Patents by Inventor Isabelle Marie Monique Valente

Isabelle Marie Monique Valente 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: 10913105
    Abstract: A fabrication method for fabricating a pattern for lost pattern casting, comprising at least one insert (10), providing at least two pattern portions (12, 14), said at least two portions being made of a material that can be eliminated, and assembling said at least two pattern portions together around at least a portion of said at least one insert in sealed manner so as to make said pattern (16).
    Type: Grant
    Filed: April 26, 2016
    Date of Patent: February 9, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Pascal Gomez, Umberto Aprile, Philippe Chabaneix, Dominque Coyez, Chantal Sylvette Langlois, Daniel Quach, Isabelle Marie Monique Valente, Matthieu Jean Luc Vollebregt
  • Publication number: 20180154427
    Abstract: A fabrication method for fabricating a pattern for lost pattern casting, comprising at least one insert (10), providing at least two pattern portions (12, 14), said at least two portions being made of a material that can be eliminated, and assembling said at least two pattern portions together around at least a portion of said at least one insert in sealed manner so as to make said pattern (16).
    Type: Application
    Filed: April 26, 2016
    Publication date: June 7, 2018
    Inventors: Pascal GOMEZ, Aprile UMBERTO, Chabaneix PHILIPPE, Dominque COYEZ, Chantal Sylvette LANGLOIS, Daniel QUACH, Isabelle Marie Monique VALENTE, Matthieu Jean Luc VOLLEBREGT
  • Patent number: 6334755
    Abstract: The invention provides a turbomachine including a device for supplying pressurized gas, the gas being bled from the compressor of the turbomachine via a bleed orifice and cooled in a cooling cavity disposed within the compressor rotor upstream of the bleed orifice. This arrangement has the effect of cooling the bled gas by heat transfer through the outer wall of the compressor rotor to the gas stream which is being compressed by the compressor upstream of the bleed orifice, and has the result of reducing the drop in the performance of the compressor as a result of the gas being bled off.
    Type: Grant
    Filed: February 18, 2000
    Date of Patent: January 1, 2002
    Assignee: Snecma Moteurs
    Inventors: Xavier Gérard André Coudray, Mischaël François Louis Derrien, Marc Roger Marchi, Philippe Christian Pellier, Jean-Claude Christian Taillant, Thierry Henri Marcel Tassin, Christophe Bernard Texier, Isabelle Marie Monique Valente
  • Patent number: 6286582
    Abstract: A process for the manufacture of a thin ceramic core involves casting a band of uniform thickness on a support from a solution of a ceramic material based on silica and zircon in a binder, drying the band, shaping the band in a mold and carrying out preheating and pressing of the band in the mold, baking the component thus obtained in a ceramic preform, and then carrying out an impregnation. The thin core obtained can be assembled together with another thin core and/or on a conventional thick central core, and can be used in precision casting such as in the production of turbine blades.
    Type: Grant
    Filed: November 9, 1999
    Date of Patent: September 11, 2001
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation “SNECMA”
    Inventors: Thierry Jean Emile Chartier, Vincent Louis Christian David, Mischaël François Louis Derrien, Eric Jean Eberschveiller, Franck Edmond Maurice Truelle, Isabelle Marie Monique Valente