Patents by Inventor Peter John Linko, III

Peter John Linko, 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).

  • Patent number: 6893225
    Abstract: An article made of a metallic material and comprising a body and a body end portion integral with the body, includes a band of the metallic material at the end portion substantially through the entire end portion, the band being under a compressive stress greater than the body. An example of the article is a turbine engine balding member in which the body is the airfoil of the member and the band is disposed at the radially outer tip portion of the airfoil. One method for providing the band includes performing roller deformation on the end portion until a desired amount of compressive stress is developed in the band substantially through the entire end portion.
    Type: Grant
    Filed: May 22, 2003
    Date of Patent: May 17, 2005
    Assignee: General Electric Company
    Inventors: David William Crall, Peter John Linko, III
  • Patent number: 6672838
    Abstract: An article made of a metallic material and comprising a body and a body end portion integral with the body, includes a band of the metallic material at the end portion substantially through the entire end portion, the band being under a compressive stress greater than the body. An example of the article is a turbine engine blading member in which the body is the airfoil of the member and the band is disposed at the radially outer tip portion of the airfoil. One method for providing the band includes performing roller deformation on the end portion until a desired amount of compressive stress is developed in the band substantially through the entire end portion.
    Type: Grant
    Filed: July 27, 2000
    Date of Patent: January 6, 2004
    Assignee: General Electric Company
    Inventors: David William Crall, Peter John Linko, III
  • Patent number: 6648596
    Abstract: A turbine blade or turbine vane includes a metallic nonfoam region, and a ceramic foam region joined to the metallic region. The ceramic foam region is an open-cell solid ceramic foam made of ceramic cell walls having an intracellular volume therebetween. The ceramic is preferably alumina. The intracellular volume may be empty porosity, or an intracellular metal such as an intracellular nickel-base superalloy.
    Type: Grant
    Filed: November 8, 2000
    Date of Patent: November 18, 2003
    Assignee: General Electric Company
    Inventors: Richard John Grylls, Curtiss Mitchell Austin, Peter John Linko, III