Patents by Inventor Huu-Thanh Tran

Huu-Thanh Tran 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: 9890644
    Abstract: A foundry core for manufacturing a blade of a turbomachine including a tip section offset, including a core element for forming various internal cavities, the core element including a leading-edge cavity internal core, central cavity internal cores, and a trailing-edge cavity internal core. The internal core for the central cavity adjacent to the internal core for the trailing-edge cavity includes a bulge extending toward the core for the leading-edge cavity.
    Type: Grant
    Filed: February 12, 2013
    Date of Patent: February 13, 2018
    Assignee: SNECMA
    Inventors: Huu-Thanh Tran, Michael Hansom, Christian Bariaud, Patrice Eneau
  • Patent number: 9410433
    Abstract: An inter-blade sealing for a turbine or compressor wheel of a turbine engine includes inserts engaged in longitudinal cavities in side edges of platforms of blades and bearing, in operation, against facing side edges of platforms of adjacent blades. Each insert has a cylindrical elongate shape and includes in its outer cylindrical surface at least one annular groove for passing platform cooling air.
    Type: Grant
    Filed: July 20, 2011
    Date of Patent: August 9, 2016
    Assignee: SNECMA
    Inventors: Damien Alquier, Jacques Auguste Amedee Boury, Pascal Courtin, Huu-Thanh Tran
  • Publication number: 20150132139
    Abstract: A foundry core for manufacturing a blade of a turbomachine including a tip section offset, including a core element for forming various internal cavities, the core element including a leading-edge cavity internal core, central cavity internal cores, and a trailing-edge cavity internal core. The internal core for the central cavity adjacent to the internal core for the trailing-edge cavity includes a bulge extending toward the core for the leading-edge cavity.
    Type: Application
    Filed: February 12, 2013
    Publication date: May 14, 2015
    Applicant: SNECMA
    Inventors: Huu-Thanh Tran, Michael Hansom, Christian Bariaud, Patrice Eneau
  • Publication number: 20140369844
    Abstract: A method of machining a blade in a three-dimensional machining center, the blade including an airfoil, a platform including upstream and downstream supports formed respectively under the upstream and downstream portions thereof for supporting a sealing liner, a blade root, and a stilt interposed between the platform and the blade root, the method including the upstream and downstream supports constituting two bearing points for a six-point positioning system for positioning the blade in the three-dimensional machining center.
    Type: Application
    Filed: January 24, 2013
    Publication date: December 18, 2014
    Applicant: SNECMA
    Inventors: Michael Hansom, Huu-Thanh Tran, Christian Bariaud
  • Publication number: 20130121810
    Abstract: An inter-blade sealing for a turbine or compressor wheel of a turbine engine includes inserts engaged in longitudinal cavities in side edges of platforms of blades and bearing, in operation, against facing side edges of platforms of adjacent blades. Each insert has a cylindrical elongate shape and includes in its outer cylindrical surface at least one annular groove for passing platform cooling air.
    Type: Application
    Filed: July 20, 2011
    Publication date: May 16, 2013
    Applicant: SNECMA
    Inventors: Damien Alquier, Jacques Auguste Amedee Boury, Pascal Courtin, Huu-Thanh Tran