Patents by Inventor Nicolas GARCIA ROSA

Nicolas GARCIA ROSA 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).

  • Assembly for a turbomachine
    Patent number: 11913378
    Abstract: The invention relates to an assembly for a turbomachine, comprising: —a nacelle comprising an inlet lip which defines an air inlet, and—a device for modifying the geometry of the air inlet, comprising: —a first spout, and—a second spout, the first spout and the second spout being translatably movable in relation the nacelle between: —a first configuration, in which the first spout forms the inlet lip and the second spout extends inside the nacelle, and—a second configuration, in which the first spout extends away from the inlet lip, and the second spout forms the inlet lip so as to define an air flow channel between a downstream surface of the first spout and an upstream surface of the second spout.
    Type: Grant
    Filed: October 15, 2020
    Date of Patent: February 27, 2024
    Assignees: INSTITUT SUPERIEUR DE L AERONAUTIQUE ET DE L ESPACE, SAFRAN AIRCRAFT ENGINES
    Inventors: Nicolas Jérôme Jean Tantot, Xavier Carbonneau, Philippe Gérard Chanez, Nicolas Garcia Rosa, Alejandro Martin Pleguezuelo, Nicolas Joseph Sirvin
  • ASSEMBLY FOR A TURBOMACHINE
    Publication number: 20230349323
    Abstract: The invention relates to an assembly for a turbomachine, comprising: —a nacelle comprising an inlet lip which defines an air inlet, and—a device for modifying the geometry of the air inlet, comprising: —a first spout, and—a second spout, the first spout and the second spout being translatably movable in relation the nacelle between: —a first configuration, in which the first spout forms the inlet lip and the second spout extends inside the nacelle, and—a second configuration, in which the first spout extends away from the inlet lip, and the second spout forms the inlet lip so as to define an air flow channel between a downstream surface of the first spout and an upstream surface of the second spout.
    Type: Application
    Filed: October 15, 2020
    Publication date: November 2, 2023
    Applicants: INSTITUT SUPERIEUR DE L AERONAUTIQUE ET DE L ESPACE, SAFRAN AIRCRAFT ENGINES
    Inventors: Nicolas Jérôme Jean TANTOT, Xavier CARBONNEAU, Philippe Gérard CHANEZ, Nicolas GARCIA ROSA, Alejandro MARTIN PLEGUEZUELO, Nicolas Joseph SIRVIN