Patents by Inventor Tom Brotherton

Tom Brotherton 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: 9446861
    Abstract: A method for health monitoring for an aircraft includes the steps of obtaining vibration data for the aircraft, obtaining navigation data for the aircraft, and determining a measure of health of the aircraft using the vibration data and the navigation data.
    Type: Grant
    Filed: January 7, 2014
    Date of Patent: September 20, 2016
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Jeffery A. Goodrich, Paul Grabill, Tom Brotherton, Robert H. Luppold
  • Publication number: 20140114527
    Abstract: A method for health monitoring for an aircraft includes the steps of obtaining vibration data for the aircraft, obtaining navigation data for the aircraft, and determining a measure of health of the aircraft using the vibration data and the navigation data.
    Type: Application
    Filed: January 7, 2014
    Publication date: April 24, 2014
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Jeffery A. Goodrich, Paul Grabill, Tom Brotherton, Robert H. Luppold
  • Patent number: 8682509
    Abstract: A system to monitor aircraft equipment, having a chassis, defining an interior compartment, an arrangement configured to accept input data of at least one aircraft parameter, the arrangement configured to be placed within an aircraft, crash survivable cockpit voice and flight data recorder, and a power supply arrangement connected to arrangement configured to accept input data and the recorder.
    Type: Grant
    Filed: February 15, 2008
    Date of Patent: March 25, 2014
    Assignee: Honeywell International Inc.
    Inventors: Jeffrey A. Goodrich, Robert H. Luppold, Tom Brotherton, Paul Grabill
  • Patent number: 8666569
    Abstract: A method for health monitoring for an aircraft includes the steps of obtaining vibration data for the aircraft, obtaining navigation data for the aircraft, and determining a measure of health of the aircraft using the vibration data and the navigation data.
    Type: Grant
    Filed: November 10, 2009
    Date of Patent: March 4, 2014
    Assignee: Honeywell International Inc.
    Inventors: Jeff Goodrich, Paul Grabill, Tom Brotherton, Rob Luppold
  • Patent number: 8521341
    Abstract: A method for fault determination for an aircraft includes the steps of generating a predicted maneuver of the aircraft using an aircraft operating input and a model of aircraft performance, determining an actual maneuver of the aircraft using information obtained from an inertial measurement system, comparing the predicted maneuver and the actual maneuver, and determining a fault of the aircraft based on the comparison of the predicted maneuver and the actual maneuver.
    Type: Grant
    Filed: June 26, 2009
    Date of Patent: August 27, 2013
    Assignee: Honeywell International Inc.
    Inventor: Tom Brotherton
  • Publication number: 20110020122
    Abstract: A computer implemented method includes receiving condition information from a plurality of condition detection sensors coupled to a wind turbine and receiving wind turbine controller information. An anomaly detection algorithm is applied to identify maintenance activities for the wind turbine as a function of both the wind turbine condition information and the wind turbine controller information.
    Type: Application
    Filed: July 22, 2010
    Publication date: January 27, 2011
    Applicant: Honeywell International Inc.
    Inventors: Girija Parthasarathy, Wendy Foslien Graber, Tom Brotherton
  • Publication number: 20100332053
    Abstract: A method for fault determination for an aircraft includes the steps of generating a predicted maneuver of the aircraft using an aircraft operating input and a model of aircraft performance, determining an actual maneuver of the aircraft using information obtained from an inertial measurement system, comparing the predicted maneuver and the actual maneuver, and determining a fault of the aircraft based on the comparison of the predicted maneuver and the actual maneuver.
    Type: Application
    Filed: June 26, 2009
    Publication date: December 30, 2010
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventor: Tom Brotherton
  • Publication number: 20100057277
    Abstract: A method for health monitoring for an aircraft includes the steps of obtaining vibration data for the aircraft, obtaining navigation data for the aircraft, and determining a measure of health of the aircraft using the vibration data and the navigation data.
    Type: Application
    Filed: November 10, 2009
    Publication date: March 4, 2010
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Jeff Goodrich, Paul Grabill, Tom Brotherton, Rob Luppold