Patents by Inventor Timothy Lee Siebert

Timothy Lee Siebert 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: 7434313
    Abstract: A repaired turbine engine stationary vane assembly, including at least one airfoil bonded between inner and outer bands, is provided by a method of providing first and second vane assembly members bonded at respective circumferential edges, for example by brazing or welding. The first vane assembly member includes the outer band, the airfoil, an inner flange, and a first segment of the inner band with a first edge, spaced from the flange and extending between and through inner band circumferential edge portions. The second vane assembly member includes a second segment of the inner band including a second edge of shape and size matched with the first edge and extending through the inner band circumferential edge portions.
    Type: Grant
    Filed: December 22, 2005
    Date of Patent: October 14, 2008
    Assignee: General Electric Company
    Inventors: Paul D. Dasilva, Timothy Lee Siebert, Gregory Matthew Ford
  • Publication number: 20070147991
    Abstract: A repaired turbine engine stationary vane assembly, including at least one airfoil bonded between inner and outer bands, is provided by a method of providing first and second vane assembly members bonded at respective circumferential edges, for example by brazing or welding. The first vane assembly member includes the outer band, the airfoil, an inner flange, and a first segment of the inner band with a first edge, spaced from the flange and extending between and through inner band circumferential edge portions. The second vane assembly member includes a second segment of the inner band including a second edge of shape and size matched with the first edge and extending through the inner band circumferential edge portions.
    Type: Application
    Filed: December 22, 2005
    Publication date: June 28, 2007
    Inventors: Paul D. Dasilva, Timothy Lee Siebert, Gregory Matthew Ford
  • Patent number: 7172389
    Abstract: A method is provided for making a repaired turbine engine stationary vane assembly including at least one airfoil bonded between spaced apart first and second platforms. The method comprises providing a first vane assembly member including at least a portion of the first platform, the airfoil, and a first segment of the second platform bonded with the airfoil. Also provided is a second vane assembly member including a second segment of the second platform with a recess of a shape and size sufficient to receive the first segment of the second platform. The first segment is placed in the recess after which the first and second segments are bonded, for example by brazing or welding. Provided is a more structurally sound repaired turbine engine stationary vane assembly including the first and second vane assembly members bonded together.
    Type: Grant
    Filed: November 16, 2004
    Date of Patent: February 6, 2007
    Assignee: General Electric Company
    Inventors: Michael Philip Hagle, Timothy Lee Siebert, Jeffrey John Reverman, Dana Leigh Ferguson, Gregory Matthew Ford