Patents by Inventor George Gould Cunningham, III

George Gould Cunningham, III 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).

  • Publication number: 20170321600
    Abstract: The gas turbine power generation system includes a core engine and a low pressure compressor. The core engine includes a high pressure compressor, a combustor, and a high pressure turbine configured in a serial flow arrangement. The high pressure compressor and the high pressure turbine are coupled together by a first shaft. The low pressure compressor is positioned axially forward of the core engine and is coupled to the first shaft.
    Type: Application
    Filed: May 6, 2016
    Publication date: November 9, 2017
    Inventors: Thomas Ory Moniz, George Gould Cunningham, III, Joseph George Rose
  • Patent number: 9518513
    Abstract: A gas turbine engine variable bleed apparatus includes a variable bleed valve door disposed in a bleed inlet in a transition duct, rotatable about two or more separate pivot points, operable to open and close an aft bleed slot extending outwardly from transition duct, and operable to open and close a forward bleed slot extending inwardly into transition duct. Door is operable to transition between a first position with aft bleed slot open and forward bleed slot closed to a second position with aft bleed slot closed and forward bleed slot open without fully closing door. Door is rotatable about an axis translatable between the two or more separate pivot points. Transition duct having a transition duct conical angle at least about 10 degrees greater than a booster conical angle of a booster outer shroud upstream of transition duct.
    Type: Grant
    Filed: January 25, 2013
    Date of Patent: December 13, 2016
    Assignee: General Electric Company
    Inventors: Byron Andrew Pritchard, Jr., Paul Alfred Pezzi, George Gould Cunningham, III, Thomas Ory Moniz, Steven Alan Ross, Raymond Gust Holm
  • Publication number: 20140245747
    Abstract: A gas turbine engine variable bleed apparatus includes a variable bleed valve door disposed in a bleed inlet in a transition duct, rotatable about two or more separate pivot points, operable to open and close an aft bleed slot extending outwardly from transition duct, and operable to open and close a forward bleed slot extending inwardly into transition duct. Door is operable to transition between a first position with aft bleed slot open and forward bleed slot closed to a second position with aft bleed slot closed and forward bleed slot open without fully closing door. Door is rotatable about an axis translatable between the two or more separate pivot points. Transition duct having a transition duct conical angle at least about 10 degrees greater than a booster conical angle of a booster outer shroud upstream of transition duct.
    Type: Application
    Filed: January 25, 2013
    Publication date: September 4, 2014
    Applicant: General Electric Company
    Inventors: Byron Andrew Pritchard, JR., Paul Alfred Pezzi, George Gould Cunningham, III, Thomas Ory Moniz, Steven Alan Ross, Raymond Gust Holm