Patents by Inventor Willard R. True
Willard R. True 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: 10901675Abstract: A method for verifying the integrity, continuity, and availability (ICA) of information displayed on an uncertified display is provided. The method comprises creating, on the high integrity device, application data for display on an uncertified display device; transmitting the application data to the uncertified display device for display; receiving, at the high integrity device from the uncertified display device, a captured image of the display captured using a screen capture feature on the uncertified display device; determining, at the high integrity device, an expected display image; comparing, at the high integrity device, the captured image of the display to the expected display image; identifying, at the high integrity device, a loss of ICA if one or more frames in the captured image fails the comparison with the expected display image; and causing the annunciation of a message indicating the loss of ICA when a loss of ICA is identified.Type: GrantFiled: October 21, 2019Date of Patent: January 26, 2021Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Willard R. True, Richard Berckefeldt, Kalluri R. Sarma
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Patent number: 10901674Abstract: A method in a high integrity device for verifying the integrity, continuity, and availability (ICA) of information displayed on an uncertified display is provided. The method comprises creating, on the high integrity device, application data for display on an uncertified display device; transmitting the application data to the uncertified display device; receiving, at the high integrity device from an optical sensing device, a captured image of the display; determining, at the high integrity device, an expected display image to be displayed on the uncertified display device; comparing, at the high integrity device, the captured image of the display to the expected display image; identifying, at the high integrity device, a loss of ICA if one or more frames in the captured image fails the comparison with the expected display image; and causing the annunciation of a message indicating the loss of ICA when a loss of ICA is identified.Type: GrantFiled: April 23, 2018Date of Patent: January 26, 2021Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Willard R. True, Richard Berckefeldt, Kalluri R. Sarma
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Patent number: 10875762Abstract: An addressable display system configured for use in a mounting adapter configured to mount a personal electronic device (PED) on an aircraft includes a transparent surface configured to overlay the display surface of a PED when the PED is mounted in the mounting adapter wherein the transparent surface includes a region that is uniformly coated with a coating layer that when activated with a select excitation wavelength is configured to emit visible light to annunciate a message indicating a problem with an image displayed on a PED display; a lighting source configured to provide light in at an excitation wavelength; a MEMS (microelectromechanical systems) scanner module that is controllable to write desired symbology for annunciation at different addressable locations on the transparent surface; and an imaging device configured to capture an image of the PED display for an integrity check of data displayed on the PED display.Type: GrantFiled: March 22, 2018Date of Patent: December 29, 2020Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Kalluri R. Sarma, Richard Berckefeldt, Willard R. True
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Patent number: 10810808Abstract: A server system on an aircraft is provided. The server system is configured to allow critical aeronautical information to be displayed on a cockpit display that is not certified for displaying critical aeronautical information. The server system includes an aircraft interface device configured to interface with one or more aeronautical systems on the aircraft to retrieve critical aeronautical information; an application module configured to generate application data for display on the cockpit display wherein the application data includes at least some of the critical aeronautical information; an interface module configured to transmit the application data to the cockpit display for display; and an integrity checking module configured to retrieve image data from an image sensor trained on a display device in the cockpit display and configured to perform an integrity check on the image data from the image sensor.Type: GrantFiled: March 13, 2018Date of Patent: October 20, 2020Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Willard R. True, Richard Berckefeldt, Kalluri R. Sarma
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Patent number: 10636390Abstract: A display integrity system for use in a mounting adapter configured to mount a personal electronic device (PED) on an aircraft is disclosed. The display integrity system includes a transparent surface configured to overlay the display surface of a PED when the PED is mounted in the mounting adapter. The transparent surface includes one or more regions embedded with one or more coating layers that when activated with a select excitation wavelength are configured to emit visible light to annunciate a message indicating a problem with an image displayed on the PED. The display integrity system further includes a lighting source housed in the mounting adapter and configured to provide light in the select excitation wavelength when activated to illuminate the transparent surface and an imaging device mounted in the mounting adapter and configured to capture an image of the PED display for transmission to a server for integrity checking.Type: GrantFiled: March 20, 2018Date of Patent: April 28, 2020Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Kalluri R. Sarma, Richard Berckefeldt, Willard R. True
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Publication number: 20200065044Abstract: A method for verifying the integrity, continuity, and availability (ICA) of information displayed on an uncertified display is provided. The method comprises creating, on the high integrity device, application data for display on an uncertified display device; transmitting the application data to the uncertified display device for display; receiving, at the high integrity device from the uncertified display device, a captured image of the display captured using a screen capture feature on the uncertified display device; determining, at the high integrity device, an expected display image; comparing, at the high integrity device, the captured image of the display to the expected display image; identifying, at the high integrity device, a loss of ICA if one or more frames in the captured image fails the comparison with the expected display image; and causing the annunciation of a message indicating the loss of ICA when a loss of ICA is identified.Type: ApplicationFiled: October 21, 2019Publication date: February 27, 2020Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Willard R. True, Richard Berckefeldt, Kalluri R. Sarma
