Patents by Inventor Barbara E. Holder

Barbara E. Holder 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: 10315778
    Abstract: A flight deck display that represents the overall health of the airplane by combining energy state, system state and configuration state into one integrated representation that is triggered by the on-board engine indication and crew alerting system. The computer system for controlling the display unit is configured to display an airplane status indicator in the form of a symbolic representation of the airplane that persists across displays. The status indicator shows the energy state of the airplane and how energy is being added or subtracted from it in terms of altitude, airspeed, thrust, wind, etc. As the airplane gains energy, there is a projection of excess energy shown in front of the airplane. As the airplane loses energy, an alerting indicator will appear around the airplane symbol if the performance of the airplane becomes is too low.
    Type: Grant
    Filed: September 25, 2015
    Date of Patent: June 11, 2019
    Assignee: The Beoing Company
    Inventor: Barbara E. Holder
  • Publication number: 20170088284
    Abstract: A flight deck display that represents the overall health of the airplane by combining energy state, system state and configuration state into one integrated representation that is triggered by the on-board engine indication and crew alerting system. The computer system for controlling the display unit is configured to display an airplane status indicator in the form of a symbolic representation of the airplane that persists across displays. The status indicator shows the energy state of the airplane and how energy is being added or subtracted from it in terms of altitude, airspeed, thrust, wind, etc. As the airplane gains energy, there is a projection of excess energy shown in front of the airplane. As the airplane loses energy, an alerting indicator will appear around the airplane symbol if the performance of the airplane becomes is too low.
    Type: Application
    Filed: September 25, 2015
    Publication date: March 30, 2017
    Applicant: THE BOEING COMPANY
    Inventor: Barbara E. Holder
  • Patent number: 8527871
    Abstract: A method is disclosed for generating a quick reference handbook for use on a mobile platform. The method may involve providing a machine-readable medium for use with a processor having a memory. The machine-readable medium may provide instructions for causing the processor to generate a quick reference handbook (QRH). The QRH may be created through the use of checklists organized in accordance with a plurality of grouping schemes that include at least a plurality of: Immediate Action; Systems; and Engine Indication and Crew Alerting System (EICAS) messages. Differentiating criteria may also be used for decisions steps, action steps, and navigation steps within the checklists to thereby enable a user to discriminate between the steps.
    Type: Grant
    Filed: May 19, 2010
    Date of Patent: September 3, 2013
    Assignee: The Boeing Company
    Inventors: Barbara E. Holder, William A. McKenzie
  • Patent number: 8131410
    Abstract: In accordance with an embodiment, a method includes displaying information corresponding to automatically controlled engine thrust levels during a reduced engine thrust period of flight of an aircraft. The information corresponds to one or more parameters associated with a flight control computer of the aircraft. In an alternate aspect, the displayed information includes alphanumeric information formatted in accordance with a sequential order of the automatically controlled engine thrust levels. In a further aspect, the alphanumeric information corresponds to first, second and third engine thrust levels.
    Type: Grant
    Filed: June 15, 2007
    Date of Patent: March 6, 2012
    Assignee: The Boeing Company
    Inventors: Mark I. Nikolic, Barbara E. Holder
  • Publication number: 20100293454
    Abstract: A method is disclosed for generating a quick reference handbook for use on a mobile platform. The method may involve providing a machine-readable medium for use with a processor having a memory. The machine-readable medium may provide instructions for causing the processor to generate a quick reference handbook (QRH). The QRH may be created through the use of checklists organized in accordance with a plurality of grouping schemes that include at least a plurality of: Immediate Action; Systems; and Engine Indication and Crew Alerting System (EICAS) messages. Differentiating criteria may also be used for decisions steps, action steps, and navigation steps within the checklists to thereby enable a user to discriminate between the steps.
    Type: Application
    Filed: May 19, 2010
    Publication date: November 18, 2010
    Applicant: The Boeing Company
    Inventors: Barbara E. Holder, William A. McKenzie
  • Patent number: 7735005
    Abstract: Aspects of the present invention provide a style guide, formatting methods, and electronic/digital versions for quick reference handbooks (QRH) for mobile platforms. Using one or more of the style guide and formatting methods to create quick reference handbooks can provide improvements in safety through error and workload reduction during non-normal situations, improvements in operator understanding of checklists and information contained in the checklists, reduced customer changes needed to create an airline quick reference handbook, reduced documentation maintenance costs, and/or reduced training costs through standardized format and content.
    Type: Grant
    Filed: October 4, 2005
    Date of Patent: June 8, 2010
    Assignee: The Boeing Company
    Inventors: Barbara E. Holder, William A. McKenzie
  • Publication number: 20080312781
    Abstract: In accordance with an embodiment, a method includes displaying information corresponding to automatically controlled engine thrust levels during a reduced engine thrust period of flight of an aircraft. The information corresponds to one or more parameters associated with a flight control computer of the aircraft. In an alternate aspect, the displayed information includes alphanumeric information formatted in accordance with a sequential order of the automatically controlled engine thrust levels. In a further aspect, the alphanumeric information corresponds to first, second and third engine thrust levels.
    Type: Application
    Filed: June 15, 2007
    Publication date: December 18, 2008
    Applicant: The Boeing Company
    Inventors: Mark I. Nikolic, Barbara E. Holder