Patents by Inventor Andrew Hayes Thompson

Andrew Hayes Thompson 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: 6293085
    Abstract: The present invention is addressed to a control logic for determining the occurrence of shaft decoupling in a gas turbine engine. The control logic in the preferred embodiment receives inputs for shaft rotational speed and/or compressor pressure and uses these parameters for making a determination of shaft decoupling in fractions of a second, before serious damage to the gas turbine engine can occur. The control logic also utilizes multiple interval sampling, and sampling over multiple channels to verify any determination of shaft decoupling. Once a shaft decouple has been verified, fuel flow to the engine is cut off, thus shutting down the engine.
    Type: Grant
    Filed: November 29, 2000
    Date of Patent: September 25, 2001
    Assignee: Pratt & Whitney Canada Corp.
    Inventors: Andrew Hayes Thompson, Carmine Lisio, Antonio Hernani Nobre
  • Publication number: 20010000090
    Abstract: The present invention is addressed to a control logic for determining the occurrence of shaft decoupling in a gas turbine engine. The control logic in the preferred embodiment receives inputs for shaft rotational speed and/or compressor pressure and uses these parameters for making a determination of shaft decoupling in fractions of a second, before serious damage to the gas turbine engine can occur. The control logic also utilizes multiple interval sampling, and sampling over multiple channels to verify any determination of shaft decoupling. Once a shaft decouple has been verified, fuel flow to the engine is cut off, thus shutting down the engine.
    Type: Application
    Filed: November 29, 2000
    Publication date: April 5, 2001
    Inventors: Andrew Hayes Thompson, Carmine Lisio, Antonio Nobre
  • Patent number: 6176074
    Abstract: The present invention is addressed to a control logic for determining the occurrence of shaft decoupling in a gas turbine engine. The control logic in the preferred embodiment receives inputs for shaft rotational speed and/or compressor pressure and uses these parameters for making a determination of shaft decoupling in fractions of a second, before serious damage to the gas turbine engine can occur. The control logic also utilizes multiple interval sampling, and sampling over multiple channels to verify any determination of shaft decoupling. Once a shaft decouple has been verified, fuel flow to the engine is cut off, thus shutting down the engine.
    Type: Grant
    Filed: June 5, 1998
    Date of Patent: January 23, 2001
    Assignee: Pratt & Whitney Canada Corp.
    Inventors: Andrew Hayes Thompson, Carmine Lisio, Antonio Hernani Nobre