Patents by Inventor Guillaume Maurice René PATIN

Guillaume Maurice René PATIN 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).

  • Turbine engine assembly comprising a nose cone and a front shroud
    Patent number: 10794189
    Abstract: The invention relates to an assembly for a turbine engine extending about a longitudinal axis, comprising: a nose cone (20) comprising a conical body (22) extending about the longitudinal axis and a flange (23) comprising a first contact surface (24) forming an extension of an inner surface (25) of the conical body (22); a front shroud (21) comprising an overall annular body (26) extending about the longitudinal axis and a flange (27) comprising a first contact surface (28) forming an extension of an outer surface (29) of the annular body (26), the first contact surface (24) of the nose cone (20) being in contact with the first contact surface (28) of the front shroud (21), the first contact surfaces (24, 28) of the nose cone (20) and the front shroud (21) being tilted in the downstream direction towards the longitudinal axis, so that the flange (23) of the nose cone (20) is secured to the flange (27) of the front shroud (21); and attachment elements (30) configured to clamp the first contact surface (24) of
    Type: Grant
    Filed: July 27, 2017
    Date of Patent: October 6, 2020
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Alexis Thomas Chaboud, Alexandre Michel Henri Hasquenoph, Guillaume Maurice René Patin
  • TURBINE ENGINE ASSEMBLY COMPRISING A NOSE CONE AND A FRONT SHROUD
    Publication number: 20190169990
    Abstract: The invention relates to an assembly for a turbine engine extending about a longitudinal axis, comprising: a nose cone (20) comprising a conical body (22) extending about the longitudinal axis and a flange (23) comprising a first contact surface (24) forming an extension of an inner surface (25) of the conical body (22); a front shroud (21) comprising an overall annular body (26) extending about the longitudinal axis and a flange (27) comprising a first contact surface (28) forming an extension of an outer surface (29) of the annular body (26), the first contact surface (24) of the nose cone (20) being in contact with the first contact surface (28) of the front shroud (21), the first contact surfaces (24, 28) of the nose cone (20) and the front shroud (21) being tilted in the downstream direction towards the longitudinal axis, so that the flange (23) of the nose cone (20) is secured to the flange (27) of the front shroud (21); and attachment elements (30) configured to clamp the first contact surface (24) of
    Type: Application
    Filed: July 27, 2017
    Publication date: June 6, 2019
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Alexis Thomas CHABOUD, Alexandre Michel Henri HASQUENOPH, Guillaume Maurice René PATIN