Patents by Inventor Ira E. Zoock
Ira E. Zoock 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: 10216187Abstract: A vehicle includes a frame, drive elements configured to drive movements of the frame, and a computer configured to receive mission planning and manual commands and to control operations of the drive elements to operate in a safe mode in which mission commands are accepted but manual commands are refused, a manual mode in which mission commands are refused but manual commands are accepted and an enroute mode. The computer is further configured to only allow mode transitions directly between the safe mode and the manual mode and directly between the safe mode and the enroute mode.Type: GrantFiled: June 15, 2017Date of Patent: February 26, 2019Assignee: SIKORSKY AIRCRAFT CORPORATIONInventors: Thomas Zygmant, Jesse J. Lesperance, Ira E. Zoock, James A. Kelly
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Publication number: 20170285638Abstract: A vehicle includes a frame, drive elements configured to drive movements of the frame, and a computer configured to receive mission planning and manual commands and to control operations of the drive elements to operate in a safe mode in which mission commands are accepted but manual commands are refused, a manual mode in which mission commands are refused but manual commands are accepted and an enroute mode. The computer is further configured to only allow mode transitions directly between the safe mode and the manual mode and directly between the safe mode and the enroute mode.Type: ApplicationFiled: June 15, 2017Publication date: October 5, 2017Inventors: Thomas Zygmant, Jesse J. Lesperance, Ira E. Zoock, James A. Kelly
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Patent number: 9778655Abstract: An aircraft is provided and includes a frame, drive elements configured to drive movements of the frame and a computer configured to receive mission planning and manual commands and to control operations of the drive elements to operate in a safe mode in which mission commands are accepted but manual commands are refused, a manual mode in which mission commands are refused but manual commands are accepted and an enroute mode. The computer is further configured to only allow mode transitions between the safe and manual modes and between the safe and enroute modes.Type: GrantFiled: August 26, 2016Date of Patent: October 3, 2017Assignee: SIKORSKY AIRCRAFT CORPORATIONInventors: Thomas Zygmant, Jesse J. Lesperance, Ira E. Zoock, James A. Kelly
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Publication number: 20160363934Abstract: An aircraft is provided and includes a frame, drive elements configured to drive movements of the frame and a computer configured to receive mission planning and manual commands and to control operations of the drive elements to operate in a safe mode in which mission commands are accepted but manual commands are refused, a manual mode in which mission commands are refused but manual commands are accepted and an enroute mode. The computer is further configured to only allow mode transitions between the safe and manual modes and between the safe and enroute modes.Type: ApplicationFiled: August 26, 2016Publication date: December 15, 2016Inventors: Thomas Zygmant, Jesse J. Lesperance, Ira E. Zoock, James A. Kelly
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Patent number: 9499264Abstract: An aircraft is provided and includes a frame, drive elements configured to drive movements of the frame and a computer configured to receive mission planning and manual commands and to control operations of the drive elements to operate in a safe mode in which mission commands are accepted but manual commands are refused, a manual mode in which mission commands are refused but manual commands are accepted and an enroute mode. The computer is further configured to only allow mode transitions between the safe and manual modes and between the safe and enroute modes.Type: GrantFiled: May 29, 2015Date of Patent: November 22, 2016Assignee: SIKORSKY AIRCRAFT CORPORATIONInventors: Thomas Zygmant, Jesse J. Lesperance, Ira E. Zoock, James A. Kelly
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Publication number: 20160077523Abstract: A ground-based aircraft control system including at least one data receiver/transmitter module configured to transmit aircraft control and data signals to an aircraft to control the flight of the aircraft and to receive data signals from the aircraft. At least one controller including a voice command recognition module configured to receive voice commands, to generate control signals based on the voice commands, and to transmit the control signals and command audio signals to the aircraft via the at least one data receiver/transmitter module. The at least one controller is configured to receive non-command voice audio signals and to transmit the non-command voice audio signals to the aircraft via the at least one data receiver/transmitter module.Type: ApplicationFiled: July 22, 2013Publication date: March 17, 2016Applicant: Sikorsky Aircraft CorporationInventors: Thomas Zygmant, Jesse J. Lesperance, Ira E. Zoock, James A. Kelly
