Patents by Inventor Yves C. L. A. Honnorat

Yves C. L. A. Honnorat 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: 5549809
    Abstract: The invention is directed to a method for hardening a metallic part by shot blasting. In prior art hardening processes, debris from the projectiles is frequently encrusted on the surface of the part and forms indents whose bottom is often sharp and which may constitute a starting point for rupture caused by metal fatigue. The inventive process allows hardening without damaging the surface of the part. Prior to shot blasting, a metallic protection film which may, for example, be made of nickel or a nickel-base alloy, is electrolytically deposited on the part. The protection film is thick enough to adhere to the metallic part throughout the shot blasting step but thin enough to allow the shot blasting to work harden the part and to impart a residual compressive stress thereto. After the shot blasting is completed, the protection film is removed.
    Type: Grant
    Filed: August 11, 1994
    Date of Patent: August 27, 1996
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "Snecma"
    Inventors: Eric L. P. Barreau, Yves C. L. A. Honnorat, Robert L. Martinou, Catherine M. H. Richin
  • Patent number: 5419868
    Abstract: A method of manufacturing a part made of a composite material having a metallic matrix, for example of titanium or a titanium based alloy, comprises depositing the matrix material on a continuous length of reinforcing fiber, for example of the SiC type, to produce a coating of a predetermined thickness, winding the thus coated fiber onto a former of suitable shape until a desired thickness is obtained, and then heating and isostatically compacting the wound coated fiber to produce the required part.
    Type: Grant
    Filed: December 4, 1992
    Date of Patent: May 30, 1995
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "SNECMA"
    Inventor: Yves C. L. A. Honnorat
  • Patent number: 5079100
    Abstract: Engine components of steel or superalloy subject to wear from alternating friction at medium temperatures in the region of 700.degree. C. are provided with a protective wear-resistant coating bya) electrophoretic deposition of a metal-ceramic structure comprising a mixture of from 85% to 50% of metallic powder and from 15% to 50% of ceramic powder, the metallic powder being a cobalt-based superalloy of type KC 25 NW or of M Cr Al Y wherein M represents at least one metal chosen from the group consisting of Ni, Co and Fe with the possible addition of Ta, and the ceramic powder being an oxide such as Al.sub.2 O.sub.3 or Cr.sub.2 O.sub.3, a carbide such as SiC or Cr.sub.3 C.sub.2, a nitride such as BN or TiN, or a boride such as TiB.sub.2 ;b) electrolytic pre-nickeling said deposit in an electrolysis bath at a pH between 6 and 8, andc) electrolytic nickeling said pre-nickeled deposit in an acid bath of sulphamate type.
    Type: Grant
    Filed: November 9, 1989
    Date of Patent: January 7, 1992
    Assignee: Societe Nationale d'Etude et de Construction de Motors d'Aviation
    Inventors: Martine Descamp, Yves C. L. A. Honnorat, Michel M. Ruimi