Patents by Inventor Stéphane Beilliard

Stéphane Beilliard 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).

  • Air intake for aircraft nacelle, and propulsion assembly including such air intake
    Patent number: 8985506
    Abstract: The invention relates to an air intake for an aircraft nacelle that includes a shroud that can be mounted on the fan casing of a turbojet engine. The shroud is sized so as to define a circumferential gap relative to the casing. Punctual linking means between the shroud and the casing are discretely distributed at the periphery of the shroud.
    Type: Grant
    Filed: January 21, 2009
    Date of Patent: March 24, 2015
    Assignee: Aircelle
    Inventors: Guy Bernard Vauchel, Laurent Georges Valleroy, Stéphane Beilliard, Fabien Bravin
  • SEAL FOR A TURBOJET ENGINE PYLON AND NACELLE, AND TURBOJET ENGINE PYLON-NACELLE ASSEMBLY INCORPORATING SUCH A SEAL
    Publication number: 20140318149
    Abstract: A fire-resistant seal for a propulsion assembly which includes a pylon, an O-duct type nacelle of a turbojet engine. The nacelle includes an inner fixed nacelle structure and a combustion gas ejection primary nozzle, and the fire-resistant seal is placed in an annular sector defined by the inner fixed nacelle and the gas ejection primary nozzle. In particular, the fire-resistant seal includes a plurality of baffles, and the plurality of baffles are longitudinally disposed so as not to interfere each other during a longitudinal translational movement of the inner fixed nacelle structure relative to the combustion gas ejection primary nozzle.
    Type: Application
    Filed: July 7, 2014
    Publication date: October 30, 2014
    Inventors: Jean-Bernard Guillon, Alexandre Phi, Stéphane Beilliard
  • AIR INTAKE FOR AIRCRAFT NACELLE, AND PROPULSION ASSEMBLY INCLUDING SUCH AIR INTAKE
    Publication number: 20100320316
    Abstract: The invention relates to an air intake for an aircraft nacelle that comprises a shroud (19) that can be mounted on the fan casing (15) of a turbojet engine (1). The shroud (19) is sized so as to define a circumferential gap (J) relative to the casing (15). Punctual linking means (27, 33) between the shroud (19) and the casing (15) are discretely distributed at the periphery of said shroud (19).
    Type: Application
    Filed: January 21, 2009
    Publication date: December 23, 2010
    Applicant: AIRCELLE
    Inventors: Guy Bernard Vauchel, Laurent Georges Valleroy, Stéphane Beilliard, Fabien Bravin