Patents Assigned to Turbine Engine Components Technologies Corporation
  • Patent number: 9050671
    Abstract: An apparatus is configured for use with an electrode and a CNC machine tool. The apparatus includes a holder configured to hold the electrode in a position projecting outward from the holder, and a pull stud configured to mount the holder on the CNC machine tool. The apparatus further includes a driving mechanism that is operative to provide a motive force, and a coupling configured to couple the holder with the driving mechanism when the holder is not mounted on the CNC machine tool. The holder is configured to transmit the motive force from the coupling to the electrode in the holder to move the electrode outward of the holder.
    Type: Grant
    Filed: September 28, 2011
    Date of Patent: June 9, 2015
    Assignee: Turbine Engine Components Technologies Corporation
    Inventors: Louis Christian Bigelow, Sami R. Hermes
  • Patent number: 8256118
    Abstract: A metal leading edge of a turbine fan blade is manufactured by cutting and shaping an elongated metal part. The metal part has front and rear edges extending lengthwise of the part, and has a generally wedge-shaped transverse cross-section with opposite sides diverging from the front edge toward the rear edge. A cavity is cut inward from the rear edge toward the front edge. This provides the part with a generally V-shaped transverse cross-section having opposite side walls diverging rearwardly from the front edge. A mandrel is inserted into the cavity, and the side walls of the V-shaped part are deflected toward each other to constrict the cavity into the configuration of the mandrel. The part is then mounted as a metal leading edge by inserting a turbine fan blade component into the constricted cavity and fastening the part to the component.
    Type: Grant
    Filed: September 27, 2010
    Date of Patent: September 4, 2012
    Assignee: Turbine Engine Components Technologies Corporation
    Inventor: Jerald C. Cammer
  • Publication number: 20110010937
    Abstract: A metal leading edge of a turbine fan blade is manufactured by cutting and shaping an elongated metal part. The metal part has front and rear edges extending lengthwise of the part, and has a generally wedge-shaped transverse cross-section with opposite sides diverging from the front edge toward the rear edge. A cavity is cut inward from the rear edge toward the front edge. This provides the part with a generally V-shaped transverse cross-section having opposite side walls diverging rearwardly from the front edge. A mandrel is inserted into the cavity, and the side walls of the V-shaped part are deflected toward each other to constrict the cavity into the configuration of the mandrel. The part is then mounted as a metal leading edge by inserting a turbine fan blade component into the constricted cavity and fastening the part to the component.
    Type: Application
    Filed: September 27, 2010
    Publication date: January 20, 2011
    Applicant: Turbine Engine Components Technologies Corporation
    Inventor: Jerald C. Cammer
  • Patent number: 7805839
    Abstract: A metal leading edge of a turbine fan blade is manufactured by cutting and shaping an elongated metal part. The metal part has front and rear edges extending lengthwise of the part, and has a generally wedge-shaped transverse cross-section with opposite sides diverging from the front edge toward the rear edge. A cavity is cut inward from the rear edge toward the front edge. This provides the part with a generally V-shaped transverse cross-section having opposite side walls diverging rearwardly from the front edge. A mandrel is inserted into the cavity, and the side walls of the V-shaped part are deflected toward each other to constrict the cavity into the configuration of the mandrel. The part is then mounted as a metal leading edge by inserting a turbine fan blade component into the constricted cavity and fastening the part to the component.
    Type: Grant
    Filed: December 31, 2007
    Date of Patent: October 5, 2010
    Assignee: Turbine Engine Components Technologies Corporation
    Inventor: Jerald C Cammer