Patents by Inventor Jackie Lee King

Jackie Lee King 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).

  • Publication number: 20100000468
    Abstract: A method and masking assembly for masking a dovetail portion of a turbine blade during coating of an airfoil portion of the blade. The masking assembly comprises at least two masking members, each having an exterior surface and an oppositely-disposed undulatory surface complementary to one of oppositely-disposed undulatory surfaces of the dovetail portion. By mating the masking members, the undulatory surfaces thereof define an interior cavity within the masking assembly that accommodates the dovetail portion, and the undulatory surfaces of the masking members contact the undulatory surfaces of the dovetail portion to entrap the dovetail portion within the interior cavity of the masking assembly.
    Type: Application
    Filed: July 28, 2009
    Publication date: January 7, 2010
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Matthew David Saylor, Jackie Lee King
  • Patent number: 7632541
    Abstract: A method and masking assembly for masking a dovetail portion of a turbine blade during coating of an airfoil portion of the blade. The masking assembly comprises at least two masking members, each having an exterior surface and an oppositely-disposed undulatory surface complementary to one of oppositely-disposed undulatory surfaces of the dovetail portion. By mating the masking members, the undulatory surfaces thereof define an interior cavity within the masking assembly that accommodates the dovetail portion, and the undulatory surfaces of the masking members contact the undulatory surfaces of the dovetail portion to entrap the dovetail portion within the interior cavity of the masking assembly.
    Type: Grant
    Filed: March 13, 2006
    Date of Patent: December 15, 2009
    Assignee: General Electric Company
    Inventors: Matthew David Saylor, Jackie Lee King
  • Publication number: 20090252872
    Abstract: A method and masking assembly for masking a dovetail portion of a turbine blade during coating of an airfoil portion of the blade. The masking assembly comprises at least two masking members, each having an exterior surface and an oppositely-disposed undulatory surface complementary to one of oppositely-disposed undulatory surfaces of the dovetail portion. By mating the masking members, the undulatory surfaces thereof define an interior cavity within the masking assembly that accommodates the dovetail portion, and the undulatory surfaces of the masking members contact the undulatory surfaces of the dovetail portion to entrap the dovetail portion within the interior cavity of the masking assembly.
    Type: Application
    Filed: March 13, 2006
    Publication date: October 8, 2009
    Applicant: General Electric Company
    Inventors: Matthew David Saylor, Jackie Lee King
  • Patent number: 6933012
    Abstract: A surface of an article is protected by coating the surface with a silicon-containing coating by preparing a coating mixture of silicon, a halide activator, and an oxide powder, positioning the surface of the article in gaseous communication with the coating mixture, and heating the surface of the article and the coating mixture to a coating temperature of from about 1150° F. to about 1500° F. The article is preferably a component of a gas turbine engine made of a nickel-base superalloy.
    Type: Grant
    Filed: December 13, 2002
    Date of Patent: August 23, 2005
    Assignee: General Electric Company
    Inventors: Nripendra Nath Das, Bangalore Aswatha Nagaraj, Matthew David Saylor, Jackie Lee King
  • Publication number: 20040115467
    Abstract: A surface of an article is protected by coating the surface with a silicon-containing coating by preparing a coating mixture of silicon, a halide activator, and an oxide powder, positioning the surface of the article in gaseous communication with the coating mixture, and heating the surface of the article and the coating mixture to a coating temperature of from about 1150° F. to about 1500° F. The article is preferably a component of a gas turbine engine made of a nickel-base superalloy.
    Type: Application
    Filed: December 13, 2002
    Publication date: June 17, 2004
    Inventors: Nripendra Nath Das, Bangalore Aswatha Nagaraj, Matthew David Saylor, Jackie Lee King