Patents by Inventor Alireza Majd
Alireza Majd 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: 11305886Abstract: A method, apparatus, and system for displaying information for an aircraft on a display device in a flight deck of the aircraft. A computer system in the aircraft displays a dynamic home page in a graphical user interface on the display device in the flight deck of the aircraft. The information in the dynamic home page is based on the information used to operate the aircraft during a current phase of flight. The computer system changes the information in the dynamic home page as the current phase of flight changes or non-normal conditions occur during operation of the aircraft.Type: GrantFiled: June 7, 2019Date of Patent: April 19, 2022Assignee: The Boeing CompanyInventors: Brian David Gilbert, Alireza Majd, Paul D. Burkhead, Alessandro Edward Galli, John Wiedemann
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Patent number: 11268827Abstract: An interactive speed profile bar that enables crew awareness of the overall planned flight trajectory speed profile. The speed profile bar will have a graphical depiction (e.g., virtual buttons having alphanumeric symbology) of some or all of the speed segments of the speed profile. Each graphical element (e.g., virtual button) includes symbology identifying the applicable speed mode and corresponding target speed change. Each speed segment will start at the inflection point where the speed change will occur in the flight plan, and will continue until the next trajectory speed change. The speed profile bar will be interactive, allowing the flight crew to select the speed segment to change, in response to which selection the system displays graphical user interface elements showing a menu of the available speed segment options. Each individual speed segment is represented by an individual virtual button that can be selected by touching the screen or other input device.Type: GrantFiled: January 30, 2020Date of Patent: March 8, 2022Assignee: The Boeing CompanyInventors: Peter D. Gunn, John Wiedemann, Alireza Majd, Robert J. Myers, Brian D. Gilbert
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Patent number: 11262900Abstract: A method, apparatus, and system for displaying information for an aircraft on a display device in a flight deck of the aircraft. Aircraft information is received for a current flight of the aircraft. An interactive strip is displayed in a graphical user interface on the display device in the flight deck of the aircraft. The aircraft information and controls are displayed within regions in the interactive strip, enabling a pilot to operate the aircraft using the interactive strip.Type: GrantFiled: June 7, 2019Date of Patent: March 1, 2022Assignee: The Boeing CompanyInventors: Paul D. Burkhead, Alireza Majd, John Wiedemann
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Patent number: 11137873Abstract: A method and apparatus for displaying information for an aircraft on display devices in a flight deck of the aircraft. A computer system in the aircraft identifies information used to operate the aircraft. The computer system selects a display configuration from a plurality of display configurations for the display devices. The computer system displays the information in windows on display devices in the flight deck of the aircraft in the display configuration. The display configuration simplifies access to the information used to operate the aircraft.Type: GrantFiled: August 31, 2020Date of Patent: October 5, 2021Assignee: The Boeing CompanyInventors: Brian David Gilbert, John Wiedemann, Sherwin S. Chen, Alireza Majd
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Patent number: 11008117Abstract: Systems and methods for enabling a user (e.g., a pilot) to input information to a computer at a flight deck display station using both a split keyboard and a touch screen. The split keyboard provides space in front of the touch-screen display device, which space is available for a pilot to use as an arm or wrist rest while manually interacting with the touch screen. For example, the split keyboard may be mounted to a shelf having an empty central or middle portion in front of the touch-screen display device. The split keyboard concept entails placing one keypad on one side and another keypad on the other side of the empty middle shelf portion, both keypads being communicatively to the keyboard controller of the computer that controls the display device. The open space between the keypads may also be used for meal trays or tablet computers.Type: GrantFiled: February 24, 2020Date of Patent: May 18, 2021Assignee: The Boeing CompanyInventors: Sandra C. Dam, Christopher D. Haus, Alireza Majd, John Wiedemann, Alessandro E. Galli, Brandon R. Boekelman
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Patent number: 10761676Abstract: A method, apparatus, and system for displaying information for an aircraft on display devices in a flight deck of the aircraft. A computer system in the aircraft identifies information used to operate the aircraft. The computer system selects a display configuration from a plurality of display configurations for the display devices based on a first set of tasks assigned to a pilot for a current flight and a second set of tasks assigned to a copilot for the current flight of the aircraft. The computer system displays the information in windows on display devices in the flight deck of the aircraft in the display configuration. The display configuration simplifies access to the information used by the pilot to perform the first set of tasks and the copilot to perform the second set of tasks.Type: GrantFiled: September 25, 2018Date of Patent: September 1, 2020Assignee: The Boeing CompanyInventors: Brian David Gilbert, John Wiedemann, Sherwin S. Chen, Alireza Majd
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Publication number: 20200166374Abstract: An interactive speed profile bar that enables crew awareness of the overall planned flight trajectory speed profile. The speed profile bar will have a graphical depiction (e.g., virtual buttons having alphanumeric symbology) of some or all of the speed segments of the speed profile. Each graphical element (e.g., virtual button) includes symbology identifying the applicable speed mode and corresponding target speed change. Each speed segment will start at the inflection point where the speed change will occur in the flight plan, and will continue until the next trajectory speed change. The speed profile bar will be interactive, allowing the flight crew to select the speed segment to change, in response to which selection the system displays graphical user interface elements showing a menu of the available speed segment options. Each individual speed segment is represented by an individual virtual button that can be selected by touching the screen or other input device.Type: ApplicationFiled: January 30, 2020Publication date: May 28, 2020Applicant: The Boeing CompanyInventors: Peter D. Gunn, John Wiedemann, Alireza Majd, Robert J. Myers, Brian D. Gilbert
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Patent number: 10584979Abstract: An interactive speed profile bar that enables crew awareness of the overall planned flight trajectory speed profile. The speed profile bar will have a graphical depiction (e.g., virtual buttons having alphanumeric symbology) of some or all of the speed segments of the speed profile. Each graphical element (e.g., virtual button) includes symbology identifying the applicable speed mode and corresponding target speed change. Each speed segment will start at the inflection point where the speed change will occur in the flight plan, and will continue until the next trajectory speed change. The speed profile bar will be interactive, allowing the flight crew to select the speed segment to change, in response to which selection the system displays graphical user interface elements showing a menu of the available speed segment options. Each individual speed segment is represented by an individual virtual button that can be selected by touching the screen or other input device.Type: GrantFiled: September 28, 2018Date of Patent: March 10, 2020Assignee: The Boeing CompanyInventors: Peter D. Gunn, John Wiedemann, Alireza Majd, Robert J. Myers, Brian D. Gilbert