Patents by Inventor James Donald Paduano
James Donald Paduano 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: 11693407Abstract: An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.Type: GrantFiled: May 4, 2020Date of Patent: July 4, 2023Assignee: The Boeing CompanyInventors: Jessica E. Duda, John Tylko, David Mindell, Fabrice Kunzi, Michael Piedmonte, John Allee, Joshua Torgerson, Jason Ryan, James Donald Paduano, John Brooke Wissler, Andrew Musto, Wendy Feenstra
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Patent number: 10942041Abstract: An aircraft, system, and method for sensing and/or releasing chemical agents by an aircraft is disclosed. The aircraft, system, and method may employ a chemical sensor, a wind sensor, an imaging device for capturing environmental features, and/or a processor operably coupled therewith. The processor may be used for collecting data from the chemical sensor, the wind sensor, and the imaging device to identify a navigational waypoint and to provide commands to the chemical sensor or to the aircraft based at least in part on collected data.Type: GrantFiled: July 27, 2018Date of Patent: March 9, 2021Assignee: Aurora Flight Sciences CorporationInventors: Amanda Kaufman, William Robert Bosworth, James Donald Paduano, Riley C. Griffin, Sachin Jain
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Publication number: 20200301422Abstract: An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.Type: ApplicationFiled: May 4, 2020Publication date: September 24, 2020Inventors: Jessica E. Duda, John Tylko, David Mindell, Fabrice Kunzi, Michael Piedmonte, John Allee, Joshua Torgerson, Jason Ryan, James Donald Paduano, John Brooke Wissler, Andrew Musto, Wendy Feenstra
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Patent number: 10642270Abstract: An aircrew automation system and method for use in an aircraft. The aircrew automation system comprises one or more processors, an optical perception system, an actuation system, and a human-machine interface. The optical perception system monitors, in real-time, one or more cockpit instruments of the aircraft visually to generate flight situation data. The actuation system mechanically engages at least one flight control of the aircraft in response to the one or more flight commands. The human-machine interface provides an interface between a human pilot and the aircrew automation system. The human-machine interface comprises a display device to display a status of the aircraft and the actuation system.Type: GrantFiled: July 8, 2019Date of Patent: May 5, 2020Assignee: Aurora Flight Sciences CorporationInventors: Jessica E. Duda, John Tylko, David Mindell, Fabrice Kunzi, Michael Piedmonte, John Allee, Joshua Torgerson, Jason Ryan, James Donald Paduano, John Brooke Wissler, Andrew Musto, Wendy Feenstra
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Publication number: 20200064840Abstract: An aircrew automation system and method for use in an aircraft. The aircrew automation system comprises one or more processors, an optical perception system, an actuation system, and a human-machine interface. The optical perception system monitors, in real-time, one or more cockpit instruments of the aircraft visually to generate flight situation data. The actuation system mechanically engages at least one flight control of the aircraft in response to the one or more flight commands. The human-machine interface provides an interface between a human pilot and the aircrew automation system. The human-machine interface comprises a display device to display a status of the aircraft and the actuation system.Type: ApplicationFiled: July 8, 2019Publication date: February 27, 2020Inventors: Jessica E. Duda, John Tylko, David Mindell, Fabrice Kunzi, Michael Piedmonte, John Allee, Joshua Torgerson, Jason Ryan, James Donald Paduano, John Brooke Wissler, Andrew Musto, Wendy Feenstra
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Publication number: 20200033157Abstract: An aircraft, system, and method for sensing and/or releasing chemical agents by an aircraft is disclosed. The aircraft, system, and method may employ a chemical sensor, a wind sensor, an imaging device for capturing environmental features, and/or a processor operably coupled therewith. The processor may be used for collecting data from the chemical sensor, the wind sensor, and the imaging device to identify a navigational waypoint and to provide commands to the chemical sensor or to the aircraft based at least in part on collected data.Type: ApplicationFiled: July 27, 2018Publication date: January 30, 2020Inventors: Amanda Kaufman, William Robert Bosworth, James Donald Paduano, Riley C. Griffin, Sachin Jain
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Patent number: 10359779Abstract: An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.Type: GrantFiled: March 21, 2017Date of Patent: July 23, 2019Assignee: Aurora Flight Sciences CorporationInventors: Jessica E. Duda, John Tylko, David Mindell, Fabrice Kunzi, Michael Piedmonte, John Allee, Joshua Torgerson, Jason Ryan, James Donald Paduano, John Brooke Wissler, Andrew Musto, Wendy Feenstra
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Publication number: 20170277185Abstract: An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.Type: ApplicationFiled: March 21, 2017Publication date: September 28, 2017Inventors: Jessica E. Duda, John Tylko, David Mindell, Fabrice Kunzi, Michael Piedmonte, John Allee, Joshua Torgerson, Jason Ryan, James Donald Paduano, John Brooke Wissler, Andrew Musto, Wendy Feenstra
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Patent number: 9682774Abstract: A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends.Type: GrantFiled: October 6, 2014Date of Patent: June 20, 2017Assignee: Aurora Flight Sciences CorporationInventors: James Donald Paduano, Paul Nils Dahlstrand, John Brooke Wissler, Adam Woodworth
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Patent number: 9540101Abstract: A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends.Type: GrantFiled: October 6, 2014Date of Patent: January 10, 2017Assignee: Aurora Flight Sciences CorporationInventors: James Donald Paduano, Paul Nils Dahlstrand, John Brooke Wissler, Adam Woodworth
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Publication number: 20150336663Abstract: A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends.Type: ApplicationFiled: October 6, 2014Publication date: November 26, 2015Inventors: JAMES DONALD PADUANO, PAUL NILS DAHLSTRAND, JOHN BROOKE WISSLER, ADAM WOODWORTH
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Publication number: 20150336666Abstract: A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends.Type: ApplicationFiled: October 6, 2014Publication date: November 26, 2015Inventors: JAMES DONALD PADUANO, PAUL NILS DAHLSTRAND, JOHN BROOKE WISSLER, ADAM WOODWORTH
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Publication number: 20150021430Abstract: A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends.Type: ApplicationFiled: October 6, 2014Publication date: January 22, 2015Inventors: JAMES DONALD PADUANO, PAUL NILS DAHLSTRAND, JOHN BROOKE WISSLER, ADAM WOODWORTH
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Publication number: 20130206921Abstract: A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends.Type: ApplicationFiled: February 15, 2012Publication date: August 15, 2013Applicant: AURORA FLIGHT SCIENCES CORPORATIONInventors: James Donald Paduano, Paul Nils Dahlstrand, John Brooke Wissler