Patents by Inventor David R. Wiley

David R. Wiley 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: 8707799
    Abstract: A method for manufacturing an apparatus with a flow passage includes providing a preform apparatus with a preform flow passage. Flow area of the preform flow passage is determined to provide determined flow area data. The determined flow area data is compared to reference flow area data to provide flow area comparison data. The preform apparatus is chemical milled based on the flow area comparison data.
    Type: Grant
    Filed: September 30, 2011
    Date of Patent: April 29, 2014
    Assignee: United Technologies Corporation
    Inventors: David R. Wiley, Reed A. Kakuska
  • Patent number: 8572979
    Abstract: A combustor liner cap assembly is provided for use in a multiple fuel nozzle combustor of a gas turbine. The combustor liner cap assembly includes a tube plate having a plurality of fuel nozzle openings and a plurality of open ended premix tubes extending aft from the tube plate. Each premix tube has a forward end having a forward edge, the forward end being received in a corresponding one of the fuel nozzle openings. Each premix tube is secured to the tube plate aft of the forward edge of the forward end of the premix tube, for example, metallurgically bonded, such as by welding or brazing, to the tube plate or threaded into the tube plate.
    Type: Grant
    Filed: June 24, 2010
    Date of Patent: November 5, 2013
    Assignee: United Technologies Corporation
    Inventors: Craig F. Smith, Hannes A. Alholm, Jonathan J. Eastwood, Dennis J. Duhamel, David A. Burns, Claude I. Barnett, Jr., Randy J. Danburg, Jeffrey D. Melman, David R. Wiley, Monica Pacheco-Tougas
  • Publication number: 20130085592
    Abstract: A method for manufacturing an apparatus with a flow passage includes providing a preform apparatus with a preform flow passage. Flow area of the preform flow passage is determined to provide determined flow area data. The determined flow area data is compared to reference flow area data to provide flow area comparison data. The preform apparatus is chemical milled based on the flow area comparison data.
    Type: Application
    Filed: September 30, 2011
    Publication date: April 4, 2013
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: David R. Wiley, Reed A. Kakuska
  • Publication number: 20110314823
    Abstract: A combustor liner cap assembly is provided for use in a multiple fuel nozzle combustor of a gas turbine. The combustor liner cap assembly includes a tube plate having a plurality of fuel nozzle openings and a plurality of open ended premix tubes extending aft from the tube plate. Each premix tube has a forward end having a forward edge, the forward end being received in a corresponding one of the fuel nozzle openings. Each premix tube is secured to the tube plate aft of the forward edge of the forward end of the premix tube, for example, metallurgically bonded, such as by welding or brazing, to the tube plate or threaded into the tube plate.
    Type: Application
    Filed: June 24, 2010
    Publication date: December 29, 2011
    Applicant: United Technologies Corporation
    Inventors: Craig F. Smith, Hannes A. Alholm, Jonathan J. Eastwood, Dennis J. Duhamel, David A. Burns, Claude I. Barnett, JR., Randy J. Danburg, Jeffrey D. Melman, David R. Wiley, Monica Pacheco-Tougas