Patents by Inventor Dalero Winston Berkeley

Dalero Winston Berkeley 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: 8751413
    Abstract: A bearing monitoring system includes at least one sensor, and a fuzzy logic enabled device operatively connected to the at least one sensor. The fuzzy logic enabled device includes a fuzzy logic rule set that is configured and disposed to determine a component condition based on an input from the at least one sensor.
    Type: Grant
    Filed: July 26, 2011
    Date of Patent: June 10, 2014
    Assignee: General Electric Company
    Inventors: Roopesh Bhaskaran Nagathil, Dalero Winston Berkeley, David Lynn Linkenauger, Jason Fredrick Nichols
  • Publication number: 20130031043
    Abstract: A bearing monitoring system includes at least one sensor, and a fuzzy logic enabled device operatively connected to the at least one sensor. The fuzzy logic enabled device includes a fuzzy logic rule set that is configured and disposed to determine a component condition based on an input from the at least one sensor.
    Type: Application
    Filed: July 26, 2011
    Publication date: January 31, 2013
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Roopesh Bhaskaran Nagathil, Dalero Winston Berkeley, David Lynn Linkenauger, Jason Fredrick Nichols
  • Patent number: 6907738
    Abstract: A pilot air system for a combustor of a gas turbine including: a pilot air compressor having inlet connectable to in to a main passageway, wherein the main passageway receives compressed air from a compressor for the gas turbine; a pilot air platform positioned adjacent to the combustor of the gas turbine, wherein the pilot air compressor is positioned on the platform; an inline throttling valve coupled to the first main passageway; a by-pass passageway for the pilot air, proximate to the platform, and arranged in parallel to the main passageway and compressor, wherein the by-pass passageway receives pilot air from the main passageway downstream of the pilot air compressor and passes a portion of the compressed pilot air to the main passageway upstream of the pilot air compressor; a by-pass throttling valve inline with the by-pass passageway to meter pilot air flowing through the by-pass passageway, and the main passageway having an outlet connectable to the combustor.
    Type: Grant
    Filed: April 19, 2004
    Date of Patent: June 21, 2005
    Assignee: General Electric Company
    Inventors: Dalero Winston Berkeley, Robert A. McLeod, Michael Paul Black, Doug Dean
  • Patent number: 6901761
    Abstract: A pilot air system for providing pilot air to a combustor of a gas turbine wherein the system includes: an inlet to receive a portion of compressed air discharged by a compressor of the gas turbine, wherein the portion of the compressed air is pilot air; a main passageway coupled to the inlet and providing a passage for the pilot air; an inline throttling valve coupled to the main passageway and metering a pressure of the compressed air in the main passageway; a pilot air compressor in series with the main passageway; a by-pass passageway for the pilot air and arranged in parallel to the main passageway and compressor, wherein the by-pass passageway receives pilot air from the main passageway downstream of the compressor and passes a portion of the compressed pilot air to the main passageway upstream of the compressor; a by-pass throttling valve inline with the by-pass passageway to meter pilot air flowing through said by-pass passageway, and the main passageway is connectable to the combustor.
    Type: Grant
    Filed: February 24, 2004
    Date of Patent: June 7, 2005
    Assignee: General Electric Company
    Inventors: Dalero Winston Berkeley, Robert A. McLeod, Michael Paul Black, Doug Dean