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Patent number: 10338337Abstract: A display system configured for displaying critical aeronautical information on an aircraft display that is not certified for displaying critical aeronautical information comprises a mounting adapter and an application server. The mounting adapter is configured to mount, in an aircraft cockpit, a personal electronic device (PED) wherein the PED is not certified to display critical aeronautical information. The mounting adapter further comprises a surface with an actuatable covering that is configured to be overlaid on a PED display and an actuation source configured to actuate the covering. The application server is configured to execute a module that generates critical aeronautical information, transmit the generated critical aeronautical information to the PED for display, determine whether a problem exists with the image displayed on the PED display, and enable the actuation source to cause the covering to annunciate a message indicating a problem with the image displayed on the PED display.Type: GrantFiled: March 8, 2018Date of Patent: July 2, 2019Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Richard Berckefeldt, Willard R. True, Kalluri R. Sarma
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Publication number: 20190179585Abstract: A method in a high integrity device for verifying the integrity, continuity, and availability (ICA) of information displayed on an uncertified display is provided. The method comprises creating, on the high integrity device, application data for display on an uncertified display device; transmitting the application data to the uncertified display device; receiving, at the high integrity device from an optical sensing device, a captured image of the display; determining, at the high integrity device, an expected display image to be displayed on the uncertified display device; comparing, at the high integrity device, the captured image of the display to the expected display image; identifying, at the high integrity device, a loss of ICA if one or more frames in the captured image fails the comparison with the expected display image; and causing the annunciation of a message indicating the loss of ICA when a loss of ICA is identified.Type: ApplicationFiled: April 23, 2018Publication date: June 13, 2019Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Willard R. True, Richard Berckefeldt, Kalluri R. Sarma
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Publication number: 20190179097Abstract: A display system configured for displaying critical aeronautical information on an aircraft display that is not certified for displaying critical aeronautical information comprises a mounting adapter and an application server. The mounting adapter is configured to mount, in an aircraft cockpit, a personal electronic device (PED) wherein the PED is not certified to display critical aeronautical information. The mounting adapter further comprises a surface with an actuatable covering that is configured to be overlaid on a PED display and an actuation source configured to actuate the covering. The application server is configured to execute a module that generates critical aeronautical information, transmit the generated critical aeronautical information to the PED for display, determine whether a problem exists with the image displayed on the PED display, and enable the actuation source to cause the covering to annunciate a message indicating a problem with the image displayed on the PED display.Type: ApplicationFiled: March 8, 2018Publication date: June 13, 2019Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Richard Berckefeldt, Willard R. True, Kalluri R. Sarma
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Publication number: 20190180718Abstract: A display integrity system for use in a mounting adapter configured to mount a personal electronic device (PED) on an aircraft is disclosed. The display integrity system includes a transparent surface configured to overlay the display surface of a PED when the PED is mounted in the mounting adapter. The transparent surface includes one or more regions embedded with one or more coating layers that when activated with a select excitation wavelength are configured to emit visible light to annunciate a message indicating a problem with an image displayed on the PED. The display integrity system further includes a lighting source housed in the mounting adapter and configured to provide light in the select excitation wavelength when activated to illuminate the transparent surface and an imaging device mounted in the mounting adapter and configured to capture an image of the PED display for transmission to a server for integrity checking.Type: ApplicationFiled: March 20, 2018Publication date: June 13, 2019Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Kalluri R. Sarma, Richard Berckefeldt, Willard R. True
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Publication number: 20190180530Abstract: A server system on an aircraft is provided. The server system is configured to allow critical aeronautical information to be displayed on a cockpit display that is not certified for displaying critical aeronautical information. The server system includes an aircraft interface device configured to interface with one or more aeronautical systems on the aircraft to retrieve critical aeronautical information; an application module configured to generate application data for display on the cockpit display wherein the application data includes at least some of the critical aeronautical information; an interface module configured to transmit the application data to the cockpit display for display; and an integrity checking module configured to retrieve image data from an image sensor trained on a display device in the cockpit display and configured to perform an integrity check on the image data from the image sensor.Type: ApplicationFiled: March 13, 2018Publication date: June 13, 2019Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Willard R. True, Richard Berckefeldt, Kalluri R. Sarma
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Publication number: 20190177157Abstract: An addressable display system configured for use in a mounting adapter configured to mount a personal electronic device (PED) on an aircraft includes a transparent surface configured to overlay the display surface of a PED when the PED is mounted in the mounting adapter wherein the transparent surface includes a region that is uniformly coated with a coating layer that when activated with a select excitation wavelength is configured to emit visible light to annunciate a message indicating a problem with an image displayed on a PED display; a lighting source configured to provide light in at an excitation wavelength; a MEMS (microelectromechanical systems) scanner module that is controllable to write desired symbology for annunciation at different addressable locations on the transparent surface; and an imaging device configured to capture an image of the PED display for an integrity check of data displayed on the PED display.Type: ApplicationFiled: March 22, 2018Publication date: June 13, 2019Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Kalluri R. Sarma, Richard Berckefeldt, Willard R. True
