Patents by Inventor Daniel J. Fogarty

Daniel J. Fogarty 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: 10539955
    Abstract: A system is provided for integrating failure data for different failure analysis layouts. The system includes a data validator and layout engine. The data validator is configured to validate failure analysis data for a complex system including a plurality of systems. The failure analysis data includes failure data identifying failed systems, and design data describing the complex system and possible failures of at least some of its systems. In this regard, the data validator is configured to perform one or more consistency checks between the failure data and design data to thereby integrate the failure data for a plurality of different failure analysis layouts. The layout engine is in turn configured to selectively generate and communicate any one or more of the plurality of different layouts of the failure analysis data, with at least some of the failure analysis data being shared between at least some of the different layouts.
    Type: Grant
    Filed: June 15, 2012
    Date of Patent: January 21, 2020
    Assignee: The Boeing Company
    Inventors: Tyler Junichi Petri, Daniel J. Fogarty, David Harding Jones, Allison Moran, Kevin Nicholas King
  • Patent number: 10282896
    Abstract: A method for zone analysis. A zone is identified in a three-dimensional physical model of a vehicle. The three-dimensional physical model includes geometry information and location information for physical components. An effect of an undesired operation of a group of components in a zone within the three-dimensional physical model of the vehicle is identified based on the three-dimensional physical model of the vehicle and a logical model of the vehicle including a logical architecture linking logical components to each other. Logical components in the logical model are mapped to the physical components in the three-dimensional physical model of the vehicle.
    Type: Grant
    Filed: June 3, 2015
    Date of Patent: May 7, 2019
    Assignee: The Boeing Company
    Inventors: Tyler Junichi Petri, Daniel J. Fogarty, David H. Jones, Roger Keith Nicholson, Lars Fucke, Kimberly Motonaga, Kevin Nicholas King, Chad Richard Douglas
  • Patent number: 10180995
    Abstract: A failure-effect validation system includes an effects modeler configured to develop a cumulative effects model for failure modes of the complex system, and by which a model of the complex system is extendible to form an extended complex-system model. The effects modeler is also configured to develop search targets each of which includes logical expressions of notable hazards and other factors that contribute to the cumulative effects, such as crew workload, safety margin and/or physiological effects. A model analysis system is configured to perform an automated analysis using the extended complex-system model and search targets, and in which the automated analysis includes a graph search of possible states of the extended complex-system model to locate search targets. And the effects assessment system is configured to selectively generate a layout of failure analysis data including at least a portion of the extended complex-system model and results of the automated analysis.
    Type: Grant
    Filed: July 15, 2013
    Date of Patent: January 15, 2019
    Assignee: The Boeing Company
    Inventors: David H. Jones, Tyler J. Petri, Daniel J. Fogarty, Chad R. Douglas, Roger Nicholson, Lars Fucke, Stephen Sweeney, Ricardo M. Fricks, Kevin Nicholas King
  • Publication number: 20170161969
    Abstract: A system and method are disclosed for establishing hierarchal subcomponent sensor communication for a vehicle. A database includes information associated with a plurality of subcomponents having a sensor. A software modeling tool implements a safety model and a fault detection and isolation (FDI) model. The safety model determines a probability of a constraint being violated given a probability of failure of each subcomponent. The FDI model determines a probability associated with a risk exposure for known and unknown faults for each subcomponent. A processor identifies those subcomponent sensors that reduce risk-exposure based on probabilities generated using the safety model and FDI model and generates an output of a set of vehicle subcomponent sensors for connection to an vehicle communication system for communication at a higher level of hierarchy, such that the vehicle communication system can receive information indicative of a subcomponent fault and generate an alert about the fault.
    Type: Application
    Filed: December 7, 2015
    Publication date: June 8, 2017
    Inventors: Greg A. Kimberly, David H. Jones, Richard V. Robinson, Tyler J. Petri, Daniel J. Fogarty
  • Publication number: 20150019187
    Abstract: A failure-effect validation system includes an effects modeler configured to develop a cumulative effects model for failure modes of the complex system, and by which a model of the complex system is extendible to form an extended complex-system model. The effects modeler is also configured to develop search targets each of which includes logical expressions of notable hazards and other factors that contribute to the cumulative effects, such as crew workload, safety margin and/or physiological effects. A model analysis system is configured to perform an automated analysis using the extended complex-system model and search targets, and in which the automated analysis includes a graph search of possible states of the extended complex-system model to locate search targets. And the effects assessment system is configured to selectively generate a layout of failure analysis data including at least a portion of the extended complex-system model and results of the automated analysis.
    Type: Application
    Filed: July 15, 2013
    Publication date: January 15, 2015
    Applicant: The Boeing Company
    Inventors: David H. Jones, Tyler J. Petri, Daniel J. Fogarty, Chad R. Douglas, Roger Nicholson, Lars Fucke, Stephen Sweeney, Ricardo M. Fricks
  • Publication number: 20130339795
    Abstract: A system is provided for integrating failure data for different failure analysis layouts. The system includes a data validator and layout engine. The data validator is configured to validate failure analysis data for a complex system including a plurality of systems. The failure analysis data includes failure data identifying failed systems, and design data describing the complex system and possible failures of at least some of its systems. In this regard, the data validator is configured to perform one or more consistency checks between the failure data and design data to thereby integrate the failure data for a plurality of different failure analysis layouts. The layout engine is in turn configured to selectively generate and communicate any one or more of the plurality of different layouts of the failure analysis data, with at least some of the failure analysis data being shared between at least some of the different layouts.
    Type: Application
    Filed: June 15, 2012
    Publication date: December 19, 2013
    Applicant: The Boeing Company
    Inventors: Tyler Junichi Petri, Daniel J. Fogarty, David Harding Jones, Allison Moran, Kevin Nicholas King