Patents by Inventor Scott T. Fusare

Scott T. Fusare 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).

  • Monitoring systems and methods for aircraft landing gear
    Patent number: 8818739
    Abstract: A system and method for monitoring loads applied to aircraft landing gear structure. The method includes the step of interrogating at least one sensor positioned proximate the landing gear structure by way of data acquisition circuitry to yield strain data. The method further includes the step of instructing the data acquisition circuitry with respect to a sampling rate and data resolution for interrogation.
    Type: Grant
    Filed: October 14, 2011
    Date of Patent: August 26, 2014
    Assignee: Goodrich Corporation
    Inventors: Radoslaw R. Zakrzewski, Michael A. Lynch, Scott T. Fusare, Brandon Hicks, Bradley W. Baird
  • Wireless power transmission system and method for an aircraft sensor system
    Patent number: 8686590
    Abstract: An aircraft sensor system including a primary module configured to be attached to an aircraft portion and operative to transmit electrical power wirelessly. A secondary module configured to be attached to an aircraft component, the secondary module operative to receive electrical power wirelessly from the primary module. At least one sensor configured to be operatively attached to a portion of the aircraft component and electrically coupled to the secondary module, wherein the at least one sensor is operative to measure a desired parameter of the aircraft component.
    Type: Grant
    Filed: March 14, 2011
    Date of Patent: April 1, 2014
    Assignee: Simmonds Precision Products, Inc.
    Inventors: Robert S. Bugash, Scott T. Fusare
  • Wireless Power Transmission System and Method for an Aircraft Sensor System
    Publication number: 20120234971
    Abstract: An aircraft sensor system including a primary module configured to be attached to an aircraft portion and operative to transmit electrical power wirelessly. A secondary module configured to be attached to an aircraft component, the secondary module operative to receive electrical power wirelessly from the primary module. At least one sensor configured to be operatively attached to a portion of the aircraft component and electrically coupled to the secondary module, wherein the at least one sensor is operative to measure a desired parameter of the aircraft component.
    Type: Application
    Filed: March 14, 2011
    Publication date: September 20, 2012
    Applicant: Simmonds Precision Products, Inc.
    Inventors: Robert S. Bugash, Scott T. Fusare
  • MONITORING SYSTEMS AND METHODS FOR AIRCRAFT LANDING GEAR
    Publication number: 20120095703
    Abstract: A system and method for monitoring loads applied to aircraft landing gear structure. The method includes the step of interrogating at least one sensor positioned proximate the landing gear structure by way of data acquisition circuitry to yield strain data. The method further includes the step of instructing the data acquisition circuitry with respect to a sampling rate and data resolution for interrogation.
    Type: Application
    Filed: October 14, 2011
    Publication date: April 19, 2012
    Applicant: Goodrich Corporation
    Inventors: Radoslaw R. Zakrzewski, Michael A. Lynch, Scott T. Fusare, Brandon Hicks, Bradley W. Baird