Patents by Inventor James Warren Hackler

James Warren Hackler 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: 7328623
    Abstract: A sensor assembly includes a housing and a tube. The housing has a first leading edge portion which is capable of being located in a compressor/fan inlet flow path and which includes an interior wall section. The tube has a proximal portion including an air inlet which is adapted to receive a compressor bleed air flow and a distal portion which is located in the housing and which includes at least one air outlet hole. The hole is spaced apart from the interior wall section and is aligned to direct at least some compressor bleed air flow to impinge against the interior wall section. The housing includes an opening which receives air from the flow path when the housing is located in the flow path, wherein the opening is adapted for fluid communication with a sensor, and wherein the sensor measures at least one of air temperature and air pressure.
    Type: Grant
    Filed: March 20, 2006
    Date of Patent: February 12, 2008
    Assignee: General Electric Company
    Inventors: Jason Corey Slagle, William Carl Ruehr, Jared Stephan Ashley, James Warren Hackler, Jansen James Litter, Meiyun Li, John Clisby Blanton
  • Publication number: 20020136631
    Abstract: A gas turbine engine including an active clearance control system that facilitates extending a useful life of a rotor assembly in a cost effective and reliable manner is described. The engine includes at least one rotor assembly and an engine casing that extends circumferentially around the rotor assembly, such that a tip clearance is defined between the rotor assembly and the engine casing. The clearance control system includes a plurality of panels that couple to extend circumferentially around the engine. Each clearance control system panel includes a circumferential feed duct that is formed integrally with the panel.
    Type: Application
    Filed: March 23, 2001
    Publication date: September 26, 2002
    Inventors: Scott Richard Zearbaugh, Steven Louis Brickner, James Warren Hackler, Lonnie Ray Chadwell
  • Patent number: 6454529
    Abstract: A gas turbine engine including an active clearance control system that facilitates extending a useful life of a rotor assembly in a cost effective and reliable manner is described. The engine includes at least one rotor assembly and an engine casing that extends circumferentially around the rotor assembly, such that a tip clearance is defined between the rotor assembly and the engine casing. The clearance control system includes a plurality of panels that couple to extend circumferentially around the engine. Each clearance control system panel includes a circumferential feed duct that is formed integrally with the panel.
    Type: Grant
    Filed: March 23, 2001
    Date of Patent: September 24, 2002
    Assignee: General Electric Company
    Inventors: Scott Richard Zearbaugh, Steven Louis Brickner, James Warren Hackler, Lonnie Ray Chadwell