Patents by Inventor Kalimulla Khan

Kalimulla Khan has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Publication number: 20240104483
    Abstract: Disclosed are methods and systems for converting data from an external system to data to be used by an internal system. For instance, a method may include receiving at least one user selection from a list of domains for executing at least one task, determining one or more data requirements corresponding to the at least one user selection, in response to determining the one or more data requirements, retrieving data from one or more external systems, converting the retrieved data based on the one or more data requirements, the converting including extracting data from the retrieved data based on the one or more data requirements, validating the extracted data, the validating including determining that the extracted data meets or exceeds a primary data requirement threshold, and outputting the validated extracted data to a data model for use by an internal system to execute the at least one task.
    Type: Application
    Filed: September 28, 2022
    Publication date: March 28, 2024
    Inventors: Kalimulla Khan, Srihari Jayathirtha, Wade Lindsey, Afzal Hussaini Wiquar, Venkata Pradeep Kolla, Krishna Pillutla
  • Publication number: 20240078912
    Abstract: A method for optimizing a transit of a vehicle with an estimated time of arrival to a destination includes, during the transit of the vehicle, performing, by one or more processors located off-board the vehicle, operations including: receiving data impacting the estimated time of arrival of the vehicle to the destination; optimizing, based on the received data, a parameter for an operation of the vehicle to maintain the estimated time of arrival to the destination within a threshold time, wherein the optimizing the parameter includes changing one or more of a speed or a route of the vehicle; and sending the optimized parameter to the vehicle.
    Type: Application
    Filed: November 18, 2022
    Publication date: March 7, 2024
    Inventors: Kalimulla KHAN, Manish GOSWAMI, Raghu SHAMASUNDAR
  • Patent number: 11893907
    Abstract: Systems and methods are disclosed for evidence-based training of aircraft operators. For example, a computer-implemented method may include: analyzing aircraft flight data indicative of actions performed by an aircraft operator in operating aircraft, to thereby determine an assessment of a performance of the aircraft operator in operating aircraft; based on the assessment, determining a training scenario to be presented to the aircraft operator via a training simulator as part of training for the aircraft operator; providing, to the training simulator, information indicative of the determined training scenario; receiving, from the training simulator, training flight data indicative of actions performed by the aircraft operator during a simulation of the scenario using the training simulator; and based on the training flight data and the assessment, determining an evaluation of the training for the aircraft operator.
    Type: Grant
    Filed: September 10, 2020
    Date of Patent: February 6, 2024
    Assignee: Honeywell International Inc.
    Inventors: Raghu Shamasundar, Mahesh Sivaratri, Kalimulla Khan, Srihari Jayathirtha
  • Publication number: 20240021086
    Abstract: A flight deck system is configured to: receive a data model populated with flight data obtained while performing a core avionics function; receive configuration information from an external source that identifies a specific plurality of flight data items to extract from the data model; extract from the data model data values for the specific plurality of flight data items identified in the configuration information; generate an optical code that encodes the extracted data values; generate an HMI display that provides a selectable link for causing the optical code to be displayed in the aircraft; cause the HMI display to be display on an aircraft display; and cause the optical code to be displayed on an aircraft display responsive to selection of the selectable link; wherein the optical code provides encoded data values corresponding to the specific plurality of flight data items for decoding and display by a mobile device.
    Type: Application
    Filed: September 19, 2022
    Publication date: January 18, 2024
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Raghu Shamasundar, Kalimulla Khan, Sreenivasan Govindillam, Nathan Krishna Moorthy
  • Publication number: 20240021090
    Abstract: Methods and systems for providing platform agnostic flight management data access for a flight management system (FMS) of an aircraft have been developed. First, a configuration file is loaded to a configuration database. The configuration file is for a data format of an external data source from the aircraft. Upon receiving a data access request from a user for external data from the external data source, downloading the configuration file is downloaded to an FMS data formatter. The configuration file is parsed with a data processor component of the FMS data formatter to update a rule set. The FMS data formatter receives an external data file from an application programing interface (API) of the external data source. The external data file is parsed with a rule engine of the FMS data formatter using the updated rule set. A flight plan file is generated with the FMS data formatter using the parsed external data file and sent to the FMS on the aircraft.
    Type: Application
    Filed: October 3, 2022
    Publication date: January 18, 2024
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Subhransu Sahoo, Kalimulla Khan, Raghu Shamasundar, Kirupakar J., Robert Son
  • Patent number: 11830370
    Abstract: Methods, systems, and apparatuses provided for predicting a Mach Tuck situation. The method includes generating a flight plan for the aircraft of at least one supersonic flight path segment in accordance with a flight plan criteria entered via an input interface wherein the aircraft traverses at least one supersonic flight path segment at an airspeed approaching or exceeding a supersonic airspeed; predicting based on an impact of a weather condition forecast to occur at a selected region of the supersonic flight path segment while the aircraft is operating at the airspeed approaching or exceeding the supersonic speed that an overpressure condition will occur causing an aerodynamic effect to the aircraft that results in the aircraft exceeding an operating limitation causing the Mach Tuck situation; and modifying the flight plan in a manner to lessen the impact of the weather condition forecast to occur to prevent the Mach Tuck situation.
