Patents by Inventor Pierre Josso

Pierre Josso 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: 20090017329
    Abstract: The method according to the invention comprises the following operations: a) prepare a substrated formed of the said intermetallic alloy; b) deposit a coating of gold on the surface to be protected of the substrate; and c) subject the substrate thus equipped with the gold coating to annealing in controlled conditions in order to bring about limited diffusion of the gold into the surface to be protected. The invention is applicable in particular to parts of gas turbines, e.g. parts of aircraft engines.
    Type: Application
    Filed: July 8, 2008
    Publication date: January 15, 2009
    Inventors: Marie-Pierre Bacos, Pierre Josso
  • Publication number: 20070281175
    Abstract: The invention relates to a method of brazing a Ti—Al alloy. According to the invention, a layer of nickel (2) is disposed between a part (1) which is made from titanium aluminide and a brazing sheet (3), such as to enable: the aforementioned part (1) to be brazed to another metallic material (4) without the aluminium diffusing from one to the other; and a stable link with good mechanical strength to be produced. The invention can be used for the assembly of aircraft engine parts which are made from titanium aluminide and nickel-based superalloy.
    Type: Application
    Filed: July 15, 2004
    Publication date: December 6, 2007
    Inventors: Carine Hoffmann, Marie-Pierre Bacos, Pierre Josso, Serge Naveos
  • Publication number: 20070108255
    Abstract: Hollow metal spheres are heated in a high vacuum in the presence of an organic substance, at a temperature at least equal to the melting point of a eutectic between carbon and the metallic constituents of the said spheres.
    Type: Application
    Filed: July 7, 2006
    Publication date: May 17, 2007
    Inventors: Jason Nadler, Pierre Josso, Marie-Pierre Bacos, Florin Paun
  • Publication number: 20070071991
    Abstract: In order to protect a monocrystalline superalloy rich in rhenium against corrosion whilst avoiding the formation of progressive secondary reaction zones, a layer (3) formed of tungsten and cobalt is deposited on its surface before aluminisation treatment.
    Type: Application
    Filed: February 1, 2006
    Publication date: March 29, 2007
    Inventors: Marie-Pierre Bacos, Pierre Josso
  • Patent number: 7160582
    Abstract: The invention concerns a method wherein the substrate (5) to be coated is immersed in an autocatalytic chemical deposit bath (4), for example nickel, contained in a stainless steel vessel (1) and wherein can be optionally mixed a suspended MCrAlY alloy, so as to form a metal deposit (nickel) wherein are optionally included powder particles. The invention is characterised in that, to provide a prolonged operation of the bath, it consists in measuring with a voltmeter (8) the difference of potential between the substrate (5) and a reference electrode (6) immersed in the bath (4), and in imposing between the substrate (5) and the vessel (1) an electric current produced by a generator (10), said current being adjusted by a regulator (11) so as to maintain said potential difference at a selected value.
    Type: Grant
    Filed: March 26, 2001
    Date of Patent: January 9, 2007
    Assignee: Office National d'Etudes et de Recherches Aerospatiales
    Inventors: Benoît Girard, Marie-Pierre Bacos, Eric Berger, Pierre Josso
  • Publication number: 20040241833
    Abstract: The invention concerns a method wherein the substrate (5) to be coated is immersed in an autocatalytic chemical deposit bath (4), for example nickel, contained in a stainless steel vessel (1) and wherein can be optionally mixed a suspended MCrAlY alloy, so as to form a metal deposit (nickel) wherein are optionally included powder particles. The invention is characterised in that, to provide a prolonged operation of the bath, it consists in measuring with a voltmeter (8) the difference of potential between the substrate (5) and a reference electrode (6) immersed in the bath (4), and in imposing between the substrate (5) and the vessel (1) an electric current produced by a generator (10), said current being adjusted by a regulator (11) so as to maintain said potential difference at a selected value.
    Type: Application
    Filed: October 22, 2003
    Publication date: December 2, 2004
    Inventors: Benoit Girard, Marie-Pierre Bacos, Eric Berger, Pierre Josso
  • Publication number: 20040194858
    Abstract: This relates to an improvement to the process of aluminization or activated cementation in which a donor cement containing the aluminium is attacked at high temperature and in a neutral or reducing atmosphere by a gaseous ammonium halide to form a gaseous aluminium halide which decomposes on contact with a nickel-based substrate depositing aluminium metal thereon.
    Type: Application
    Filed: March 31, 2004
    Publication date: October 7, 2004
    Inventors: Marie-Pierre Bacos, Pierre Josso, Serge Naveos
  • Patent number: 6695960
    Abstract: The invention concerns a method comprising a step which consists in producing, on a precursor alloy powder containing at least the elements Cr, Al and Y, using a chemical or electrolytic deposition bath, a deposition containing at least a modifying element such as platinum, palladium, ruthenium or rhenium. The modifying element enhances the capacity of the coating to form from phase &bgr;, by exposure to oxygen at high temperature, an adhesive alumina surface barrier. The invention is useful for protecting against corrosion and oxidation at high temperatures aviation turbine blades.
