Patents by Inventor Petr Krupansky
Petr Krupansky 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).
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Patent number: 11514772Abstract: A generator set monitoring and control system includes a generator set located in a first location, an on-site controller located near the first location, and a remote display, located in a second location. The remote display is configured to send instructions to at least one of the generator set and on-site controller, receive genset operation outputs from the on-site controller, and display genset operation outputs.Type: GrantFiled: March 22, 2021Date of Patent: November 29, 2022Assignee: ComAp a.s.Inventors: Jan Holub, P{hacek over (r)}emysl B{hacek over (e)}la{hacek over (s)}ka, Aleksandar Popović, Jiri Dunovsky, Petr Krupanský
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Publication number: 20220207269Abstract: A mobile device includes a memory, a processor in communication with the memory, a camera, a display, and an interactive diagnostic module. The interactive diagnostic module is configured to obtain image data from the camera. The image data is associated with at least one of a genset and a genset controller, and the image data includes at least one reference point from the at least one of the generator set and the generator set controller. The interactive diagnostic module is also configured to render the image data on the display and generate augmented reality feature(s). The augmented reality feature(s) is generated based on the at least one reference point. Additionally, the interactive diagnostic module is configured to create a user interface with the rendered image data and the augmented reality feature(s) integrated with the image data.Type: ApplicationFiled: December 31, 2020Publication date: June 30, 2022Inventors: Jan Holub, Jose Grenard, Petr Krupanský
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Publication number: 20210209926Abstract: A generator set monitoring and control system includes a generator set located in a first location, an on-site controller located near the first location, and a remote display, located in a second location. The remote display is configured to send instructions to at least one of the generator set and on-site controller, receive genset operation outputs from the on-site controller, and display genset operation outputs.Type: ApplicationFiled: March 22, 2021Publication date: July 8, 2021Inventors: Jan Holub, Premysl Balaska, Aleksandar Popovic, Jiri Dunovsky, Petr Krupanský
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Patent number: 10957181Abstract: A generator set monitoring and control system includes a generator set located in a first location, an on-site controller located near the first location, and a remote display, located in a second location. The remote display is configured to send instructions to at least one of the generator set and on-site controller, receive genset operation outputs from the on-site controller, and display genset operation outputs.Type: GrantFiled: November 7, 2019Date of Patent: March 23, 2021Assignee: ComAp a.s.Inventors: Jan Holub, P{hacek over (r)}emysl B{hacek over (e)}la{hacek over (s)}ka, Aleksandar Popović, Jiri Dunovský, Petr Krupanský
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Patent number: 9864368Abstract: A method for calculating vertical trajectory values is provided. The method obtains aircraft performance data for a particular aircraft and atmospheric condition data associated with an air route; calculates a cost-efficient vertical trajectory for the air route, based on the aircraft performance data and the atmospheric condition data, wherein the cost-efficient vertical trajectory comprises a plurality of altitude values for minimizing cost for the particular aircraft during travel of the air route; obtains an altitude consistency threshold; and adjusts the cost-efficient vertical trajectory using the altitude consistency parameter, to create an optimized vertical trajectory for the aircraft route.Type: GrantFiled: February 8, 2016Date of Patent: January 9, 2018Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Petr Krupansky, Jaroslav Jonak, Vitezslav Cip
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Publication number: 20170227955Abstract: A method for calculating vertical trajectory values is provided. The method obtains aircraft performance data for a particular aircraft and atmospheric condition data associated with an air route; calculates a cost-efficient vertical trajectory for the air route, based on the aircraft performance data and the atmospheric condition data, wherein the cost-efficient vertical trajectory comprises a plurality of altitude values for minimizing cost for the particular aircraft during travel of the air route; obtains an altitude consistency threshold; and adjusts the cost-efficient vertical trajectory using the altitude consistency parameter, to create an optimized vertical trajectory for the aircraft route.Type: ApplicationFiled: February 8, 2016Publication date: August 10, 2017Inventors: Petr Krupansky, Jaroslav Jonak, Vitezslav Cip
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Patent number: 9711055Abstract: This disclosure is directed to systems and methods for smart transitioning between aircraft trajectory management modes. In one example, a system is configured to track a speed of a target aircraft in flight ahead of an own aircraft on which the system is positioned. The system is further configured to determine whether the target aircraft has maintained a rate of change in speed within a selected range of variation in change of speed, for a selected period of time. The system is further configured to enable an activation of a merging trajectory management mode of the own aircraft in response to determining that the own aircraft is in a trajectory management mode transition airspace and that the target aircraft has maintained the rate of change in speed within the selected range of variation in change of speed, for the selected period of time.Type: GrantFiled: June 8, 2015Date of Patent: July 18, 2017Assignee: Honeywell International Inc.Inventors: Petr Vesely, Petr Krupansky, Pavel Klang, Jaroslav Jonak, Michal Polansky
