Patents by Inventor Jennifer L. Gertley

Jennifer L. Gertley 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).

  • Patent number: 9738378
    Abstract: A system and method for braking an aircraft. A processor unit identifies an operating condition of the aircraft. The processor unit displays available modes indications on a display device on the aircraft. The available modes indications indicate modes of operating an automatic braking system on the aircraft that are available for selection by an operator based on the operating condition of the aircraft. The processor unit receives a mode selection from an operator interface. The mode selection indicates a selected mode of operating the automatic braking system that is selected by the operator from the available modes. The processor unit displays on the display device a selected mode indication indicating the selected mode.
    Type: Grant
    Filed: April 8, 2016
    Date of Patent: August 22, 2017
    Assignee: THE BOEING COMPANY
    Inventors: Mark Ivan Nikolic, Joseph A. Sikora, William Lawrence Hunt, Jean M. Crane, Jennifer L. Gertley
  • Patent number: 8417396
    Abstract: A method of operating an air traffic control system may include receiving, by a control system, an instruction from a control system user. The method may further include providing, by the control system, the instruction to an airplane via a data link between the control system and a system of the airplane. In addition, the method may include adjusting, by the airplane system, at least one airplane control to correspond to the instruction.
    Type: Grant
    Filed: September 22, 2011
    Date of Patent: April 9, 2013
    Assignee: The Boeing Company
    Inventors: William L. Goodman, Syed T. Shafaat, John A. Brown, Jennifer L. Gertley, Robert P. Smith
  • Patent number: 8315787
    Abstract: Situational Awareness and Guidance Reference (SAGR) and associated methods and systems are disclosed. A system in accordance to one embodiment of the disclosure includes a display system utilized for a traffic application and an SAGR associated with the own-ship symbol providing longitudinal and lateral guidance reference. In a manual implementation, the SAGR aids human operators achieve required longitudinal and lateral spacing from selected traffic by depicting a small operating region on a navigational map display within which an aircraft will have achieved the required spacing. Such depiction of the deviation guidance may be with respect to time or distance relative to selected traffic aircraft or to fixed structure, and engaged in an automatic or manual mode.
    Type: Grant
    Filed: October 16, 2011
    Date of Patent: November 20, 2012
    Assignee: The Boeing Company
    Inventors: Syed Taji Shafaat, Jennifer L. Gertley
  • Publication number: 20120035842
    Abstract: Situational Awareness and Guidance Reference (SAGR) and associated methods and systems are disclosed. A system in accordance to one embodiment of the disclosure includes a display system utilized for a traffic application and an SAGR associated with the own-ship symbol providing longitudinal and lateral guidance reference. In a manual implementation, the SAGR aids human operators achieve required longitudinal and lateral spacing from selected traffic by depicting a small operating region on a navigational map display within which an aircraft will have achieved the required spacing. Such depiction of the deviation guidance may be with respect to time or distance relative to selected traffic aircraft or to fixed structure, and engaged in an automatic or manual mode.
    Type: Application
    Filed: October 16, 2011
    Publication date: February 9, 2012
    Applicant: The Boeing Company
    Inventors: Syed Taji SHAFAAT, Jennifer L. GERTLEY
  • Publication number: 20120010763
    Abstract: A method of operating an air traffic control system may include receiving, by a control system, an instruction from a control system user. The method may further include providing, by the control system, the instruction to an airplane via a data link between the control system and a system of the airplane. In addition, the method may include adjusting, by the airplane system, at least one airplane control to correspond to the instruction.
    Type: Application
    Filed: September 22, 2011
    Publication date: January 12, 2012
    Applicant: THE BOEING COMPANY
    Inventors: William L. Goodman, Syed T. Shafaat, John A. Brown, Jennifer L. Gertley, Robert P. Smith
  • Patent number: 8046159
    Abstract: A method of receiving an instruction by an airplane from a control system includes facilitating, by the airplane, a user of a system of the airplane in accepting or rejecting the instruction. The instruction may be received by the airplane via a data link between the control system and the airplane system. If the instruction is accepted, the method may further include loading, by the airplane, the instruction into the airplane system and/or adjusting, by the airplane, at least one airplane control to correspond to the instruction.