    Type: Grant
    Filed: October 8, 2021
    Date of Patent: November 28, 2023
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Paulo da Costa Mello, Anil Kumar Songa, Kalimulla Khan, Kantha Chikkegowda
  • Publication number: 20230365270
    Abstract: Disclosed are methods, systems, and one or more computer-readable mediums for providing, by an integrated flight deck (IFD) networked computing system, data acquisition for generating a plurality of inflight operation insights, the IFD networked computing system comprising: a presentation platform, a plurality of framework components, a software development kit (SDK) framework, and one or more user interface libraries configured to develop a plurality of applications from the presentation platform and add one or more additional SDKs and/or libraries to the presentation platform; aggregating, by an orchestrator of the SDK framework, a plurality of data sources to fuse data from the plurality of data sources and create a data packet comprising real-time flight data; generating, the plurality of inflight operation insights by analyzing a plurality of key performance indicators of the created data packet; and assessing a flight parameter based on the generated inflight operation insights.
    Type: Application
    Filed: September 9, 2022
    Publication date: November 16, 2023
    Inventors: KIRUPAKAR JANAKIRAMAN, KALIMULLA KHAN, Phillip TOEWS, Ramkumar RAJENDRAN, Manish GOSWAMI, SRIHARI JAYATHIRTHA
  • Patent number: 11790789
    Abstract: Methods and systems are provided for guiding or otherwise assisting operation of an aircraft en route to an airport. One method involves identifying a reference point in advance of a runway, dynamically determining a gliding vertical trajectory for the aircraft en route to the reference point based at least in part on a current altitude of the aircraft at a current aircraft location and gliding characteristics of the aircraft, and providing a graphical indication of a difference between a predicted altitude of the aircraft at a location corresponding to the reference point resulting from the gliding vertical trajectory and an altitude criterion associated with the reference point. The graphical indication of the difference dynamically updates as the aircraft travels.
    Type: Grant
    Filed: August 3, 2020
    Date of Patent: October 17, 2023
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Kiran Venkataramana, Kalimulla Khan, Raghu Shamasundar
  • Patent number: 11763684
    Abstract: A joint-decision making system for a vehicle operator and a dispatcher is disclosed, comprising: a vehicle operator engine implemented on a vehicle system configured to: detect a trigger event condition; retrieve vehicle information relevant to the event trigger condition; receive additional information relevant to the event trigger condition; generate a suggested response based on the trigger event condition, retrieved vehicle information, and received additional information; display the suggested response on a graphical user interface of the vehicle operator engine; and transmit the trigger event condition, vehicle information, and suggested response to a dispatcher engine; and the dispatcher engine implemented on a ground system configured to: receive the event trigger condition, vehicle information, and suggested response from the vehicle operator engine; retrieve the additional information relevant to the event trigger condition; and display the suggested response on a graphical user interface of the dis
    Type: Grant
    Filed: February 22, 2021
    Date of Patent: September 19, 2023
    Assignee: Honeywell International Inc.
    Inventors: Yi Zhong, Raghu Shamasundar, Dan Li, Ramkumar Rajendran, Kalimulla Khan, Visakh Sivadasan
  • Publication number: 20230237404
    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.
    Type: Application
    Filed: January 21, 2022
    Publication date: July 27, 2023
    Inventors: SRIHARI JAYATHIRTHA, Kalimulla KHAN, Jayasenthilnathan BALASUBRAMANIAN, Yogiraj Dattaram MORE
  • Publication number: 20230215281
    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.
    Type: Application
    Filed: February 17, 2022
    Publication date: July 6, 2023
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Subhransu Sahoo, Kalimulla Khan, Raghu Shamasundar, Sreenivasan Govindillam, Richard Snyder
  • Publication number: 20230177966
    Abstract: Disclosed are methods and systems for bi-directional communication between one or more vehicles and a cloud based computing system. For instance, a method may include processing, by a first digital twin of the cloud based computing system, a first request received from and/or sent to a gateway unit associated with a first vehicle, the request comprising data related to one or more vehicle operations; validating, by an avionics data processing service (ADPS) in communication with the gateway unit, the first request against an operational parameter corresponding to the one or more vehicle operations; upon validating the first request, matching, by the ADPS, the operational parameter with a flight operation; and upon matching the operational parameter with the flight operation, inserting, by the ADPS, a modified flight operation into the flight management system of the vehicle.
    Type: Application
    Filed: June 22, 2022
    Publication date: June 8, 2023
    Applicant: Honeywell International Inc.
    Inventors: Kirupakar JANAKIRAMAN, Kalimulla KHAN, Todd MATHIS, Ramkumar RAJENDRAN, Srihari JAYATHIRTHA, Subhransu SAHOO
  • Publication number: 20230150690
    Abstract: Disclosed are systems, methods, and non-transitory computer-readable medium for providing a safe landing for a vehicle. The method may include: displaying, on one or more displays, a 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.
