Patents by Inventor Mathieu ZARONE

Mathieu ZARONE 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).

  • Engine pylon rear secondary structure
    Patent number: 12371176
    Abstract: An engine pylon rear secondary structure for an aircraft comprising an engine pylon (30) suspending an engine (20) to a wing (10), the engine pylon rear secondary structure comprising: a front attachment interface (310); an aft attachment interface (320); a composite beam (301) connecting the front attachment interface (310) and the aft attachment interface (320); the composite beam (301) comprising a first section (501) and a second section (502) integral with the first section; frames (330) configured for supporting fairing panels (340) and being attached to the first section (501) of the composite beam; and fairing panels (340) attached to outer faces of the frames; wherein the composite beam is of a U-shaped cross-section, the frames (330) comprising three brackets (431, 432, 433) configured to be attached to the composite beam on three external faces of the U-shaped cross-section.
    Type: Grant
    Filed: July 16, 2024
    Date of Patent: July 29, 2025
    Assignee: DAHER AEROSPACE
    Inventors: Cyril Raguet, Valérie Sorez, Mathieu Zarone
  • Engine pylon rear secondary structure
    Publication number: 20250026480
    Abstract: An engine pylon rear secondary structure for an aircraft comprising an engine pylon (30) suspending an engine (20) to a wing (10), the engine pylon rear secondary structure comprising: a front attachment interface (310); an aft attachment interface (320); a composite beam (301) connecting the front attachment interface (310) and the aft attachment interface (320); the composite beam (301) comprising a first section (501) and a second section (502) integral with the first section; frames (330) configured for supporting fairing panels (340) and being attached to the first section (501) of the composite beam; and fairing panels (340) attached to outer faces of the frames; wherein the composite beam is of a U-shaped cross-section, the frames (330) comprising three brackets (431, 432, 433) configured to be attached to the composite beam on three external faces of the U-shaped cross-section.
    Type: Application
    Filed: July 16, 2024
    Publication date: January 23, 2025
    Applicant: DAHER AEROSPACE
    Inventors: Cyril RAGUET, Valérie SOREZ, Mathieu ZARONE