Patents by Inventor Lola AULIAC

Lola AULIAC 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: 20220127965
    Abstract: The invention relates to a fan rotor for a turbomachine, comprising including a fan disk, fan blades with a leading edge and a trailing edge, platforms inserted between the blades and fixed to the periphery of the disk, each including an aerodynamic surface extending from the leading edges to the trailing edges of the blades. The aerodynamic surface includes an upstream longitudinal portion on the side of the leading edges and a downstream longitudinal portion on the side of the trailing edges, the upstream longitudinal portion being supported by a first member of the platform fixed to the disk in a pivotable manner, and the downstream longitudinal portion being independent of the upstream longitudinal portion and supported by a second member of the platform which is independent of the first member and fixed to the disk in a pivotable manner.
    Type: Application
    Filed: March 19, 2020
    Publication date: April 28, 2022
    Inventors: Jeremy Philippe Pierre EDYNAK, Jeremy GUIVARC'H, Lola AULIAC, Thibaut Dominique Augustin GIRARD, Pierre Jean FAIVRE D'ARCIER
  • Patent number: 11078918
    Abstract: Seal (10) for an inter-blade platform intended to extend circumferentially about an axis and to be mounted between two axial ends of the inter-blade platform, including a first part (10a) in contact with a first blade adjacent to a first circumferential end of the platform, and a second part (10b) in contact with a second blade adjacent to a second circumferential end of the platform, the first part (10a) and the second part (10b) of the seal (10) being fixed to each other such that a displacement in the circumferential direction of one of the two parts (10a, 10b) of the seal (10) causes a displacement of the other part (10a, 10b) of the seal (10) in the same direction, when the two parts (10a, 10b) of the seal (10) are fixed to each other.
    Type: Grant
    Filed: January 3, 2020
    Date of Patent: August 3, 2021
    Assignees: SAFRAN AIRCRAFT ENGINES, SAFRAN
    Inventors: Thibaut Dominique Augustin Girard, Lola Auliac, Jérémy Guivarc'h, Jérémy Philippe Pierre Edynak, Pierre Jean Faivre D'Arcier
  • Publication number: 20200217217
    Abstract: Seal (10) for an inter-blade platform intended to extend circumferentially about an axis and to be mounted between two axial ends of the inter-blade platform, including a first part (10a) in contact with a first blade adjacent to a first circumferential end of the platform, and a second part (10b) in contact with a second blade adjacent to a second circumferential end of the platform, the first part (10a) and the second part (10b) of the seal (10) being fixed to each other such that a displacement in the circumferential direction of one of the two parts (10a, 10b) of the seal (10) causes a displacement of the other part (10a, 10b) of the seal (10) in the same direction, when the two parts (10a, 10b) of the seal (10) are fixed to each other.
    Type: Application
    Filed: January 3, 2020
    Publication date: July 9, 2020
    Applicants: SAFRAN AIRCRAFT ENGINES, SAFRAN
    Inventors: Thibaut Dominique Augustin GIRARD, Lola AULIAC, Jeremy GUIVARC'H, Jeremy Philippe Pierre EDYNAK, Pierre Jean FAIVRE D'ARCIER