Patents by Inventor Gérard Philippe Gauthier

Gérard Philippe Gauthier 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).

  • Publication number: 20080173002
    Abstract: The present invention relates to a method for treating an airflow, laden with oil particles, flowing in a tube (9) communicating with a rolling bearing enclosure of a gas turbine engine, wherein said airflow is made to travel into a coking box (20) associated with a heating means, in which the air is heated to a sufficient temperature to coke the oil particles contained in the airflow. Preferably, the solid residues produced by the coking are collected in the coking box (20).
    Type: Application
    Filed: July 6, 2007
    Publication date: July 24, 2008
    Applicant: SNECMA
    Inventors: Gerard Philippe Gauthier, Jean-Pierre Mourlan
  • Patent number: 6379480
    Abstract: The invention concerns a method for producing parts made of thin, light and rigid metal alloy essentially having the following steps: producing a core having the part shape; producing cavities in the core; producing shells made of metal alloy combined with reinforcing fibers with high modulus of elasticity; densifying the shells; and diffusion welding of the shells on the core by compression at temperature and pressure conditions for isothermal forging of the metal alloy used.
    Type: Grant
    Filed: June 15, 2000
    Date of Patent: April 30, 2002
    Assignee: Societe National d'Etude et de Construction de Moteurs d'Aviation “snecma”
    Inventors: Daniel Georges Girault, Gérard Philippe Gauthier, Ludovic Edmond Camille Molliex
  • Patent number: 6034012
    Abstract: Composite material comprising a CAS+BAS vitroceramic matrix reinforced with SiC fibers and exhibiting a small difference between the thermal expansion coefficients of the matrix and the fibers is obtained by using a matrix having a BaO/(BaO+CaO) molar ratio of between 25% and 55% and predominant phases of triclinic anorthite and monoclinic celsian.
    Type: Grant
    Filed: July 17, 1997
    Date of Patent: March 7, 2000
    Assignees: Societe National D'Etude Et De Construction De Moteurs D'Aviation (SNECMA), Office National D'Etudes Et De Recherches Aerospatiales (ONERA)
    Inventors: Gerard Philippe Gauthier, Yves Emile Marie Ange Laurent, Susanne Obradovic, Olivier Henri Sudre, Patrick Victor Auguste Verdier
  • Patent number: 5733495
    Abstract: A blank consisting of a spirally wound fiber for use in the manufacture of a fiber reinforced article of composite material is made by winding the fiber onto a helical track on the surface of a frusto-conical spindle, covering the wound fiber with a thermoplastic binder which sets to form a frusto-conical shell encasing the fiber, removing the shell from the spindle and placing the shell with its base on a plate, and heating the shell starting from its base so as to soften it and cause it to progressively collapse onto the plate to form a disc comprising a spirally wound fiber. If necessary the collapse of the shell may be assisted by pressing on the shell in a direction towards the plate.
    Type: Grant
    Filed: September 25, 1996
    Date of Patent: March 31, 1998
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
    Inventors: Jean-Claude Robert Berthelemy, Gerard Philippe Gauthier, Ludovic Edmond Camille Molliex, Alain Robert Yves Perroux
  • Patent number: 5642851
    Abstract: An apparatus for producing a circular metal article reinforced by fibres in selected parts of its cross-section is described in which a metal blank of the article is formed and provided with at least one annular groove opening in the axial direction, preforms of reinforcing fibre and filler metal are placed in the groove which is then closed by a metal plug, and the assembly is isothermally forged to produce the article in a single forging step which serves to compress the preforms, weld the assembly together, and shape the article. Such articles may be used for machining high performance rotors for turbojet engines.
    Type: Grant
    Filed: March 20, 1996
    Date of Patent: July 1, 1997
    Assignee: Societe Nationale D'Etude et de Construction de Moteurs D'Aviation "Snecma"
    Inventors: Jean-Claude Berthelemy, Gilles Jean-Michel Bessenay, Gerard Philippe Gauthier, Daniel Georges Girault, Ludovic Edmond Camille Molliex