Patents by Inventor Stéphane Sylvain BOIS

Stéphane Sylvain BOIS 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: 11879341
    Abstract: A turbine for a turbine engine extending along an axis includes an annular casing and at least one turbine stage having a nozzle and a rotor impeller wheel surrounded by a sealing ring with an abradable element. The impeller wheel and the sealing ring are located downstream of the nozzle, and the sealing ring has an upstream end held on the casing by locking means. The turbine includes elastic sealing means in contact with the locking means as well as with the nozzle or the casing so as to press the locking means against the sealing ring. The locking means includes a radially outer portion with a C-shaped cross-section and a radial portion extending radially inwards from the outer portion. The sealing means include two elastic seals bearing on the radial portion, respectively, on either side of the radial portion.
    Type: Grant
    Filed: April 12, 2021
    Date of Patent: January 23, 2024
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Simon Nicolas Morliere, Nicolas Jean-Marc Marcel Beauquin, Stéphane Sylvain Bois, Sébastien Philippe Edith Bourgeois
  • Publication number: 20230184126
    Abstract: A turbine for a turbine engine extending along an axis includes an annular casing and at least one turbine stage having a nozzle and a rotor impeller wheel surrounded by a sealing ring with an abradable element. The impeller wheel and the sealing ring are located downstream of the nozzle, and the sealing ring has an upstream end held on the casing by locking means. The turbine includes elastic sealing means in contact with the locking means as well as with the nozzle or the casing so as to press the locking means against the sealing ring. The locking means includes a radially outer portion with a C-shaped cross-section and a radial portion extending radially inwards from the outer portion. The sealing means include two elastic seals bearing on the radial portion, respectively on either side of the radial portion.
    Type: Application
    Filed: April 12, 2021
    Publication date: June 15, 2023
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Simon Nicolas MORLIERE, Nicolas Jean-Marc Marcel BEAUQUIN, Stéphane Sylvain BOIS, Sébastien Philippe Edith BOURGEOIS