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.

Inventor： Saravanakumar Gurusamy ,  Madhava Gadicherla ,  Jayasenthilnathan Balasubramanian

IPC: G08G5/00 ,  G06F16/29 ,  G08G5/04

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.

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.

Inventor： Saravanakumar Gurusamy ,  Madhava Gadicheria ,  Jayasenthilnathan Balasubramanian

IPC: B60L53/60 ,  H02J7/00 ,  B60L58/12

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.

公开(公告)号：US20210383704A1

公开(公告)日：2021-12-09

申请号：US16941246

申请日：2020-07-28

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Jayasenthilnathan B. ,  Saravanakumar Gurusamy ,  Madhava Gadicherla

IPC: G08G5/00 ,  B64C39/02 ,  H04W4/40

Abstract: Methods and systems for providing off-board recharge station information for an urban air mobility (UAM) vehicle flying on an intended trip. The method includes displaying a map showing the UAM vehicle at a current location, the intended trip, and an endurance line that represents an extent of the available UAM charge. The method retrieves recharge station information including a station name, location, number of recharge ports at the station, and a compatibility type for each of the recharge ports. The method identifies recharge stations that are compatible with the UAM vehicle and can be reached from the intended trip with the UAM available charge, and also updates information associated with the identified recharge stations responsive to a received real-time status update. The method visually depicts the identified recharge stations and visually distinguishes an identified recharge station having a shortest path deviation from the intended trip.

公开(公告)号：US10887451B2

公开(公告)日：2021-01-05

申请号：US16173349

申请日：2018-10-29

Applicant: Honeywell International Inc.

Inventor： Vivek Kumar Pandey ,  Supriya Mallick ,  Saravanakumar Gurusamy

IPC: H04W4/10 ,  H04M3/12 ,  H04M3/20 ,  H04B7/185 ,  G06F3/041

Abstract: A method and system provide a backup push-to-talk (PTT) function for a transmitter in a stuck microphone condition. The method determines whether a stuck microphone condition exists in the transmitter, and if the stuck microphone condition exists, the method alerts a user that the stuck microphone condition exists. The method then enables a backup PTT interface for the transmitter such that a backup PTT button is available to the user to activate the backup PTT function. The method alerts the user when the backup PTT function is activated, and sends a message to a receiver after the backup PTT button is engaged by the user.

公开(公告)号：US20180238996A1

公开(公告)日：2018-08-23

申请号：US15439158

申请日：2017-02-22

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Saravanakumar Gurusamy ,  Madhava Gadicherla ,  Jayasenthilnathan B ,  Roger W Burgin

IPC: G01S7/24 ,  G09G5/36 ,  G09G5/02 ,  G01S13/95 ,  G01S7/00 ,  G08G5/00

CPC classification number: G01S7/24 ,  G01C23/00 ,  G01S7/003 ,  G01S7/062 ,  G01S7/22 ,  G01S7/52036 ,  G01S7/52071 ,  G01S13/953 ,  G01W1/00 ,  G06F3/0484 ,  G08G5/0008 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/0052 ,  G08G5/0091 ,  G09G5/02 ,  G09G2320/0666 ,  G09G2380/12

Abstract: A method for presenting weather information onboard an aircraft is provided. The method obtains a first set of weather data from aircraft onboard radar system; obtains a second set of weather data from external sources including one or more external aircraft, a satellite, a remote server, and a ground-based weather station, wherein the communication device is compatible a communication protocol for the external sources, and wherein the communication protocol comprises at least one of a datalink communication protocol, a satellite communication protocol, a very high frequency (VHF) radio communication protocol, and a transponder communication protocol; and presents graphical elements comprising a first set of graphical elements associated with the first set of weather data and a second set of graphical elements associated with the second set of weather data, wherein the second set of graphical elements include visual characteristics distinguishable from the first set of graphical elements.

公开(公告)号：US09355567B2

公开(公告)日：2016-05-31

申请号：US13962669

申请日：2013-08-08

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Kiran Gopala Krishna ,  Saravanakumar Gurusamy ,  Vishnu Vardhan Reddy Annapureddy

IPC: G08G5/04 ,  B64C25/44 ,  G08G5/00 ,  G08G5/06

CPC classification number: G08G5/04 ,  B64C25/44 ,  G08G5/0021 ,  G08G5/065

Abstract: A system and method display a hazard free area around an aircraft that is modified to alert a pilot if a threshold distance between a detected object and the aircraft is reached. The modification may include, for example, altering the size of the hazard free area and its color. Additional information that may be displayed includes distance to the object, width of the hazard free area, stopping distance of the aircraft, and a route to avoid the object.

