Patents by Inventor Sylvie Wintenberger

Sylvie Wintenberger 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: 9243562
    Abstract: A rotating inlet cowl for a turbine engine includes a rotation axis. The rotating inlet cowl includes a forward cone defining a forward end of the inlet cowl. The forward end is configured to be eccentric relative to the rotation axis of the inlet cowl. Furthermore, the forward cone is truncated by a truncation surface defining the forward end of the inlet cowl.
    Type: Grant
    Filed: February 12, 2015
    Date of Patent: January 26, 2016
    Assignee: SNECMA
    Inventors: Mickael Delapierre, Herve Gignoux, Gael Loro, Sylvie Wintenberger
  • Publication number: 20160003146
    Abstract: A rotating inlet cowl for a turbine engine includes a rotation axis. The rotating inlet cowl includes a forward cone defining a forward end of the inlet cowl. The forward end is configured to be eccentric relative to the rotation axis of the inlet cowl. Furthermore, the forward cone is truncated by a truncation surface defining the forward end of the inlet cowl.
    Type: Application
    Filed: February 12, 2015
    Publication date: January 7, 2016
    Applicant: SNECMA
    Inventors: Mickael DELAPIERRE, Herve Gignoux, Gael Loro, Sylvie Wintenberger
  • Patent number: 8997451
    Abstract: An engine and pod assembly for an aircraft includes a pod receiving an engine having an air intake. A rotating nose cone extends on the nose cone, as well as a device for limiting the formation of ice. The device includes means for creating a circumferential heterogeneity of ice on the nose cone.
    Type: Grant
    Filed: March 12, 2010
    Date of Patent: April 7, 2015
    Assignee: Sagem Defense Securite
    Inventors: François Dufresne de Virel, Michel Pealat, Patrick Joyez, Bruce Pontoizeau, Jean-François Lacuisse, Sylvie Wintenberger
  • Patent number: 8984855
    Abstract: A rotating inlet cowl for a turbine engine, having a rotation axis and for which the forward end is arranged to be eccentric relative to this rotation axis. Furthermore, a forward cone of the cowl is truncated by a truncation surface defining the forward end of the inlet cowl.
    Type: Grant
    Filed: March 31, 2010
    Date of Patent: March 24, 2015
    Assignee: SNECMA
    Inventors: Mickael Delapierre, Herve Gignoux, Gael Loro, Sylvie Wintenberger
  • Publication number: 20120036827
    Abstract: A rotating inlet cowl for a turbine engine, having a rotation axis and for which the forward end is arranged to be eccentric relative to this rotation axis. Furthermore, a forward cone of the cowl is truncated by a truncation surface defining the forward end of the inlet cowl.
    Type: Application
    Filed: March 29, 2010
    Publication date: February 16, 2012
    Applicant: SNECMA
    Inventors: Mickael Delapierre, Herve Gignoux, Gael Loro, Sylvie Wintenberger
  • Publication number: 20120036826
    Abstract: An engine and pod assembly for an aircraft includes a pod receiving an engine having an air intake. A rotating nose cone extends on the nose cone, as well as a device for limiting the formation of ice. The device includes means for creating a circumferential heterogeneity of ice on the nose cone.
    Type: Application
    Filed: March 12, 2010
    Publication date: February 16, 2012
    Applicant: SAGEM DEFENSE SECURITE
    Inventors: Francois Dufresne De Virel, Michel Pealat, Patrick Joyez, Bruce Pontoizeau, Jean-Francois Lacuisse, Sylvie Wintenberger