Patents by Inventor Olivier Eve

Olivier Eve 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).

  • Aircraft floor of optimized compactness and housing utility members
    Patent number: 8899521
    Abstract: An aircraft floor portion includes crossmembers. Each crossmember comprises a top partial crossmember and a bottom crossmember, with at least one gap being left between the top partial crossmember and the bottom partial crossmember of each crossmember.
    Type: Grant
    Filed: June 25, 2010
    Date of Patent: December 2, 2014
    Assignee: Airbus Operations
    Inventors: Romain Delahaye, Guillaume Gallant, Olivier Eve
  • Connection of a fuselage to an aircraft wing
    Patent number: 8770518
    Abstract: A wing box rib, joining an aircraft wing to the wing box and to the rest of the structure, extends advantageously over an adjacent part of the fuselage, having in particular an upper line situated above a junction line of the wing upper surface panel. 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 favorable manner.
    Type: Grant
    Filed: March 23, 2012
    Date of Patent: July 8, 2014
    Assignee: Airbus Operations S.A.S.
    Inventors: Dominique Guittard, Olivier Eve, Frédéric Fort, Jérôme Colmagro, François 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
  • Aircraft floor of optimized compactness
    Publication number: 20110001008
    Abstract: An aircraft floor portion includes crossmembers. Each crossmember comprises a top partial crossmember and a bottom crossmember, with at least one gap being left between the top partial crossmember and the bottom partial crossmember of each crossmember.
    Type: Application
    Filed: June 25, 2010
    Publication date: January 6, 2011
    Applicant: AIRBUS OPERATIONS
    Inventors: Romain Delahaye, Guillaume Gallant, Olivier Eve
  • PRIMARY ENGINE STRUT STRUCTURE OF AN AIRCRAFT
    Publication number: 20090294579
    Abstract: The disclosed embodiments relate to a primary engine strut structure of an aircraft characterized in that it includes single-piece composite panels while replacing the metallic spars and metal panels, the composite panels having a lay-up of fibers oriented along crosswise directions whereby integrating, in the width of the skin of the panles, a lattice structure that replaces longitudinal and transversal stiffeners of the spars and metal panels.
    Type: Application
    Filed: July 13, 2006
    Publication date: December 3, 2009
    Applicant: AIRBUS FRANCE
    Inventors: Olivier Eve, Jean-Pierre Cabanac