Patents by Inventor Greg Carlucci
Greg Carlucci 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: 11385072Abstract: Methods and systems are provided for presenting an energy state associated with an aircraft with respect to an operating envelope region for a procedure to restart an engine of the aircraft. One method involves providing a graphical user interface display having a first reference axis corresponding to a first energy state parameter and a second reference axis corresponding to a second energy state parameter different from the first energy state parameter, providing a graphical representation of an operating envelope region associated with a procedure for starting an engine of the aircraft with respect to the first and second reference axes, obtaining current values for the first and second energy state parameters for the aircraft, and providing a graphical representation of the aircraft positioned with respect to the first and second reference axes based on the current values for the first and second energy state parameters.Type: GrantFiled: July 15, 2019Date of Patent: July 12, 2022Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Sripathi Ramachandra, Greg Carlucci, Karel Mundel, Richard Snyder, Mark Pearson, Udipi Ranga Ananthram, PraveenKumar Ayyathurai, Samrat Kar
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Patent number: 11328610Abstract: Systems and methods of searching stored flight plan information using a custom search query including at least one aircraft parameter condition or environmental parameter condition. The systems and method include receiving, using a user interface module, a custom search query comprising an aircraft parameter condition or an environmental condition; searching, using a processor module, stored flight plan information for instances in the stored flight plan information that satisfy the aircraft parameter condition or environmental condition; and displaying, using a display module, the instances in the stored flight plan information that satisfy the aircraft parameter condition or environmental condition.Type: GrantFiled: July 24, 2018Date of Patent: May 10, 2022Assignee: Honeywell International Inc.Inventors: Sripathi Ramachandra, Mark Pearson, Greg Carlucci, Richard Snyder
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Patent number: 11043130Abstract: An aircraft and a method for operating the same may include, but is not limited to, a flight management system, a vertical situation display, and a processor configured to determine a first variable, a second variable and a third variable, determine flight plan data for the first, second and third variables, generate display data for the vertical situation display, the display data including the scale of the first second and third variables and a vector corresponding to the flight plan data of the first variable and second variable scaled to the first scale and the second scale, wherein the scale of the third variable is non-linear and varies based upon the flight plan data corresponding to the third variable relative to the vector, and output the generated display data to the vertical situation display for display on the vertical situation display.Type: GrantFiled: August 10, 2018Date of Patent: June 22, 2021Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Sripathi Ramachandra, Greg Carlucci, Richard Snyder, Mohammed Ibrahim Mohideen, Mark Pearson, Hyden Lopez, Christopher Raj Mariadoss
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Publication number: 20210018333Abstract: Methods and systems are provided for presenting an energy state associated with an aircraft with respect to an operating envelope region for a procedure to restart an engine of the aircraft. One method involves providing a graphical user interface display having a first reference axis corresponding to a first energy state parameter and a second reference axis corresponding to a second energy state parameter different from the first energy state parameter, providing a graphical representation of an operating envelope region associated with a procedure for starting an engine of the aircraft with respect to the first and second reference axes, obtaining current values for the first and second energy state parameters for the aircraft, and providing a graphical representation of the aircraft positioned with respect to the first and second reference axes based on the current values for the first and second energy state parameters.Type: ApplicationFiled: July 15, 2019Publication date: January 21, 2021Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Sripathi Ramachandra, Greg Carlucci, Karel Mundel, Richard Snyder, Mark Pearson, Udipi Ranga Ananthram, PraveenKumar Ayyathurai, Samrat Kar
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Patent number: 10706726Abstract: Methods and systems for a flight display system are provided. The method includes: commanding a vertical situation display (VSD) and a lateral navigation display (ND) to render, concurrently, a viewing segment of a flight plan. The method includes receiving a user input selecting a section of the viewing segment, the user input being received on only one of the VSD and the ND. The method continues by commanding, concurrently, the VSD and the ND to visually distinguish the section, and to demark the section on the VSD with starting points and ending points. The method identifies a flight parameter, and for the flight parameter, includes (a) determining which display, among the VSD and the ND, is appropriate for the rendering of flight parameter information; (b) generating flight parameter information based on (a); and (c) overlaying the flight parameter information on the appropriate display.Type: GrantFiled: March 6, 2018Date of Patent: July 7, 2020Assignee: HONEYWELL INTERNATIONAL INC.Inventors: Sripathi Ramachandra, Mark Pearson, Greg Carlucci, Richard Snyder, Balaji Srinivasan
