Patents by Inventor Liliana Gomes Pereira

Liliana Gomes Pereira 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: 11686205
    Abstract: An angular sector of a fixed blade ring of a turbomachine, in particular a stator or a guide vane assembly, includes, relative to the axis of said fixed blade ring, a radially outer platform, a radially inner platform, at least two blades extending between said platforms, and at least one block of abradable honeycomb material extending on the inside of the inner platform between transverse ends of the sector. The block of abradable material includes at least one transverse end wall shaped according to a toothed profile having at least one radially oriented tooth extending across an entire radial thickness of said block.
    Type: Grant
    Filed: May 22, 2019
    Date of Patent: June 27, 2023
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Thomas Nolwenn Emmanuel Delahaye, Kamel Benderradji, Alain Marc Lucien Bromann, Liliana Gomes Pereira, Delphine Hermance Maxime Parent
  • Patent number: 11371352
    Abstract: A holding device is used with a centripetal air sampling member of a rotor assembly that includes and downstream rotor discs and a centripetal air sampling member. The holding device has an annular support element with a housing configured to receive the air sampling member in a radial orientation, a first lateral extension, and a second lateral extension rigidly attached to the downstream rotor disc, extending substantially following the longitudinal axis and radially arranged externally with respect to the first extension. The holding device also includes a wedging ring axially arranged between a portion of the downstream rotor disc and the support element, the wedging ring being configured to simultaneously urge, under the action of a centrifugal force, the first extension in radial abutment against the second extension and the support element in radial abutment against a portion of the upstream rotor disc.
    Type: Grant
    Filed: November 13, 2018
    Date of Patent: June 28, 2022
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Thomas Nolwenn Emmanuel Delahaye, Alain Marc Lucien Bromann, Liliana Gomes Pereira, Delphine Hermance Maxime Parent, Kamel Benderradji
  • Publication number: 20210207488
    Abstract: An angular sector of a fixed blade ring of a turbomachine, in particular a stator or a guide vane assembly, includes, relative to the axis of said fixed blade ring, a radially outer platform, a radially inner platform, at least two blades extending between said platforms, and at least one block of abradable honeycomb material extending on the inside of the inner platform between transverse ends of the sector. The block of abradable material includes at least one transverse end wall shaped according to a toothed profile having at least one radially oriented tooth extending across an entire radial thickness of said block.
    Type: Application
    Filed: May 22, 2019
    Publication date: July 8, 2021
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Thomas Nolwenn Emmanuel Delahaye, Kamel Benderradji, Alain Marc Lucien Bromann, Liliana Gomes Pereira, Delphine Hermance Maxime Parent
  • Publication number: 20200263549
    Abstract: A holding device is disclosed for a centripetal air sampling member of a rotor assembly that includes and downstream rotor discs and a centripetal air sampling member. The holding device has an annular support element with a housing configured to receive the air sampling member in a radial orientation, a first lateral extension, and a second lateral extension rigidly attached to the downstream rotor disc, extending substantially following the longitudinal axis and radially arranged externally with respect to the first extension. The holding device also includes a wedging ring axially arranged between a portion of the downstream rotor disc and the support element, the wedging ring being configured to simultaneously urge, under the action of a centrifugal force, the first extension in radial abutment against the second extension and the support element in radial abutment against a portion of the upstream rotor disc.
    Type: Application
    Filed: November 13, 2018
    Publication date: August 20, 2020
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Thomas Nolwenn Emmanuel Delahaye, Alain Marc Lucien Bromann, Liliana Gomes Pereira, Delphine Hermance Maxime Parent, Kamel Benderradji