Patents by Inventor Geoffrey Juan DESMEURE

Geoffrey Juan DESMEURE 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).

  • Patent number: 11244093
    Abstract: A method simulates behavior of a structure by finite element calculation in which a global model represents the structure, a local model represents an area of the structure including geometric details, and an auxiliary model represents the area without the geometric details. The method includes determining by finite element calculation in the global model of a nodal displacement field corresponding to a loading applied to the global model; applying the nodal displacement field to the local and auxiliary models and determining the corresponding forces; calculating a correction when convergence of the solution obtained for the global model is not achieved, and the applying is resumed with a nodal displacement field calculated in the global model after implementing the correction; determining values of internal variables for the different loading increments; and assessing the evolution in the behavior of the structure over time as a function of these values.
    Type: Grant
    Filed: March 16, 2018
    Date of Patent: February 8, 2022
    Assignees: Safran Aircraft Engines, CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (CNRS)
    Inventors: Geoffrey Juan Desmeure, Maxime Guy Roland Blanchard, Olivier Francois Gerard Allix, Pierre Noel Gosselet
  • Patent number: 10984153
    Abstract: A method of determining a maximum acceptable alternating stress at a point of a part subjected to cyclic loading: simulating that the part is subjected to constant loading equal to a threshold value during a level period, and assuming that the part has elasto-viscoplastic behavior; from the results of the simulation, determining a final static stress at the point at the end or after the end of the level period; and for the point under consideration, using a Goodman diagram to determine the maximum acceptable alternating stress, which is determined for a static stress equal to the final static stress; the duration of the level period being equal to the duration of the loading of the testpieces that were used to draw up the Goodman diagram.
    Type: Grant
    Filed: July 19, 2016
    Date of Patent: April 20, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Geoffrey Juan Desmeure, Francois Pierre Michel Comte, Anais Suzanne Amelie Gaubert, Arnaud Cyril Longuet, Marine Laetitia Camille Chevalier, Michael Piers Hansom, Lucie Marie Ida Lanciaux
  • Publication number: 20190286769
    Abstract: A method simulates behavior of a structure by finite element calculation in which a global model represents the structure, a local model represents an area of the structure including geometric details, and an auxiliary model represents the area without the geometric details. The method includes determining by finite element calculation in the global model of a nodal displacement field corresponding to a loading applied to the global model; applying the nodal displacement field to the local and auxiliary models and determining the corresponding forces; calculating a correction when convergence of the solution obtained for the global model is not achieved, and the applying is resumed with a nodal displacement field calculated in the global model after implementing the correction; determining values of internal variables for the different loading increments; and assessing the evolution in the behavior of the structure over time as a function of these values.
    Type: Application
    Filed: March 16, 2018
    Publication date: September 19, 2019
    Applicants: Safran Aircraft Engines, CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (CNRS)
    Inventors: Geoffrey Juan Desmeure, Maxime Guy Roland Blanchard, Olivier Francois Gerard Allix, Pierre Noel Gosselet
  • Publication number: 20180232472
    Abstract: A method of determining a maximum acceptable alternating stress at a point of a part subjected to cyclic loading: simulating that the part is subjected to constant loading equal to a threshold value during a level period, and assuming that the part has elasto-viscoplastic behavior; from the results of the simulation, determining a final static stress at the point at the end or after the end of the level period; and for the point under consideration, using a Goodman diagram to determine the maximum acceptable alternating stress, which is determined for a static stress equal to the final static stress; the duration of the level period being equal to the duration of the loading of the testpieces that were used to draw up the Goodman diagram.
    Type: Application
    Filed: July 19, 2016
    Publication date: August 16, 2018
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Geoffrey Juan DESMEURE, Francois Pierre Michel COMTE, Anais Suzanne Amelie GAUBERT, Arnaud Cyril LONGUET, Marine Laetitia Camille CHEVALIER, Michael Piers HANSOM, Lucie Marie Ida LANCIAUX