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Publication number: 20200051441Abstract: An aircraft and a method for operating the same are provided. The aircraft, for example, may include, but is not limited to, a flight management system, a vertical situation display, and a processor configured to determine a first variable, a second variable and a third variable, determine flight plan data for the first, second and third variables, generate display data for the vertical situation display, the display data including the scale of the first second and third variables and a vector corresponding to the flight plan data of the first variable and second variable scaled to the first scale and the second scale, wherein the scale of the third variable is non-linear and varies based upon the flight plan data corresponding to the third variable relative to the vector, and output the generated display data to the vertical situation display for display on the vertical situation display.Type: ApplicationFiled: August 10, 2018Publication date: February 13, 2020Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Sripathi Ramachandra, Greg Carlucci, Richard Snyder, Mohammed Ibrahim Mohideen, Mark Pearson, Hyden Lopez, Christopher Raj Mariadoss
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Publication number: 20200035109Abstract: Systems and methods of searching stored flight plan information using a custom search query including at least one aircraft parameter condition or environmental parameter condition. The systems and method include receiving, using a user interface module, a custom search query comprising an aircraft parameter condition or an environmental condition; searching, using a processor module, stored flight plan information for instances in the stored flight plan information that satisfy the aircraft parameter condition or environmental condition; and displaying, using a display module, the instances in the stored flight plan information that satisfy the aircraft parameter condition or environmental condition.Type: ApplicationFiled: July 24, 2018Publication date: January 30, 2020Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Sripathi Ramachandra, Mark Pearson, Greg Carlucci, Richard Snyder
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Publication number: 20190279514Abstract: Methods and systems for a flight display system are provided. The method includes: commanding a vertical situation display (VSD) and a lateral navigation display (ND) to render, concurrently, a viewing segment of a flight plan. The method includes receiving a user input selecting a section of the viewing segment, the user input being received on only one of the VSD and the ND. The method continues by commanding, concurrently, the VSD and the ND to visually distinguish the section, and to demark the section on the VSD with starting points and ending points. The method identifies a flight parameter, and for the flight parameter, includes (a) determining which display, among the VSD and the ND, is appropriate for the rendering of flight parameter information; (b) generating flight parameter information based on (a); and (c) overlaying the flight parameter information on the appropriate display.Type: ApplicationFiled: March 6, 2018Publication date: September 12, 2019Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Sripathi Ramachandra, Mark Pearson, Greg Carlucci, Richard Snyder, Balaji Srinivasan
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Patent number: 8503484Abstract: A node comprises a host computer operable to execute application tasks and to transmit data; a local time-triggered Ethernet switch operable to enforce temporal constraints on time-triggered data; and a time-triggered Ethernet controller coupled to the local time-triggered Ethernet switch and operable to be coupled to a time-triggered Ethernet switch in each of a plurality of other control nodes. The time-triggered Ethernet controller is further operable to communicate with the plurality of other control nodes to synchronize a local clock to establish a global time base and to provide a signal to the host computer for the host computer to synchronize execution of the application tasks by the host computer with the execution of application tasks in each of the plurality of other control nodes.Type: GrantFiled: January 19, 2009Date of Patent: August 6, 2013Assignee: Honeywell International Inc.Inventors: Ted Bonk, William Todd Smithgall, Mitch Fletcher, Greg Carlucci
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Publication number: 20100183016Abstract: A node comprises a host computer operable to execute application tasks and to transmit data; a local time-triggered Ethernet switch operable to enforce temporal constraints on time-triggered data; and a time-triggered Ethernet controller coupled to the local time-triggered Ethernet switch and operable to be coupled to a time-triggered Ethernet switch in each of a plurality of other control nodes.Type: ApplicationFiled: January 19, 2009Publication date: July 22, 2010Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Ted Bonk, William Todd Smithgall, Mitch Fletcher, Greg Carlucci