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Publication number: 20150346725Abstract: An aircraft is provided and includes a frame, drive elements configured to drive movements of the frame and a computer configured to receive mission planning and manual commands and to control operations of the drive elements to operate in a safe mode in which mission commands are accepted but manual commands are refused, a manual mode in which mission commands are refused but manual commands are accepted and an enroute mode. The computer is further configured to only allow mode transitions between the safe and manual modes and between the safe and enroute modes.Type: ApplicationFiled: May 29, 2015Publication date: December 3, 2015Inventors: Thomas Zygmant, Jesse J. Lesperance, Ira E. Zoock, James A. Kelly
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Patent number: 9120569Abstract: Embodiments are directed to receiving, by a control station, an input including a command for re-location of a vehicle from a first location to a second location, the input identifying the second location, determining, by the control station, at least one of a distance, a direction, an altitude, and a latitude and longitude for the vehicle to travel from the first location to the second location, and transmitting, by the control station, the command and the at least one of a distance, a direction, an altitude, and a latitude and longitude to the vehicle.Type: GrantFiled: August 2, 2012Date of Patent: September 1, 2015Assignee: SIKORSKY AIRCRAFT CORPORATIONInventors: Thomas Zygmant, Jesse J. Lesperance, Ira E. Zoock
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Patent number: 8967544Abstract: A method of releasing cargo suspended from at least one cargo hook release pendant in a suspension system coupled to a cargo hook release system includes receiving a voltage release signal at a cargo hook control interface and a cargo release harness assembly; receiving an energizing voltage signal at the cargo release harness assembly; energizing a relay in response to receiving the energizing voltage signal, the relay being electrically coupled to the cargo release harness assembly; automatically transmitting the voltage release signal from the cargo release harness assembly to at least one cargo hook release pendant in response to energizing the relay; and automatically releasing the cargo from at least one cargo hook release pendant in response to automatically transmitting the voltage release signal. Also, the cargo hook release system includes the cargo hook control interface, the cargo release harness assembly, and at least one cargo hook release pendant.Type: GrantFiled: May 9, 2012Date of Patent: March 3, 2015Assignee: Sikorsky Aircraft CorporationInventors: James A. Kelly, Jesse J. Lesperance, Ira E. Zoock, Thomas Zygmant
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Publication number: 20140236387Abstract: Embodiments are directed to receiving, by a control station, an input including a command for re-location of a vehicle from a first location to a second location, the input identifying the second location, determining, by the control station, at least one of a distance, a direction, an altitude, and a latitude and longitude for the vehicle to travel from the first location to the second location, and transmitting, by the control station, the command and the at least one of a distance, a direction, an altitude, and a latitude and longitude to the vehicle.Type: ApplicationFiled: August 2, 2012Publication date: August 21, 2014Applicant: SIKORKSY AIRCRAFT CORPORATIONInventors: Thomas Zygmant, Jesse J. Lesperance, Ira E. Zoock
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Publication number: 20130299640Abstract: A method of releasing cargo suspended from at least one cargo hook release pendant in a suspension system coupled to a cargo hook release system includes receiving a voltage release signal at a cargo hook control interface and a cargo release harness assembly; receiving an energizing voltage signal at the cargo release harness assembly; energizing a relay in response to receiving the energizing voltage signal, the relay being electrically coupled to the cargo release harness assembly; automatically transmitting the voltage release signal from the cargo release harness assembly to at least one cargo hook release pendant in response to energizing the relay; and automatically releasing the cargo from at least one cargo hook release pendant in response to automatically transmitting the voltage release signal. Also, the cargo hook release system includes the cargo hook control interface, the cargo release harness assembly, and at least one cargo hook release pendant.Type: ApplicationFiled: May 9, 2012Publication date: November 14, 2013Applicant: SIKORSKY AIRCRAFT CORPORATIONInventors: James A. Kelly, Jesse J. Lesperance, Ira E. Zoock, Thomas Zygmant