Patents by Inventor Antoine Patrice Marie Desreumaux

Antoine Patrice Marie Desreumaux 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: 10677074
    Abstract: In the method for carrying out work, according to the invention, in order to maintain a metal turbine engine motor, such as a drum, in an operational state: an upstream and/or downstream face (343) of a circumferential groove (34) of the rotor is ground, with said face having recessed marks that the grinding is intended to remove or at least blur, and foils (43) are placed in the groove between the blades of the rotor (24) and the rotor, at least in the area where the face has been ground.
    Type: Grant
    Filed: October 12, 2015
    Date of Patent: June 9, 2020
    Assignee: Safran Aircraft Engines
    Inventors: Antoine Patrice Marie Desreumaux, Patrick Jean-Louis Reghezza
  • Patent number: 10213882
    Abstract: A method for repairing a fan casing in which the inner surface is damaged, includes attaching a reinforcement element to the fan casing, the reinforcement element being attached to the outer surface of the fan casing opposite the damage.
    Type: Grant
    Filed: December 16, 2015
    Date of Patent: February 26, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Antoine Patrice Marie Desreumaux, Patrick Jean-Louis Reghezza, Sébastien Marc Jean-Michel Perez
  • Publication number: 20170348808
    Abstract: A method for repairing a fan casing in which the inner surface is damaged, includes attaching a reinforcement element to the fan casing, the reinforcement element being attached to the outer surface of the fan casing opposite the damage.
    Type: Application
    Filed: December 16, 2015
    Publication date: December 7, 2017
    Inventors: Antoine Patrice Marie DESREUMAUX, Patrick Jean-Louis REGHEZZA, Sébastien Marc Jean-Michel PEREZ
  • Publication number: 20170234148
    Abstract: In the method for carrying out work, according to the invention, in order to maintain a metal turbine engine motor, such as a drum, in an operational state: an upstream and/or downstream face (343) of a circumferential groove (34) of the rotor is ground, with said face having recessed marks that the grinding is intended to remove or at least blur, and foils (43) are placed in the groove between the blades of the rotor (24) and the rotor, at least in the area where the face has been ground.
    Type: Application
    Filed: October 12, 2015
    Publication date: August 17, 2017
    Applicant: Safran Aircraft Engines
    Inventors: Antoine Patrice Marie Desreumaux, Patrick Jean-Louis Reghezza