Patents by Inventor Sylvain Frederic AVAKIAN

Sylvain Frederic AVAKIAN 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).

  • Publication number: 20240035385
    Abstract: Assembly comprising a body extending around a central axis, the body having an outer surface from which a plurality of blades extend, each of said blades having a blade root and a blade tip, defining an inner radial end and an outer radial end of the blade relative to the central axis, said blades having the same blade height measured radially relative to the central axis, characterized in that each of the blades is connected to the body by its blade root via a connection having a nonzero connection height, so that for the plurality of said blades, the connection height of two successive blades is different.
    Type: Application
    Filed: February 1, 2022
    Publication date: February 1, 2024
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Sylvain PHOURATSAMAY, Sylvain Frédéric AVAKIAN, Mickael CAVAREC
  • Patent number: 10975881
    Abstract: A centrifugal impeller having an axis of rotation extending from front to rear, and including a body extending around the axis of rotation, the body having a front portion and a rear portion of larger section than the front portion, the impeller also have blades projecting from a front face of the body, the body presenting a setback in its front face between two consecutive blades, which setback is situated at a circumferential distance from the two blades.
    Type: Grant
    Filed: April 25, 2018
    Date of Patent: April 13, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Sylvain Frederic Avakian, Arnaud Jacques Jean Gascq, Felipe Winston Gomez Moyano, Damien Bernard Emeric Guegan
  • Publication number: 20180313360
    Abstract: A centrifugal impeller (18) having an axis of rotation (X) extending from front to rear, and comprising a body (20) extending around the axis of rotation (X), the body (20) having a front portion and a rear portion of larger section than the front portion, the impeller also have blades (24, 25) projecting from a front face (20a) of the body (20), the body (20) presenting a setback (30) in its front face (20a) between two consecutive blades (24, 25), which setback (30) is situated at a circumferential distance from said two blades (24, 25).
    Type: Application
    Filed: April 25, 2018
    Publication date: November 1, 2018
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Sylvain Frederic AVAKIAN, Arnaud Jacques Jean Gascq, Felipe Winston Gomez Moyano, Damien Bernard Emeric Guegan