Patents by Inventor Gary Joseph Drlik

Gary Joseph Drlik 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: 6397604
    Abstract: In a land based gas turbine including a compressor, a combustor and turbine section including at least three stages, an improvement comprising an inlet into a third stage nozzle from the compressor for feeding cooling air from the compressor to the third stage nozzle; at least one passageway running substantially radially through each airfoil of the third stage nozzle and an associated diaphragm, into an annular space between the rotor and the diaphragm; and passageways communicating between the annular space and individual buckets of the third stage.
    Type: Grant
    Filed: February 1, 2001
    Date of Patent: June 4, 2002
    Assignee: General Electric Company
    Inventors: Sacheverel Quentin Eldrid, James Lee Burns, Gene David Palmer, Sal Albert Leone, Gary Joseph Drlik, Edward Eugene Gibler
  • Patent number: 6321447
    Abstract: The concentric wrench includes an outer tube having flats at one end and a gripping surface at an opposite end. An inner tube has interior flats at one end and a gripping surface at its opposite end. With the inner and outer tubes disposed about a pressure transmitting conduit, the tubes may be inserted into a blind access opening in the outer turbine casing to engage the flats of the tubes against hex nuts of an internal fitting. By relatively rotating the tubes using the externally exposed gripping surfaces, the threaded connection between the parts of the fitting bearing the respective hex nuts can be tightened or loosened.
    Type: Grant
    Filed: March 13, 2000
    Date of Patent: November 27, 2001
    Assignee: General Electric Company
    Inventors: Kurt Neal Laurer, Gary Joseph Drlik, Edward Eugene Gibler
  • Publication number: 20010025476
    Abstract: In a land based gas turbine including a compressor, a combustor and turbine section including at least three stages, an improvement comprising an inlet into a third stage nozzle from the compressor for feeding cooling air from the compressor to the third stage nozzle; at least one passageway running substantially radially through each airfoil of the third stage nozzle and an associated diaphragm, into an annular space between the rotor and the diaphragm; and passageways communicating between the annular space and individual buckets of the third stage.
    Type: Application
    Filed: February 1, 2001
    Publication date: October 4, 2001
    Applicant: General Electric Company
    Inventors: Sacheverel Quentin Eldrid, James Lee Burns, Gene David Palmer, Sal Albert Leone, Gary Joseph Drlik, Edward Eugene Gibler