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Patent number: 10273020Abstract: A mounting apparatus configured to mount a personal electronic device (PED) in an aircraft flight deck and provide a visible indication on the PED display when a fault condition exists includes an optical sensor positioned to view the PED display and configured to record an image of the PED display; an optically transparent surface configured to be overlaid on the PED display; an actuatable covering on the surface wherein the actuatable covering has a first optically transparent state and a second optically emissive state; an excitation source configured to cause the covering to switch from the first state to the second state; and a controller configured to transmit an image of the PED display recorded by the optical sensor to a server and command, responsive to receipt of an enable signal from the server, the actuation source to actuate the covering to indicate that the fault condition exists.Type: GrantFiled: March 13, 2018Date of Patent: April 30, 2019Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Richard Berckefeldt, Willard R. True, Kalluri R. Sarma
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Patent number: 9967707Abstract: In some examples, a first entity is configured to request weather data for a region of interest from a second entity. The second entity may transmit the requested weather data to the first entity in response to receiving the request. In some examples, the second entity only transmits the weather data to the first entity only in response to receiving a specific request for the weather data. Conversely, the first entity may only receive the weather data from the second entity in response to transmitting a request for the weather data.Type: GrantFiled: April 16, 2014Date of Patent: May 8, 2018Assignee: Honeywell International Inc.Inventors: Carl Esposito, Kenneth R. Jongsma, Willard R. True
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Patent number: 9330573Abstract: Provided are methods and systems for the automatic calculation and presentation of data on a display device alerting a pilot that a change in flight plan is desirable, possible and administratively compliant under air traffic control protocol. The methods and systems may automatically request the flight clearance over a data link or the pilot may override the data link.Type: GrantFiled: September 21, 2009Date of Patent: May 3, 2016Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Ruy C. Brandao, Rosa Maria Nicole Weber, Willard R. True, Michael L. Olive, Christine Marie Haissig
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Publication number: 20150304813Abstract: In some examples, a first entity is configured to request weather data for a region of interest from a second entity. The second entity may transmit the requested weather data to the first entity in response to receiving the request. In some examples, the second entity only transmits the weather data to the first entity only in response to receiving a specific request for the weather data. Conversely, the first entity may only receive the weather data from the second entity in response to transmitting a request for the weather data.Type: ApplicationFiled: April 16, 2014Publication date: October 22, 2015Applicant: Honeywell International Inc.Inventors: Carl Esposito, Kenneth R. Jongsma, Willard R. True
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Patent number: 8284674Abstract: A method includes selecting a first communications network from a plurality of communications networks based on one or more aircraft state inputs. The one or more aircraft state inputs include at least one of a flight phase, a flight event, an aircraft position, an aircraft trajectory, an aircraft state, and an aircraft distance from a ground station. The method further includes transmitting data over the first communication network. The method further includes selecting a second communications network from the plurality of communications networks based on a change in the one or more aircraft state inputs.Type: GrantFiled: May 28, 2010Date of Patent: October 9, 2012Assignee: Honeywell International Inc.Inventors: Willard R. True, Alfonso Malaga, Matt E. Larsen, Richard J. Eckert
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Patent number: 8280563Abstract: A system to send air traffic control (ATC) data-link messages from an aircraft is provided. The system includes ATC applications in a first portion of an application layer, non-ATC applications in a second portion of the application layer; and a communication manager in the aircraft having two addresses for the aircraft. The communication manager includes a first copy of software in a first data link layer and a second copy of the software in a second data link layer. ATC data-link messages are sent from the aircraft independent of non-ATC data-link messages sent from the aircraft.Type: GrantFiled: November 13, 2009Date of Patent: October 2, 2012Assignee: Honeywell International Inc.Inventors: Thomas F. McGuffin, Willard R. True
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Patent number: 8223062Abstract: Systems and methods communicate weather information between aircraft using low bandwidth communication transceivers. An exemplary embodiment receives weather information from a weather radar system on board a remote aircraft, processes the received weather information into weather radar image information that is displayable on at least a display, processes the weather radar image information into a reduced size dataset, and communicates the reduced size dataset to an installation aircraft over the low bandwidth communication channel, wherein the low bandwidth communication channel is generated by a low bandwidth communication transceiver on board the remote aircraft.Type: GrantFiled: May 27, 2009Date of Patent: July 17, 2012Assignee: Honeywell International Inc.Inventors: Brian Paul Bunch, Michael M. Grove, Willard R. True, Ken Kuttler
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Publication number: 20110118904Abstract: A system to send air traffic control (ATC) data-link messages from an aircraft is provided. The system includes ATC applications in a first portion of an application layer, non-ATC applications in a second portion of the application layer; and a communication manager in the aircraft having two addresses for the aircraft. The communication manager includes a first copy of software in a first data link layer and a second copy of the software in a second data link layer. ATC data-link messages are sent from the aircraft independent of non-ATC data-link messages sent from the aircraft.Type: ApplicationFiled: November 13, 2009Publication date: May 19, 2011Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Thomas F. McGuffin, Willard R. True