Patents by Inventor Jerome Colmagro

Jerome Colmagro 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).

  • Connector for stiffening frames between an aircraft fuselage and a wing box
    Patent number: 8746621
    Abstract: The stiffening frames (14) of an aircraft fuselage (2) remain continuous while passing through an upper panel (5) of the wing box and extend over the ribs (3) situated in that box. The overall mechanical strength of the assembly is improved, despite the notches it is necessary to make in the panel (5).
    Type: Grant
    Filed: January 11, 2012
    Date of Patent: June 10, 2014
    Assignee: AIRBUS Operations S.A.S.
    Inventors: Jean Pierre Cabanac, Jerome Colmagro, Jean Marc Durand, Ludovic Fournie, Julien Guillemaut, Francois Loyant
  • CONNECTION OF A FUSELAGE TO AN AIRCRAFT WING
    Publication number: 20120286090
    Abstract: A wing box rib (13), joining an aircraft wing (3) to the wing box and to the rest of the structure, extends advantageously over an adjacent part of the fuselage (2), having in particular an upper line (14) situated above a junction line (15) of the wing upper surface panel (3). The connection is simplified, as is the structure of the aircraft and its manufacture, a lightening is possible, and the transmission of stresses takes place in a more favourable manner.
    Type: Application
    Filed: March 23, 2012
    Publication date: November 15, 2012
    Applicant: Airbus Operations (Societe par Actions Simplifiee)
    Inventors: Dominique GUITTARD, Olivier EVE, Frédéric FORT, Jéròme COLMAGRO, François LOYANT
  • CONNECTOR FOR STIFFENING FRAMES BETWEEN AN AIRCRAFT FUSELAGE AND A WING BOX
    Publication number: 20120193475
    Abstract: The stiffening frames (14) of an aircraft fuselage (2) remain continuous while passing through an upper panel (5) of the wing box and extend over the ribs (3) situated in that box. The overall mechanical strength of the assembly is improved, despite the notches it is necessary to make in the panel (5).
    Type: Application
    Filed: January 11, 2012
    Publication date: August 2, 2012
    Applicant: Airbus Operations (S.A.S.)
    Inventors: Jean Pierre CABANAC, Jérôme Colmagro, Jean Marc Durand, Ludovic Fournie, Julien Guillemaut, François Loyant