Patents by Inventor Victor H. Reyes

Victor H. Reyes 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: 9688386
    Abstract: A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a first drive arm, a first drive link, and a support arm. A second linkage assembly couples the flap assembly and the first drive arm, and comprises a drive transfer arm, a middle connection segment, and a bullnose link.
    Type: Grant
    Filed: June 13, 2016
    Date of Patent: June 27, 2017
    Assignee: The Boeing Company
    Inventors: Seiya Sakurai, Stephen J. Fox, Victor H. Reyes
  • Publication number: 20160297513
    Abstract: A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a first drive arm, a first drive link, and a support arm. A second linkage assembly couples the flap assembly and the first drive arm, and comprises a drive transfer arm, a middle connection segment, and a bullnose link.
    Type: Application
    Filed: June 13, 2016
    Publication date: October 13, 2016
    Inventors: Seiya Sakurai, Stephen J. Fox, Victor H. Reyes
  • Patent number: 9365284
    Abstract: A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a first drive arm, a first drive link, and a support arm. A second linkage assembly couples the flap assembly and the first drive arm, and comprises a drive transfer arm, a middle connection segment, and a bullnose link.
    Type: Grant
    Filed: April 22, 2013
    Date of Patent: June 14, 2016
    Assignee: The Boeing Company
    Inventors: Seiya Sakurai, Stephen J. Fox, Victor H. Reyes
  • Publication number: 20140312175
    Abstract: A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a first drive arm, a first drive link, and a support arm. A second linkage assembly couples the flap assembly and the first drive arm, and comprises a drive transfer arm, a middle connection segment, and a bullnose link.
    Type: Application
    Filed: April 22, 2013
    Publication date: October 23, 2014
    Applicant: The Boeing Company
    Inventors: Seiya Sakurai, Stephen J. Fox, Victor H. Reyes