Patents by Inventor Greg PHELPS

Greg PHELPS 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: 10400616
    Abstract: A turbine nozzle apparatus includes: a vane extending between inner and outer bands, the interior of the vane being open and communicating with an aperture in the outer band, wherein the vane and the bands are part of a monolithic whole of low-ductility material; a metallic baffle inside the vane, the baffle having upper and lower ends and a peripheral wall including a plurality of impingement holes defining an interior space, closed off by an end wall at the lower end; and a metallic retainer having a body with a shape generally matching the shape of the aperture, the body bearing against the upper end of the impingement baffle and being connected to the outer band by a plurality of mechanical fasteners.
    Type: Grant
    Filed: June 18, 2014
    Date of Patent: September 3, 2019
    Assignee: General Electric Company
    Inventors: Michael Ray Tuertscher, Darell Glenn Senile, Greg Phelps
  • Patent number: 10180073
    Abstract: A turbine nozzle includes an arcuate inner band having opposed flowpath and back sides, and an aft flange extending outward from the back side; an arcuate outer band having opposed flowpath and back sides; an airfoil-shaped turbine vane extending between the flowpath sides of the inner and outer bands, wherein the inner and outer bands and the vane comprise a ceramic low-ductility material; and a metallic collar surrounding the aft flange.
    Type: Grant
    Filed: August 6, 2014
    Date of Patent: January 15, 2019
    Assignee: General Electric Company
    Inventors: Michael Ray Tuertscher, Darrell Glenn Senile, Greg Phelps
  • Publication number: 20160177759
    Abstract: A turbine nozzle includes an arcuate inner band having opposed flowpath and back sides, and an aft flange extending outward from the back side; an arcuate outer band having opposed flowpath and back sides; an airfoil-shaped turbine vane extending between the flowpath sides of the inner and outer bands, wherein the inner and outer bands and the vane comprise a ceramic low-ductility material; and a metallic collar surrounding the aft flange.
    Type: Application
    Filed: August 6, 2014
    Publication date: June 23, 2016
    Inventors: Michael Ray TUERTSCHER, Darrell Glenn SENILE, Greg PHELPS
  • Publication number: 20160153299
    Abstract: A turbine nozzle apparatus includes: a vane extending between inner and outer bands, the interior of the vane being open and communicating with an aperture in the outer band, wherein the vane and the bands are part of a monolithic whole of low-ductility material; a metallic baffle inside the vane, the baffle having upper and lower ends and a peripheral wall including a plurality of impingement holes defining an interior space, closed off by an end wall at the lower end; and a metallic retainer having a body with a shape generally matching the shape of the aperture, the body bearing against the upper end of the impingement baffle and being connected to the outer band by a plurality of mechanical fasteners.
    Type: Application
    Filed: June 18, 2014
    Publication date: June 2, 2016
    Inventors: Michael Ray TUERTSCHER, Darell Glenn SENILE, Greg PHELPS