Patents by Inventor Julien Sedlak

Julien Sedlak 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: 8152460
    Abstract: A turbomachine compressor, including an air bleed device including a duct having a suction end opening out into an outer casing of the compressor level with a rotor wheel and a stator stage of the compressor is disclosed. A screen sheet of annular shape is mounted radially inside the casing facing a portion of the suction end of the duct so as to make the bleeding of air uniform over 360° around the axis of the compressor.
    Type: Grant
    Filed: December 11, 2008
    Date of Patent: April 10, 2012
    Assignee: SNECMA
    Inventors: Antoine Robert Alain Brunet, Laurent Jablonski, Sebastien Juste, Julien Sedlak
  • Patent number: 8052381
    Abstract: The invention relates to a turbomachine module comprising a device to improve radial clearances, comprising an outer casing (22), an inner casing (21) and at least one shock absorbing ring (5) connecting the casings, the module also comprising an annular cavity (43) on the downstream side of the ring (5), with a passage (42) formed in it through which an airflow (4) is drawn off from the primary flow (Fp). According to the invention, the device to improve radial clearances comprises a thermal inertia control device for the shock absorbing ring mounted on the shock absorbing ring (5), downstream from it, this device comprising at least one coat of thermal insulation (8), and at least partly delimiting the annular cavity (43) on the downstream side of it (43).
    Type: Grant
    Filed: December 12, 2008
    Date of Patent: November 8, 2011
    Assignee: SNECMA
    Inventors: Antoine Robert Alain Brunet, Claude Chomel, Sebastien Juste, Emmanuel Houradou, Dominique Raulin, Frederic Renault, Julien Sedlak
  • Publication number: 20090202341
    Abstract: The invention relates to a turbomachine module comprising a device to improve radial clearances, comprising an outer casing (22), an inner casing (21) and at least one shock absorbing ring (5) connecting the casings, the module also comprising an annular cavity (43) on the downstream side of the ring (5), with a passage (42) formed in it through which an airflow (4) is drawn off from the primary flow (Fp). According to the invention, the device to improve radial clearances comprises a thermal inertia control device for the shock absorbing ring mounted on the shock absorbing ring (5), downstream from it, this device comprising at least one coat of thermal insulation (8), and at least partly delimiting the annular cavity (43) on the downstream side of it (43).
    Type: Application
    Filed: December 12, 2008
    Publication date: August 13, 2009
    Applicant: SNECMA
    Inventors: Antoine Robert, Alain BRUNET, Claude CHOMEL, Sebastien JUSTE, Emmanuel HOURADOU, Dominique RAULIN, Frederic RENAULT, Julien SEDLAK
  • Publication number: 20090155056
    Abstract: A turbomachine compressor, such as a high-pressure compressor, including air bleed means comprising a duct having a suction end opening out into an outer casing of the compressor level with a rotor wheel and a stator stage of the compressor, a screen sheet of annular shape being mounted radially inside the casing facing a portion of the suction end of the duct so as to make the bleeding of air uniform over 360° around the axis of the compressor.
    Type: Application
    Filed: December 11, 2008
    Publication date: June 18, 2009
    Applicant: SNECMA
    Inventors: Antoine Robert Alain BRUNET, Laurent JABLONSKI, Sebastien JUSTE, Julien SEDLAK