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1.发明申请公开(公告)号：US20230109847A1
公开(公告)日：2023-04-13
申请号：US17544334
申请日：2021-12-07
Applicant: Honeywell International Inc.
Abstract: Disclosed are methods, systems, and non-transitory computer-readable media for providing contextual building height information to one or more operators of an aircraft. For instance, the method may include obtaining aircraft flight information including a current position and a current altitude of the aircraft; and retrieving, from a database, building information for one or more buildings located in a flight path area, the flight path area including the current position of the aircraft. The method may further include assigning one or more visual characteristics to each of the one or more buildings located in the flight path area based at least in part on the building information and the current altitude of the aircraft; and displaying, to the one or more operators of the aircraft, the one or more buildings located in the flight path area with the assigned one or more visual characteristics.
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公开(公告)号：US10909865B2
公开(公告)日：2021-02-02
申请号：US16268687
申请日：2019-02-06
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Jayasenthilnathan Balasubramanian , Saravanakumar Gurusamy , Roger W. Burgin , Vamsi K Gundluru
Abstract: A method and system for identifying and displaying alerts of air traffic by receiving input data to a processor of an aircraft wherein the input data comprises: distress, emergency, and special traffic data; generating, by a graphic device coupled to the processor, restricted and unrestricted airspace about the aircraft based the input data; displaying, by the graphic device, the restricted and unrestricted airspace on a display of the aircraft to view on a traffic map the restricted and unrestricted airspace for navigating the aircraft; and generating, by a graphic device coupled to the processor, restricted and unrestricted airspace about the aircraft based on the input data from an aircraft transponder, an emergency locator beacon and an ADS-B emitter.
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公开(公告)号：US20220063431A1
公开(公告)日：2022-03-03
申请号：US17009466
申请日：2020-09-01
Applicant: HONEYWELL INTERNATIONAL INC.
Abstract: Systems and methods are provided for displaying operating data for a re-chargeable battery for an electric vehicle. The system comprises a re-chargeable battery for powering components of an electrical vehicle, a sensor that detects a present level of charge in the battery and a display. The display receives the present level of charge of the battery from the monitor and displays the present level of charge in the battery, a required level of endurance for the battery that is based on a planned operational parameter for the vehicle, a minimum level of charge in the battery that meets the required level of endurance, and an amount of time needed to re-charge the battery to achieve the minimum level of charge.
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4.发明申请公开(公告)号：US20200251002A1
公开(公告)日：2020-08-06
申请号：US16268687
申请日：2019-02-06
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Jayasenthilnathan Balasubramanian , Saravanakumar Gurusamy , Roger W. Burgin , Vamsi K Gundluru
Abstract: A method and system for identifying and displaying alerts of air traffic by receiving input data to a processor of an aircraft wherein the input data comprises: distress, emergency, and special traffic data; generating, by a graphic device coupled to the processor, restricted and unrestricted airspace about the aircraft based the input data; displaying, by the graphic device, the restricted and unrestricted airspace on a display of the aircraft to view on a traffic map the restricted and unrestricted airspace for navigating the aircraft; and generating, by a graphic device coupled to the processor, restricted and unrestricted airspace about the aircraft based on the input data from an aircraft transponder, an emergency locator beacon and an ADS-B emitter.
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公开(公告)号：US12269610B2
公开(公告)日：2025-04-08
申请号：US17570834
申请日：2022-01-07
Applicant: Honeywell International Inc.
Inventor： Jayasenthilnathan Balasubramanian , Byron Birkedahl , Kalimulla Khan , Srihari Jayathirtha
Abstract: Disclosed are systems, methods, and non-transitory computer-readable medium for providing a safe landing for an aerial vehicle. The method may include: displaying, on one or more displays, an aerial vehicle, an intended landing zone, and a real-time flight path of the vehicle as the vehicle approaches the intended landing zone; receiving data related to one or more of the vehicle, the flight path of the vehicle, the intended landing zone, and an obstacle; determining the proximity of the vehicle relative to the center of the intended landing zone based on the received data; displaying the proximity of the vehicle relative to the center of the intended landing zone; displaying the obstacle when present; displaying an alert when the vehicle deviates in proximity to the center of the intended landing zone and/or approaches the obstacle; and upon determining a failure to respond to the alert computing flight controls to modify landing.