    Type: Grant
    Filed: November 1, 2010
    Date of Patent: October 25, 2011
    Assignee: The Boeing Company
    Inventors: William L. Goodman, Syed T. Shafaat, John A. Brown, Jennifer L. Gertley, Robert P. Smith
  • Patent number: 8041504
    Abstract: Situational Awareness and Guidance Reference (SAGR) and associated methods and systems are disclosed. A system in accordance to one embodiment of the disclosure includes a display system utilized for a traffic application and an SAGR associated with the own-ship symbol providing longitudinal and lateral guidance reference. In a manual implementation, the SAGR aids human operators achieve required longitudinal and lateral spacing from selected traffic by depicting a small operating region on a navigational map display within which an aircraft will have achieved the required spacing. Such depiction of the deviation guidance may be with respect to time or distance relative to selected traffic aircraft or to fixed structure, and engaged in an automatic or manual mode.
    Type: Grant
    Filed: December 17, 2007
    Date of Patent: October 18, 2011
    Assignee: The Boeing Company
    Inventors: Syed Taji Shafaat, Jennifer L. Gertley
  • Publication number: 20110046869
    Abstract: A method of receiving an instruction by an airplane from a control system includes facilitating, by the airplane, a user of a system of the airplane in accepting or rejecting the instruction. The instruction may be received by the airplane via a data link between the control system and the airplane system. If the instruction is accepted, the method may further include loading, by the airplane, the instruction into the airplane system and/or adjusting, by the airplane, at least one airplane control to correspond to the instruction.
    Type: Application
    Filed: November 1, 2010
    Publication date: February 24, 2011
    Applicant: The Boeing Company
    Inventors: William L. Goodman, Syed T. Shafaat, John A. Brown, Jennifer L. Gertley, Robert P. Smith
  • Patent number: 7848877
    Abstract: Methods and apparatuses for receiving, by an airplane, one or more clearances and/or instructions from a control system via a data link between the control system and a system of the airplane, are described herein. The system of the airplane may then facilitate a user in accepting or rejecting at least one of the received one or more clearances and/or instructions, and if accepted, may load the clearance and/or instructions and/or adjust controls to correspond to the clearance and/or instructions. Further, the system of the airplane may be adapted to display at least instructions indicia of whether the received instructions are met to a user.
    Type: Grant
    Filed: November 14, 2006
    Date of Patent: December 7, 2010
    Assignee: The Boeing Company
    Inventors: William L. Goodman, Syed T. Shafaat, John A. Brown, Jennifer L. Gertley, Robert P. Smith
  • Publication number: 20090157287
    Abstract: Situational Awareness and Guidance Reference (SAGR) and associated methods and systems are disclosed. A system in accordance to one embodiment of the disclosure includes a display system utilized for a traffic application and an SAGR associated with the own-ship symbol providing longitudinal and lateral guidance reference. In a manual implementation, the SAGR aids human operators achieve required longitudinal and lateral spacing from selected traffic by depicting a small operating region on a navigational map display within which an aircraft will have achieved the required spacing. Such depiction of the deviation guidance may be with respect to time or distance relative to selected traffic aircraft or to fixed structure, and engaged in an automatic or manual mode.
    Type: Application
    Filed: December 17, 2007
    Publication date: June 18, 2009
    Applicant: THE BOEING COMPANY
    Inventors: SYED TAJI SHAFAAT, JENNIFER L. GERTLEY
  • Publication number: 20080114504
    Abstract: Methods and apparatuses for receiving, by an airplane, one or more clearances and/or instructions from a control system via a data link between the control system and a system of the airplane, are described herein. The system of the airplane may then facilitate a user in accepting or rejecting at least one of the received one or more clearances and/or instructions, and if accepted, may load the clearance and/or instructions and/or adjust controls to correspond to the clearance and/or instructions. Further, the system of the airplane may be adapted to display at least instructionsindicia of whether the received instructions are met to a user.
    Type: Application
    Filed: November 14, 2006
    Publication date: May 15, 2008
    Inventors: William L. Goodman, Syed T. Shafaat, John A. Brown, Jennifer L. Gertley, Robert P. Smith