Patents by Inventor Matteo Borghini-Lilli

Matteo Borghini-Lilli 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).

  • Structural component
    Patent number: 9434463
    Abstract: A structural component, in particular for an aircraft, having a skin and at least one stiffening element for stiffening the skin. Opposite to a run-out of the stiffening element at least one supporting element is positioned. The at least one supporting element defines a supporting area that is opened to the stiffening element run-out in longitudinal direction of the stiffening element run-out and that is closed in transversal direction of the stiffening element run-out.
    Type: Grant
    Filed: September 9, 2013
    Date of Patent: September 6, 2016
    Assignee: Airbus Operations GmbH
    Inventors: Matteo Borghini-Lilli, Marc'Antonio Bentivoglio, Henrik-Bro Henriksen, Ruslan Zagreba
  • Structural component
    Publication number: 20140072769
    Abstract: A structural component, in particular for an aircraft, having a skin and at least one stiffening element for stiffening the skin. Opposite to a run-out of the stiffening element at least one supporting element is positioned. The at least one supporting element defines a supporting area that is opened to the stiffening element run-out in longitudinal direction of the stiffening element run-out and that is closed in transversal direction of the stiffening element run-out.
    Type: Application
    Filed: September 9, 2013
    Publication date: March 13, 2014
    Inventors: Matteo Borghini-Lilli, Marc'Antonio Bentivoglio, Henrik-Bro Henriksen, Ruslan Zagreba
  • STRINGER
    Publication number: 20120100343
    Abstract: A laminated composite stringer having a termination at one end in its longitudinal direction, and including a laminated stack of composite structural plies, wherein internal plies in the stack are terminated consecutively towards the stringer termination to provide a taper of reducing stack thickness. Also, a composite structure comprising a panel and the stringer; and a method of manufacturing the stringer. The composite structure may be used in aircraft.
    Type: Application
    Filed: July 5, 2010
    Publication date: April 26, 2012
    Inventors: Matteo Borghini-Lilli, Paul Hadley, Nathan Phillips