Abstract translation: 系统和方法显示飞机周围的无危险区域，如果达到检测到的物体与飞行器之间的阈值距离，该飞机被修改以警告飞行员。 该修改可以包括例如改变无危险区域的尺寸及其颜色。 可能显示的附加信息包括到物体的距离，无危险区域的宽度，飞机的停止距离以及避开物体的路线。

公开(公告)号：US11733712B2

公开(公告)日：2023-08-22

申请号：US16999525

申请日：2020-08-21

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Saravanakumar Gurusamy ,  Kantha Chikkegowda ,  Ivan Wyatt

IPC: G05D1/06 ,  G08G5/00 ,  G01C23/00 ,  G05D1/10 ,  B64D31/06

CPC classification number: G05D1/0661 ,  B64D31/06 ,  G01C23/00 ,  G05D1/106 ,  G08G5/0065

Abstract: Methods and systems for generating a vertical situation display for a noise abatement departure procedure (NADP). Other NADP relevant displays are also disclosed including display of NADP parameters on altitude tape and primary flight displays, an NADP bug on an engine display and NADP status annunciations. The methods and systems include receiving NADP parameters entered into a flight management system (FMS) on a user interface of the aircraft system. The NADP parameters include: an initial altitude at which take-off thrust should be reduced to NADP thrust, an acceleration altitude at which the aircraft should begin accelerating to a final take-off speed whilst maintaining the NADP thrust, a climb excitement altitude at which a speed target is changed to the final take-off speed whilst maintaining the NADP thrust, and an end altitude at which the NADP should be exited. The methods and systems include generating a vertical situation display for a display device of the aircraft system indicating the NADP parameters on a flight path indication.

公开(公告)号：US20220004202A1

公开(公告)日：2022-01-06

申请号：US16999525

申请日：2020-08-21

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Saravanakumar Gurusamy ,  Kantha Chikkegowda ,  Ivan Wyatt

IPC: G05D1/06 ,  B64D31/06 ,  G08G5/00 ,  G05D1/10

Abstract: Methods and systems for generating a vertical situation display for a noise abatement department procedure (NADP). Other NADP relevant displays are also disclosed including display of NADP parameters on altitude tape and primary flight displays, an NADP bug on an engine display and NADP status annunciations. The methods and systems include receiving NADP parameters entered into a flight management system (FMS) on a user interface of the aircraft system. The NADP parameters include: an initial altitude at which take-off thrust should be reduced to NADP thrust, an acceleration altitude at which the aircraft should begin accelerating to a final take-off speed whilst maintaining the NADP thrust, a climb excitement altitude at which a speed target is changed to the final take-off speed whilst maintaining the NADP thrust, and an end altitude at which the NADP should be exited. The methods and systems include generating a vertical situation display for a display device of the aircraft system indicating the NADP parameters on a flight path indication.

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

IPC: G08G5/04 ,  B64D43/00 ,  G01C23/00 ,  G08G5/00

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.

公开(公告)号：US20200049500A1

公开(公告)日：2020-02-13

申请号：US16057418

申请日：2018-08-07

Applicant: Honeywell International Inc.

Inventor： Madhava Gadicherla ,  Saravanakumar Gurusamy ,  Jayasenthilnathan B

IPC: G01C5/06 ,  G01C5/00 ,  G08G5/00

Abstract: The disclosure is directed to techniques that use a data communication system such as ADS-B to provide an output to alert an aircraft operator of an incorrect barometric pressure setting for a pressure altimeter, and provide the correct altimeter setting. For example, the system may compile the ADS-B Out data from other aircraft operating near a first aircraft to provide the barometric pressure setting in use by the other aircraft. A system of this disclosure may identify the altimeter setting used by majority of the other aircraft in a region of airspace. If a first aircraft's current barometric altimeter setting is different from the setting of the majority of the nearby aircraft, then the system may generate an output to alert the operator of the first aircraft of a potential incorrect altimeter setting as well as provide a suggested barometric altimeter setting.