490B2

公开(公告)日：2020-08-25

申请号：US15989352

申请日：2018-05-25

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Raghu Shamasundar ,  Philip Toews ,  Srihari Jayathirtha ,  Kalimulla Khan ,  Mahesh Sivaratri ,  Sreenivasan Govindillam K ,  Robert Brownlee ,  Richard Snyder

IPC: G07D5/00 ,  G07C5/08 ,  G07C5/00 ,  H04W4/42 ,  G08G5/00

Abstract: Systems and methods are disclosed for brokering data exchanges between on-board and off-board systems of a vehicle. One method comprises receiving, at a data broker engine, one or more data requests from an origination system, wherein each of the one or more data requests specifies at least one or more of a request type and a target system. Then the data broker engine determines whether the request type is a one-time transmission, a periodic transmission, an event-triggered transmission, or a change-triggered transmission. Following the determination, the data broker engine retrieves data from the target system based on the determined request type and transmits the data to the origination system.

公开(公告)号：US20220382299A1

公开(公告)日：2022-12-01

申请号：US17660889

申请日：2022-04-27

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Raghu Shamasundar ,  Subhransu Sahoo ,  Richard Snyder ,  Kalimulla Khan ,  Ramkumar Rajendran

IPC: G05D1/10 ,  G08G5/00 ,  G01C21/20

Abstract: A system and method in an aircraft for providing enhanced services is provided. In one example, the method includes: setting up triggering logic to identify a beginning point and ending point for collecting a set of avionics system data during a flight; and systematically retrieving information for use by the triggering logic to identify the beginning point and the ending point. When the beginning point is reached, the method includes systematically repeating: retrieving the set of avionics systems data; and sending, to an off-board application, data from the set of avionics system data that has changed state from prior data sent to the off- board application. When the ending point is reached, the method includes cease sending data from the set of avionics system data to the off-board application.