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Publication number: 20160358481Abstract: This disclosure is directed to systems and methods for smart transitioning between aircraft trajectory management modes. In one example, a system is configured to track a speed of a target aircraft in flight ahead of an own aircraft on which the system is positioned. The system is further configured to determine whether the target aircraft has maintained a rate of change in speed within a selected range of variation in change of speed, for a selected period of time. The system is further configured to enable an activation of a merging trajectory management mode of the own aircraft in response to determining that the own aircraft is in a trajectory management mode transition airspace and that the target aircraft has maintained the rate of change in speed within the selected range of variation in change of speed, for the selected period of time.Type: ApplicationFiled: June 8, 2015Publication date: December 8, 2016Inventors: Petr Vesely, Petr Krupansky, Pavel Klang, Jaroslav Jonak, Michal Polansky
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Patent number: 9377324Abstract: Methods and apparatus are provided for selectively balancing pilot workload. The apparatus comprises a display device configured to display a user interface (UI) and a processor. The processor is configured to determine a state of the pilot and/or a state of the aircraft, prepare modification to the UI based in part on the state of the pilot and/or the state of the aircraft such that the modification adds one or more command icons without obscuring, without removing, and without replacing any information item on the display, and to execute the modification.Type: GrantFiled: September 27, 2010Date of Patent: June 28, 2016Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Petr Krupansky, Jiri Vasek, Larry Karl Ball
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Patent number: 9020681Abstract: A method of displaying navigation limits for a planned travel route of a vehicle is presented here. The method calculates estimated navigation limits for the vehicle using an onboard subsystem of the vehicle, where the estimated navigation limits represent self-assessed navigation accuracy of the vehicle relative to the planned travel route. Contracted navigation limits are acquired for the vehicle, where the contracted navigation limits represent specified navigation accuracy of the vehicle, relative to the planned travel route, as mandated by a third party navigation controller. A navigation display is rendered on an onboard display element such that it includes graphical representations of the planned travel route, at least one of the estimated navigation limits, and at least one of the contracted navigation limits.Type: GrantFiled: June 8, 2010Date of Patent: April 28, 2015Assignee: Honeywell International Inc.Inventors: Petr Krupansky, Jiri Vasek, Pavel Kolcarek, Tomas Neuzil, John A. Wise
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Patent number: 8321069Abstract: Provided are methods and systems for the automatic assessment and presentation of data on a display device that describes the operational impact on mission critical parameters resulting from a change in a vehicle's mission plan. The change in mission plan may be inputted manually by the vehicle operator but may also be received electronically and automatically over a data up link from an outside authority.Type: GrantFiled: March 26, 2009Date of Patent: November 27, 2012Assignee: Honeywell International Inc.Inventors: Jiri Vasek, Pavel Kolcarek, Petr Krupansky
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Patent number: 8311780Abstract: 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: GrantFiled: April 23, 2009Date of Patent: November 13, 2012Assignee: Honeywell International Inc.Inventors: Petr Krupansky, Tomas Neuzil, Eva Gelnarova, Martin Herodes, Jiri Svoboda
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Publication number: 20120257684Abstract: In a first embodiment, the method includes, but is not limited to receiving a first instruction from a first party who is associated with control of the aircraft, to transmit an initial non-verbal communication to a second party who is associated with control of the aircraft. The method further includes transmitting the initial non-verbal communication to the second party over the digital communication link. The method further includes receiving a second instruction from the second party to transmit a non-verbal response to the initial non-verbal communication. The method still further includes transmitting the non-verbal response to the first party over the digital communication link. Either the initial non-verbal communication or the non-verbal response includes data that can be used to derive a text message and a graphic image, and wherein the graphic image includes information that is available to only one of the first party and the second party.Type: ApplicationFiled: April 8, 2011Publication date: October 11, 2012Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Jiri Vasek, Petr Krupansky, Pavel Kolcarek, Jaroslav Jonak
