Patents by Inventor Eva Gelnarova

Eva Gelnarova 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).

  • 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: 11210959
    Abstract: In some examples, a system that mounts on a vehicle includes a transceiver configured to transmit a first surveillance message including a first value for a quality parameter, wherein the first value indicates a first level of integrity or accuracy for the first surveillance message. The transceiver is also configured to receive a reply message to the first surveillance message. The system also includes processing circuitry configured to determine a second value for the quality parameter in response to the transceiver receiving the reply message, wherein the second quality parameter indicates a second level of integrity or accuracy for surveillance messages transmitted by the transceiver, and wherein the second level of integrity or accuracy is higher than the first level. The transceiver is configured to transmit a second surveillance message including the second value for the quality parameter in response to the processing circuitry determining the second quality parameter.
    Type: Grant
    Filed: July 19, 2019
    Date of Patent: December 28, 2021
    Assignee: Honeywell International S.R.O.
    Inventors: Petr Casek, Eva Gelnarova
  • Publication number: 20210090445
    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: Application
    Filed: September 20, 2019
    Publication date: March 25, 2021
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Karol Molnar, Eva Gelnarova, Kalimulla Khan, Srihari Jayathirtha, Raghu Shamasundar, Visakh S, Chavdar Kirov, Ivan Markov
  • Publication number: 20210005096
    Abstract: In some examples, a system that mounts on a vehicle includes a transceiver configured to transmit a first surveillance message including a first value for a quality parameter, wherein the first value indicates a first level of integrity or accuracy for the first surveillance message. The transceiver is also configured to receive a reply message to the first surveillance message. The system also includes processing circuitry configured to determine a second value for the quality parameter in response to the transceiver receiving the reply message, wherein the second quality parameter indicates a second level of integrity or accuracy for surveillance messages transmitted by the transceiver, and wherein the second level of integrity or accuracy is higher than the first level. The transceiver is configured to transmit a second surveillance message including the second value for the quality parameter in response to the processing circuitry determining the second quality parameter.
    Type: Application
    Filed: July 19, 2019
    Publication date: January 7, 2021
    Inventors: Petr Casek, Eva Gelnarova
  • Patent number: 8311780
    Abstract: A method and software program for providing a weather prediction of atmospheric parameters for an aircraft, includes collecting (202) at least one of a statistical description of the weather forecast or the historical weather data, processing (210) current atmospheric data received from sensors on-board the aircraft, forming (230) modeled data based on the processed current atmospheric data and the at least one of a statistical description of the weather forecast or the historical weather data, blending (250) the modeled data with the at least one of a statistical description of the weather forecast or the historical weather data, and predicting (270) atmospheric parameters based on the blending step.
    Type: Grant
    Filed: April 23, 2009
    Date of Patent: November 13, 2012
    Assignee: Honeywell International Inc.
    Inventors: Petr Krupansky, Tomas Neuzil, Eva Gelnarova, Martin Herodes, Jiri Svoboda
  • Publication number: 20100274542
    Abstract: A method and software program for providing a weather prediction of atmospheric parameters for an aircraft, includes collecting (202) at least one of a statistical description of the weather forecast or the historical weather data, processing (210) current atmospheric data received from sensors on-board the aircraft, forming (230) modeled data based on the processed current atmospheric data and the at least one of a statistical description of the weather forecast or the historical weather data, blending (250) the modeled data with the at least one of a statistical description of the weather forecast or the historical weather data, and predicting (270) atmospheric parameters based on the blending step.
    Type: Application
    Filed: April 23, 2009
    Publication date: October 28, 2010
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Petr Krupansky, Tomas Neuzil, Eva Gelnarova, Martin Herodes, Jiri Svoboda