    Type: Application
    Filed: January 7, 2022
    Publication date: May 18, 2023
    Inventors: Jayasenthilnathan BALASUBRAMANIAN, Byron BIRKEDAHL, Kalimulla KHAN, Srihari JAYATHIRTHA
  • Publication number: 20230062812
    Abstract: Methods, systems, and apparatuses provided for predicting a Mach Tuck situation. The method includes generating a flight plan for the aircraft of at least one supersonic flight path segment in accordance with a flight plan criteria entered via an input interface wherein the aircraft traverses at least one supersonic flight path segment at an airspeed approaching or exceeding a supersonic airspeed; predicting based on an impact of a weather condition forecast to occur at a selected region of the supersonic flight path segment while the aircraft is operating at the airspeed approaching or exceeding the supersonic speed that an overpressure condition will occur causing an aerodynamic effect to the aircraft that results in the aircraft exceeding an operating limitation causing the Mach Tuck situation; and modifying the flight plan in a manner to lessen the impact of the weather condition forecast to occur to prevent the Mach Tuck situation.
    Type: Application
    Filed: October 8, 2021
    Publication date: March 2, 2023
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Paulo da Costa Mello, Anil Kumar Songa, Kalimulla Khan, Kantha Chikkegowda
  • Publication number: 20220406195
    Abstract: Disclosed are methods, systems, and one or more computer-readable mediums for receiving, at an edge device from an external server, a rules database comprising a set of rules; receiving, by the edge device, first data from at least one device; processing, by the edge device, the received first data by comparing the received data to each rule among the set of rules; identifying a first triggering event in response to detecting a match between the received data and a rule of the rules database; and outputting an alert corresponding to the first triggering event.
    Type: Application
    Filed: March 25, 2022
    Publication date: December 22, 2022
    Inventors: Kirupakar JANAKIRAMAN, Nayyar Azam Khan RAO, Kalimulla KHAN, Prasanna M R H, Ramkumar RAJENDRAN, Deepavali Dinkarrao DESAI, Aloke ROY
  • Publication number: 20220382299
    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.
    Type: Application
    Filed: April 27, 2022
    Publication date: December 1, 2022
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Raghu Shamasundar, Subhransu Sahoo, Richard Snyder, Kalimulla Khan, Ramkumar Rajendran
  • Publication number: 20220130261
    Abstract: A joint-decision making system for a vehicle operator and a dispatcher is disclosed, comprising: a vehicle operator engine implemented on a vehicle system configured to: detect a trigger event condition; retrieve vehicle information relevant to the event trigger condition; receive additional information relevant to the event trigger condition; generate a suggested response based on the trigger event condition, retrieved vehicle information, and received additional information; display the suggested response on a graphical user interface of the vehicle operator engine; and transmit the trigger event condition, vehicle information, and suggested response to a dispatcher engine; and the dispatcher engine implemented on a ground system configured to: receive the event trigger condition, vehicle information, and suggested response from the vehicle operator engine; retrieve the additional information relevant to the event trigger condition; and display the suggested response on a graphical user interface of the dis
    Type: Application
    Filed: February 22, 2021
    Publication date: April 28, 2022
    Inventors: Yi ZHONG, Raghu SHAMASUNDAR, Dan LI, Ramkumar RAJENDRAN, Kalimulla KHAN, Visakh SIVADASAN
  • Patent number: 11270593
    Abstract: Methods and systems are provided for optimization of an aircraft flight trajectory with shortcuts. The method comprises retrieving an active flight plan stored in a flight management system (FMS) and identifying a potential shortcut with a shortcut advisor tool. The FMS monitors the location of the aircraft with respect to an identified start point of the potential shortcut. Prior to the aircraft's arrival at the identified start point, current key performance indicators (KPI) of the shortcut are evaluated with the shortcut advisor tool. The aircrew is alerted to the potential shortcut along with a preview of the performance of the aircraft upon accepting the potential shortcut. The aircrew may accept the addition of the potential shortcut to the flight plan and request approval of the shortcut by air traffic control (ATC). The active flight plan is updated with the shortcut upon approval from the ATC.
    Type: Grant
    Filed: September 20, 2019
    Date of Patent: March 8, 2022
    Assignee: Honeywell International Inc.
    Inventors: Karol Molnar, Eva Gelnarova, Kalimulla Khan, Srihari Jayathirtha, Raghu Shamasundar, Visakh S, Chavdar Kirov, Ivan Markov
  • Patent number: D939526
    Type: Grant
    Filed: February 18, 2020
    Date of Patent: December 28, 2021
    Assignee: Honeywell International Inc.
    Inventors: Kalimulla Khan, Ramkumar Rajendran, Subhransu Sahoo, Kirupakar Janakiraman, Bijitha Bg
  • Patent number: D939551
    Type: Grant
    Filed: February 18, 2020
    Date of Patent: December 28, 2021
    Assignee: Honeywell International Inc.
    Inventors: Kalimulla Khan, Ramkumar Rajendran, Subhransu Sahoo, Kirupakar Janakiraman, Bijitha Bg