Patents by Inventor David Hackler

David Hackler 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).

  • METHOD FOR MANUFACTURING LIGHTWEIGHT COMPOSITE FAIRING BAR
    Publication number: 20080314516
    Abstract: A lightweight composite fairing bar (14) for use in fabricating a composite component (16) of an aircraft. The fairing bar (14) includes a core (18) and an elongated outer shell (20) surrounding the core (18). The outer shell (20) is comprised of a laminate material, and the core (18) is comprised of epoxy syntactic foam having a lower density than that of the laminate material. The outer shell (20) is configured for supporting the composite component (16) during the manufacture of the same.
    Type: Application
    Filed: July 29, 2008
    Publication date: December 25, 2008
    Applicant: THE BOEING COMPANY
    Inventors: Dennis Albright, David Hackler, Randall Clark
  • LIGHTWEIGHT COMPOSITE FAIRING BAR AN METHOD FOR MANUFACTURING THE SAME
    Publication number: 20060280927
    Abstract: A lightweight composite fairing bar (14) for use in fabricating a composite component (16) of an aircraft. The fairing bar (14) includes a core (18) and an elongated outer shell (20) surrounding the core (18). The outer shell (20) is comprised of a laminate material, and the core (18) is comprised of epoxy syntactic foam having a lower density than that of the laminate material. The outer shell (20) is configured for supporting the composite component (16) during the manufacture of the same.
    Type: Application
    Filed: June 13, 2005
    Publication date: December 14, 2006
    Applicant: THE BOEING COMPANY
    Inventors: Dennis Albright, David Hackler, Randall Clark
  • MANDREL, MANDREL REMOVAL AND MANDREL FABRICATION TO SUPPORT A MONOLITHIC NACELLE COMPOSITE PANEL
    Publication number: 20060225265
    Abstract: The present invention discloses a mandrel for fabricating a monolithic composite nacelle panel for use on an airplane. Also disclosed is the method of constructing the mandrel, the method of assembling the mandrel, and the method of disassembling the mandrel.
    Type: Application
    Filed: March 29, 2005
    Publication date: October 12, 2006
    Applicant: THE BOEING COMPANY
    Inventors: John Burnett, David Hackler, Timothy Wilson, John Welch, Thomas Popp, Christopher Sawyer, Leo Hoadley, Leroy Fulbright, Mitchel Granger, Barry Craig, Phillip Kenney