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Publication number: 20120078450Abstract: Methods and systems are provided for executing a single continuous altitude change by an aircraft to cruise altitude using an electronic flight bag via a flight management system. The method comprises the determination of an altitude change in a flight plan during the cruise phase of the flight plan. Based on the altitude change and a mathematical model of the aircraft an optimum vertical trajectory profile or the aircraft is determined from which an angle of attack (AOA) and a thrust is derived to achieve the optimum vertical trajectory. From the AOA and the thrust, the required aircraft control variables are determined that may be applied to the engines and the control surface actuators of the aircraft.Type: ApplicationFiled: September 27, 2010Publication date: March 29, 2012Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Stephane Marche, Petr Krupansky, Tomas Neuzil, George Papageorgiou, Jean-Luc Derouineau
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Publication number: 20120075123Abstract: A system and method are provided for intelligently managing the avionics display, information, and controls to more evenly distribute pilot task loads and/or automatically configure/reconfigure displays during flights.Type: ApplicationFiled: August 9, 2011Publication date: March 29, 2012Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Claudia Keinrath, Michael Christian Dorneich, Stephen Whitlow, Bretislav Passinger, Jiri Vasek, Petr Krupansky
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Publication number: 20120078445Abstract: Methods and apparatus are provided for selectively balancing pilot workload. The apparatus comprises a display device configured to display a user interface (UI) and a processor. The processor is configured to determine a state of the pilot and/or a state of the aircraft, prepare modification to the UI based in part on the state of the pilot and/or the state of the aircraft such that the modification adds one or more command icons without obscuring, without removing, and without replacing any information item on the display, and to execute the modification.Type: ApplicationFiled: September 27, 2010Publication date: March 29, 2012Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Petr Krupansky, Jiri Vasek, Larry Karl Ball
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Publication number: 20110301842Abstract: A method of displaying navigation limits for a planned travel route of a vehicle is presented here. The method calculates estimated navigation limits for the vehicle using an onboard subsystem of the vehicle, where the estimated navigation limits represent self-assessed navigation accuracy of the vehicle relative to the planned travel route. Contracted navigation limits are acquired for the vehicle, where the contracted navigation limits represent specified navigation accuracy of the vehicle, relative to the planned travel route, as mandated by a third party navigation controller. A navigation display is rendered on an onboard display element such that it includes graphical representations of the planned travel route, at least one of the estimated navigation limits, and at least one of the contracted navigation limits.Type: ApplicationFiled: June 8, 2010Publication date: December 8, 2011Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Petr Krupansky, Jiri Vasek, Pavel Kolcarek, Tomas Neuzil, John A. Wise
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Publication number: 20100274542Abstract: 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: ApplicationFiled: April 23, 2009Publication date: October 28, 2010Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Petr Krupansky, Tomas Neuzil, Eva Gelnarova, Martin Herodes, Jiri Svoboda
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Publication number: 20100271239Abstract: A method of displaying on a display (104) of a vehicle includes presenting atmospheric uncertainties, including collecting (806) weather data (400), obtaining (802) weather information recorded along trajectories (203, 205, 207) of at least one vehicle (202, 204, 206), the weather information having a higher importance proportional to the portion of the trajectory (210, 216, 218) most recently traversed, creating (804) a threshold uncertainty map (300) of the weather information obtained along the trajectories (203, 205, 207), joining (808) the threshold uncertainty map (300) with the weather data (400), combining (810) an atmospheric field (400) with the joined threshold uncertainty map and the weather data, and displaying (812) the combined atmospheric field, threshold uncertainty map, and weather data on a display (104). The weather data may be recent, historical, or forecasted and may be modified to be a stochastic model.Type: ApplicationFiled: April 28, 2009Publication date: October 28, 2010Applicant: Honeywell International Inc.Inventors: Pavel Kolcarek, Petr Krupansky, Jiri Svoboda
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Patent number: RE48962Abstract: A method for calculating vertical trajectory values is provided. The method obtains aircraft performance data for a particular aircraft and atmospheric condition data associated with an air route; calculates a cost-efficient vertical trajectory for the air route, based on the aircraft performance data and the atmospheric condition data, wherein the cost-efficient vertical trajectory comprises a plurality of altitude values for minimizing cost for the particular aircraft during travel of the air route; obtains an altitude consistency threshold; and adjusts the cost-efficient vertical trajectory using the altitude consistency parameter, to create an optimized vertical trajectory for the aircraft route.Type: GrantFiled: January 9, 2020Date of Patent: March 8, 2022Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Petr Krupansky, Jaroslav Jonak, Vitezslav Cip