Patents by Inventor Clément Charles Jérémy Coiffier

Clément Charles Jérémy Coiffier 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: 11555408
    Abstract: Counter-rotating turbine (C) of a turbomachine (10) extending about an axis (X) and comprising an inner rotor configured to rotate about the axis of rotation (X), and comprising an inner drum on which an inner movable blading (22) is fixed, an outer rotor configured to rotate about the axis of rotation (X) in a direction opposite to the inner rotor, and comprising an outer drum (50) on which an outer movable blading (20) is fixed, the outer movable blading (20) comprising at least one fixing rod (212) extending through an orifice (51) of the outer drum (50), the outer movable blading (20) being fixed to the outer drum (50) via a clamping means (100) fixed to the fixing rod (212) from an outer face of the outer drum (50), a set ring (80) being disposed around the fixing rod (50) in the orifice (51) of the outer drum (50).
    Type: Grant
    Filed: April 3, 2020
    Date of Patent: January 17, 2023
    Assignee: Safran Aircraft Engines
    Inventors: Patrick Jean Laurent Sultana, Clément Charles Jérémy Coiffier, Olivier Renon, Laurent Cédric Zamai
  • Patent number: 11454117
    Abstract: A rotor for a contrarotating turbine comprising a drum and a blading mounted inside, the drum comprising a hook delimiting a housing having an outer wall and an inner wall, the blading comprising a blade and an outer platform provided with spoiler placed inside the housing, wherein the rotor comprises a foil comprising an elastic inner wing and an outer wing, the outer wing being arranged radially between the spoiler and the outer wall, the inner wing having a first support with the inner wall and a second support with the spoiler, the inner wing being arranged in the housing so as to exert a force on the spoiler so as to press the spoiler against the outer wall via the outer wing.
    Type: Grant
    Filed: March 6, 2020
    Date of Patent: September 27, 2022
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Patrick Jean Laurent Sultana, Olivier Renon, Laurent Cédric Zamai, Clément Charles Jérémy Coiffier
  • Publication number: 20220178331
    Abstract: A turbine includes a first rotor and a second rotor that can rotate in opposite directions and are interleaved. The turbine further includes a ring to which abradable material is secured, the ring, unsegmented, extending between the first impellers of the first rotor and the second rotor, over a sector of between 350 and 360°, and, axially between an upstream end and a downstream end of the ring, the ring is held with the second rotor.
    Type: Application
    Filed: March 6, 2020
    Publication date: June 9, 2022
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Patrick SULTANA, Olivier RENON, Laurent Cédric ZAMAI, Clément Charles Jérémy COIFFIER
  • Publication number: 20220162951
    Abstract: Counter-rotating turbine (C) of a turbomachine (10) extending about an axis (X) and comprising an inner rotor configured to rotate about the axis of rotation (X), and comprising an inner drum on which an inner movable blading (22) is fixed, an outer rotor configured to rotate about the axis of rotation (X) in a direction opposite to the inner rotor, and comprising an outer drum (50) on which an outer movable blading (20) is fixed, the outer movable blading (20) comprising at least one fixing rod (212) extending through an orifice (51) of the outer drum (50), the outer movable blading (20) being fixed to the outer drum (50) via a clamping means (100) fixed to the fixing rod (212) from an outer face of the outer drum (50), a set ring (80) being disposed around the fixing rod (50) in the orifice (51) of the outer drum (50).
    Type: Application
    Filed: April 3, 2020
    Publication date: May 26, 2022
    Applicant: Safran Aircraft Engines
    Inventors: Patrick Jean Laurent SULTANA, Clément Charles Jérémy COIFFIER, Olivier RENON, Laurent Cédric ZAMAI
  • Publication number: 20200284150
    Abstract: A rotor for a contrarotating turbine comprising a drum and a blading mounted inside, the drum comprising a hook delimiting a housing having an outer wall and an inner wall, the blading comprising a blade and an outer platform provided with spoiler placed inside the housing, wherein the rotor comprises a foil comprising an elastic inner wing and an outer wing, the outer wing being arranged radially between the spoiler and the outer wall, the inner wing having a first support with the inner wall and a second support with the spoiler, the inner wing being arranged in the housing so as to exert a force on the spoiler so as to press the spoiler against the outer wall via the outer wing.
    Type: Application
    Filed: March 6, 2020
    Publication date: September 10, 2020
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Patrick Jean Laurent Sultana, Olivier Renon, Laurent Cédric Zamai, Clément Charles Jérémy Coiffier