Patents by Inventor Olivier Harasse

Olivier Harasse 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).

  • Computer-assisted methods of quality control and corresponding quality control systems
    Patent number: 10705513
    Abstract: The disclosure herein relates to a quality control method and system in aeronautical manufacturing. The system comprises a tablet connected to a concession management server, the server being itself linked to an aircraft configuration database, a three-dimensional digital model of the aircraft and a fault database. The element to be inspected is identified using the digital model and the fault is characterized by browsing a predetermined decision tree associated with the element.
    Type: Grant
    Filed: June 17, 2015
    Date of Patent: July 7, 2020
    Assignee: Airbus Operations (S.A.S.)
    Inventor: Olivier Harasse
  • COMPUTER-ASSISTED METHODS OF QUALITY CONTROL AND CORRESPONDING QUALITY CONTROL SYSTEMS
    Publication number: 20150367961
    Abstract: The disclosure herein relates to a quality control method and system in aeronautical manufacturing. The system comprises a tablet connected to a concession management server, the server being itself linked to an aircraft configuration database, a three-dimensional digital model of the aircraft and a fault database. The element to be inspected is identified using the digital model and the fault is characterized by browsing a predetermined decision tree associated with the element.
    Type: Application
    Filed: June 17, 2015
    Publication date: December 24, 2015
    Inventor: Olivier Harasse
  • Reinforced aircraft fuselage panel and method of manufacture
    Patent number: 9034453
    Abstract: A fuselage panel made of composite material having a skin with an opening, at least part of the contour of which is reinforced by an integrated reinforcement made of composite material. The fuselage panel includes at least one liner made of composite material which is attached to and superposed on the reinforced skin portion and participates at least partially in defining the contour of the opening, the panel additionally including consolidating members, each passing at least partially through the liner and at least partially through the reinforced skin portion.
    Type: Grant
    Filed: June 22, 2009
    Date of Patent: May 19, 2015
    Assignee: AIRBUS OPERATIONS S.A.S.
    Inventors: Olivier Harasse, Francois Parreaux-Ey
  • REINFORCED AIRCRAFT FUSELAGE PANEL AND METHOD OF MANUFACTURE
    Publication number: 20110217510
    Abstract: A fuselage panel made of composite material having a skin with an opening, at least part of the contour of which is reinforced by an integrated reinforcement made of composite material. The fuselage panel includes at least one liner made of composite material which is attached to and superposed on the reinforced skin portion and participates at least partially in defining the contour of the opening, the panel additionally including consolidating members, each passing at least partially through the liner and at least partially through the reinforced skin portion.
    Type: Application
    Filed: June 22, 2009
    Publication date: September 8, 2011
    Applicant: AIRBUS OPERATIONS
    Inventors: Olivier Harasse, Francois Parreaux-Ey