Patents by Inventor Thomas Wingert

Thomas Wingert 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: 11060992
    Abstract: A probe system includes a heater and a control circuit. The heater includes a resistive heating element routed through the probe. An operational voltage is provided to the resistive heating element to provide heating for the probe. The control circuit is configured to provide a test voltage different than the operational voltage and monitor a test current generated in the resistive heating element while providing the test voltage. The control circuit is further configured to detect micro fractures in the resistive heating element based on the test current.
    Type: Grant
    Filed: March 24, 2017
    Date of Patent: July 13, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Ben Ping-Tao Fok, Thomas Wingert
  • Patent number: 10914777
    Abstract: A system and method for an aircraft includes a probe, first and second current sensors, and a control circuit. The probe includes a heater that includes a resistive heating element routed through the probe, wherein an operational current is provided to the resistive heating element to provide heating for the probe. The first current sensor is configured to sense a first current through the resistive heating element, and the second current sensor is configured to sense a second current through the resistive heating element. The control circuit is configured to determine a leakage current based on the first and second currents and determine a remaining useful life the probe based on the leakage current over time.
    Type: Grant
    Filed: June 15, 2017
    Date of Patent: February 9, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Magdi A. Essawy, Ben Ping-Tao Fok, Thomas Wingert
  • Publication number: 20180275085
    Abstract: A probe system includes a heater and a control circuit. The heater includes a resistive heating element routed through the probe. An operational voltage is provided to the resistive heating element to provide heating for the probe. The control circuit is configured to provide a test voltage different than the operational voltage and monitor a test current generated in the resistive heating element while providing the test voltage. The control circuit is further configured to detect micro fractures in the resistive heating element based on the test current.
    Type: Application
    Filed: March 24, 2017
    Publication date: September 27, 2018
    Inventors: Ben Ping-Tao Fok, Thomas Wingert
  • Publication number: 20180275185
    Abstract: A system and method for an aircraft includes a probe, first and second current sensors, and a control circuit. The probe includes a heater that includes a resistive heating element routed through the probe, wherein an operational current is provided to the resistive heating element to provide heating for the probe. The first current sensor is configured to sense a first current through the resistive heating element, and the second current sensor is configured to sense a second current through the resistive heating element. The control circuit is configured to determine a leakage current based on the first and second currents and determine a remaining useful life the probe based on the leakage current over time.
    Type: Application
    Filed: June 15, 2017
    Publication date: September 27, 2018
    Inventors: Magdi A. Essawy, Ben Ping-Tao Fok, Thomas Wingert