    Type: Grant
    Filed: June 14, 2001
    Date of Patent: February 24, 2004
    Assignee: Onera (Office National d' Etudes et de Recherchers Aerospatiales)
    Inventors: Marie Pierre Bacos, Pierre Josso
  • Patent number: 5843585
    Abstract: A thermal barrier coating for a superalloy part used, in particular, in turbomachines comprises a ceramic coating and a sub-layer interposed between the superalloy substrate and the ceramic coating, the sub-layer being composed of a nickel and/or cobalt aluminide containing at least one platinum-like metal and at least one metal for promoting the formation of a layer of oxide constituted by the alpha-allotropic variety of alumina.
    Type: Grant
    Filed: February 27, 1997
    Date of Patent: December 1, 1998
    Assignees: Societe Nationale D'Etude et de Construction de Moteurs D'Aviation "Snecma", Societe Sochata, Office National d'Etudes et de Recherche Aerospatiales (ONERA)
    Inventors: Serge Alexandre Alperine, Jean-Paul Fournes, Pierre Josso, Jacques Louis Leger, Andre Hubert Louis Malie, Denis Georges Manesse
  • Patent number: 5776620
    Abstract: The sealing composition contains powders composed, by weight, of 70 to 90% of aluminium, 5 to 25% of silicon, 0 to 5% of silica and 0.1 to 5% of moderating metal, which are dispersed in a vehicle comprising an organic binder dissolved in a solvent and a mineral binder.It is applied to the faces to be assembled of a ceramic part and of a refractory alloy or superalloy part and the whole is heated in order to eliminate said vehicle and form between the two parts a layer of mullite syncrystallized with the ceramic.
    Type: Grant
    Filed: January 22, 1996
    Date of Patent: July 7, 1998
    Assignee: Office National D'Etudes et de Recherches Aerospatiales
    Inventors: Pierre Josso, Serge Alperine
  • Patent number: 5110422
    Abstract: A surface layer of a material containing carbon and/or a carbide is produced on the outer surface of a solid carbon-based substrate (1) by selective application of material, said surface layer adhering strongly to the substrate, having a high specific surface area and having open pores (5) of a depth of at least 1 nm, and a metal material having a strong affinity for carbon, comprising at least one metal chosen from cerium, cobalt, chromium, iron, hafnium, iridium, osmium, palladium, platinum, rhodium, ruthenium, lanthanum, manganese, molybdenum, nickel, silicon, tantalum, thorium, titanium, uranium and tungsten, is deposited on said surface layer, substantially filling said pores.The metal deposit (8) may be rectified and polished without peeling off, in order to produce a mirror of low inertia.
    Type: Grant
    Filed: December 12, 1990
    Date of Patent: May 5, 1992
    Assignee: Office National d'Etudes et de Recherches Aerospatiales
    Inventors: Serge Alperine, Pierre Josso
  • Patent number: 5085693
    Abstract: The bath contains an oxalate of the metal or of each of the metals to be deposited and hydrazine as a reducing agent, together with ethylenediamine as a complexing agent and at least one stabilizing agent, said bath being highly basic and having an autocatalytic effect.
    Type: Grant
    Filed: October 10, 1990
    Date of Patent: February 4, 1992
    Assignee: Office National d'Etudes et de Recherches Aerospatiales
    Inventors: Pierre Josso, Serge Alperine, Pierre Steinmetz, Anne Constantini-Friant
  • Patent number: 4962005
    Abstract: A method including aluminization treatment preceded by a palladium predeposition treatment, the palladium being associated with at least one barrier metal selected from nickel, cobalt, and chromium, thereby avoiding hydrogen occlusion.
    Type: Grant
    Filed: October 11, 1989
    Date of Patent: October 9, 1990
    Assignee: Office National D'Etudes et de Recherches Aerospatiales
    Inventors: Serge Alperine, Pierre Josso
  • Patent number: 4486233
    Abstract: A nickel and/or cobalt chemical plating bath comprises: a salt of the metal(s) to be deposited; one or more complexing agents of said metal(s), a reducing agent based on boron or phosphorous; and a stabilizing agent. To avoid including sources of corrosion and/or toxic substances in the plating, the stabilizing agent comprises a water soluble organic compound which possesses a readily accessible electron pair, and which does not include any metal or metalloid from group IIIa (other than boron or aluminum), IVa (other than carbon), Va (other than nitrogen or phosphorous), VIa (other than oxygen), or VIIa (other than fluorine or chlorine).
    Type: Grant
    Filed: July 29, 1983
    Date of Patent: December 4, 1984
    Assignee: Office National d'Etudes et de Recherche Aerospatiales
    Inventors: Pierre Josso, Pierre Lepetit, Pierre Mazars, Marcel J. Massard, deceased