Patents by Inventor Thibaud Louis ZAIA

Thibaud Louis ZAIA 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: 20240151151
    Abstract: A turbine for a turbomachine of longitudinal axis including an alternating arrangement of annular rows of movable blades and of fixed blades and a radially inner annular cavity formed radially inside the movable and fixed blades, and a supply circuit for supplying cooling air to the inner annular cavity, the downstream end of the supply circuit comprising an inner annular row of orifices and an outer annular row of orifices opening into the radially inner annular cavity. The turbine may also include means for controlling the flow rate of supply air to the orifices of the inner and outer annular rows of orifices.
    Type: Application
    Filed: February 23, 2022
    Publication date: May 9, 2024
    Inventors: Bertrand Guillaume, Robin PELLATON, Thibaud Louis ZAIA
  • Patent number: 11879347
    Abstract: A turbomachine turbine casing that extend around an axis and includes an annular wall and a cooling device. The annular wall is provided with a casing hook which extends in radial protrusion from an inside of the annular wall. The casing hook allows a mounting, on the turbomachine turbine casing, of ring segments disposed circumferentially end to end around the axis. The cooling device includes a collector duct intended to convey cooling air, the collector duct extending circumferentially around the annular wall. The collector duct has a cooling air inlet and a cooling air outlet. The collector duct and the annular wall have a common portion, which delimits the collector duct and from which the corresponding casing hook extends.
    Type: Grant
    Filed: April 13, 2021
    Date of Patent: January 23, 2024
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Benoit Guillaume Silet, Stéphane Pierre Guillaume Blanchard, Fabien Stéphane Garnier, Thibaud Louis Zaia
  • Publication number: 20230160319
    Abstract: A turbomachine turbine casing that extend around an axis and includes an annular wall and a cooling device. The annular wall is provided with a casing hook which extends in radial protrusion from an inside of the annular wall. The casing hook allows a mounting, on the turbomachine turbine casing, of ring segments disposed circumferentially end to end around the axis. The cooling device includes a collector duct intended to convey cooling air, the collector duct extending circumferentially around the annular wall. The collector duct has a cooling air inlet and a cooling air outlet. The collector duct and the annular wall have a common portion, which delimits the collector duct and from which the corresponding casing hook extends.
    Type: Application
    Filed: April 13, 2021
    Publication date: May 25, 2023
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Benoit Guillaume SILET, Stéphane Pierre Fuillaume BLANCHARD, Fabien Stéphane GARNIER, Thibaud Louis ZAIA