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Patent Agency Ranking
公开(公告)号：US20250037589A1
公开(公告)日：2025-01-30
申请号：US18357386
申请日：2023-07-24
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Jayasenthilnathan Balasubramanian , Timothy Zieska , Alfredo Gonzalez
IPC: G08G5/00
Abstract: Embodiments of the present disclosure are directed to providing autonomous protected flight zones during emergency operations of aerial vehicles. In an example embodiment, a three-dimensional (3D) protected zone around a flight path for an aerial vehicle associated with an emergency operations event is generated based on emergency flight plan information for the aerial vehicle. Additionally, the 3D protected zone and/or the emergency flight plan information are broadcasted to a different aerial vehicle in a certain vicinity of the aerial vehicle. In response to the aerial vehicle arriving at a designated location, a removal indicator for the 3D protected zone and/or the emergency flight plan information are broadcasted to the different aerial vehicle.
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公开(公告)号：US12141731B2
公开(公告)日：2024-11-12
申请号：US17581405
申请日：2022-01-21
Applicant: Honeywell International Inc.
Inventor： Srihari Jayathirtha , Kalimulla Khan , Jayasenthilnathan Balasubramanian , Yogiraj Dattaram More
IPC: G06Q10/0635 , G06Q10/0639
Abstract: Various embodiments described herein relate to performance assurance modeling for a portfolio of assets. In this regard, a request to generate one or more performance assurance insights related to one or more assets is received. The request includes a fault descriptor describing one or more faults associated with the one or more assets. In response to the request, a first risk level associated with the one or more faults is determined based on the fault descriptor and asset data associated with the one or more assets. Additionally, in response to the request, a second risk level associated with the one or more faults is generated based on one or more predetermined relationships between faults and asset performance indicator thresholds. The one or more performance assurance insights are then generated based on a comparison between the first risk level and the second risk level.
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8.发明授权公开(公告)号：US12033525B2
公开(公告)日：2024-07-09
申请号：US17544334
申请日：2021-12-07
Applicant: Honeywell International Inc.
CPC classification number: G08G5/0086 , G06F16/29 , G08G5/0021 , G08G5/003 , G08G5/045
Abstract: Disclosed are methods, systems, and non-transitory computer-readable media for providing contextual building height information to one or more operators of an aircraft. For instance, the method may include obtaining aircraft flight information including a current position and a current altitude of the aircraft; and retrieving, from a database, building information for one or more buildings located in a flight path area, the flight path area including the current position of the aircraft. The method may further include assigning one or more visual characteristics to each of the one or more buildings located in the flight path area based at least in part on the building information and the current altitude of the aircraft; and displaying, to the one or more operators of the aircraft, the one or more buildings located in the flight path area with the assigned one or more visual characteristics.
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公开(公告)号：US11845351B2
公开(公告)日：2023-12-19
申请号：US17009466
申请日：2020-09-01
Applicant: HONEYWELL INTERNATIONAL INC.
CPC classification number: B60L53/60 , B60L58/12 , H02J7/0013 , H02J7/0048 , B60L2200/10 , B60L2270/00
Abstract: Systems and methods are provided for displaying operating data for a re-chargeable battery for an electric vehicle. The system comprises a re-chargeable battery for powering components of an electrical vehicle, a sensor that detects a present level of charge in the battery and a display. The display receives the present level of charge of the battery from the monitor and displays the present level of charge in the battery, a required level of endurance for the battery that is based on a planned operational parameter for the vehicle, a minimum level of charge in the battery that meets the required level of endurance, and an amount of time needed to re-charge the battery to achieve the minimum level of charge.
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公开(公告)号：US11731763B2
公开(公告)日：2023-08-22
申请号：US17337894
申请日：2021-06-03
Applicant: Honeywell International Inc.
Inventor： Jayasenthilnathan Balasubramanian , Srihari Jayathirtha
CPC classification number: B64D11/0015 , G08G5/0013 , G08G5/0039 , G08G5/0056 , H04W4/42 , H04W4/90
Abstract: Disclosed are methods and systems for identifying and addressing passenger issues in an aircraft. For instance, the method may include receiving sensor data corresponding to one or more sensors associated with a passenger compartment of the aircraft, analyzing the received sensor data to determine a condition of the passenger compartment of the aircraft, identifying one or more passenger issues occurring in the aircraft, and determining one or more response options to address the one or more passenger issues, based at least in part on the one or more passenger issues and an operational parameter of the aircraft. The method may further include communicating, the one or more passenger issues and the one or more response options to a passenger user interface or a ground control station and modifying an operation of the aircraft in accordance with one or more of the one or more response options.
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