Patents by Inventor Bryan H. Farrar

Bryan H. Farrar 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: 20210102469
    Abstract: A vane arc segment includes a continuous airfoil piece that defines first and second platforms and an airfoil section that extends between the first and second platforms. The airfoil section has a pressure side and a suction side. The first platform defines axially-sloped suction and pressure side circumferential mate faces, first and second axial sides, a gaspath side, a non-gaspath side, and a flange that projects from the non-gaspath side. The flange extends along at least a portion the axially-sloped suction side circumferential mate face.
    Type: Application
    Filed: October 4, 2019
    Publication date: April 8, 2021
    Inventors: Jon E. Sobanski, Howard J. Liles, Bryan H. Farrar, Cheng Gao
  • Publication number: 20210001511
    Abstract: A method of forming a ceramic matrix composite component with cooling channels includes embedding a plurality of wires into a preform structure, densifying the preform structure with embedded wires, and removing the plurality of wires to create a plurality of corresponding channels within the densified structure.
    Type: Application
    Filed: July 5, 2019
    Publication date: January 7, 2021
    Inventors: Lei Jin, Zachary P. Konopaske, Ryan M. Brodeur, Howard J. Liles, Bryan H. Farrar, Andrew J. Lazur
  • Patent number: 10724387
    Abstract: A stator vane may comprise an airfoil extending between a first platform and a second platform, a first shear tube may extend through the airfoil and relatively orthogonal to the first platform and the second platform, wherein the first shear tube extends through the first platform and the second platform. In various embodiments, a second shear tube may extend through the airfoil into the first platform and the second platform parallel the first shear tube.
    Type: Grant
    Filed: November 8, 2018
    Date of Patent: July 28, 2020
    Assignee: RAYTHEON TECHNOLOGIES CORPORATION
    Inventors: Bryan H. Farrar, Howard J. Liles, Michael G McCaffrey, Andrew J. Lazur
  • Publication number: 20200232332
    Abstract: A stator vane may comprise an airfoil extending between a first platform and a second platform, the airfoil including a core extending relatively orthogonal to the first platform and the second platform, at least one of the first platform or second platform comprising a frustic load transmission feature, wherein the frustic load transmission feature comprises at least a first angular surface disposed proximate a platform edge, wherein the first angular surface is defined by a non-orthogonal angle ? with respect to an outer platform surface.
    Type: Application
    Filed: January 17, 2019
    Publication date: July 23, 2020
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Bryan H. Farrar, Andrew J. Lazur, Howard J. Liles, Bryan P. Dube
  • Publication number: 20200149423
    Abstract: A stator vane may comprise an airfoil extending between a first platform and a second platform, a first shear tube may extend through the airfoil and relatively orthogonal to the first platform and the second platform, wherein the first shear tube extends through the first platform and the second platform. In various embodiments, a second shear tube may extend through the airfoil into the first platform and the second platform parallel the first shear tube.
    Type: Application
    Filed: November 8, 2018
    Publication date: May 14, 2020
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Bryan H. Farrar, Howard J. Liles, Michael G. McCaffrey, Andrew J. Lazur