Patents by Inventor Anthony Texier

Anthony Texier 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).

  • Method for manufacturing at least one metal turbine engine part
    Patent number: 10363633
    Abstract: A method of fabricating at least one metal part for a turbine engine, the method including the steps of casting a metal alloy by centrifuging into a permanent metal mold for making a blank; obtaining a cast blank of elongate shape and of section that is circular or polygonal; and machining the blank to make the part.
    Type: Grant
    Filed: October 9, 2013
    Date of Patent: July 30, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Celine Jeanne Marcillaud, Sebastien Digard Brou De Cuissart, Marie Mineur-Panigeon, Anthony Texier
  • Method for producing a turbine engine part, and resulting mould and intermediate blank
    Patent number: 9969035
    Abstract: The invention relates to a method for producing multiple metal turbine engine parts, comprising steps consisting in: a) casting a metal alloy in a mold in order to produce a blank (3); and b) machining the blank in order to produce the parts, characterized in that the blank obtained by casting is a solid polyhedron having first and second sides (30a, 30b) and third and fourth sides (30c, 30d), in which the third and fourth sides extend between the first and second sides, flaring apart from the first side towards the second side, first at a first angle and subsequently at a second larger angle, and said at least one part is machined in the blank.
    Type: Grant
    Filed: December 9, 2014
    Date of Patent: May 15, 2018
    Assignee: SNECMA
    Inventors: Patrick Emilien Paul Emile Huchin, Karine Deschandol, Sébastien Digard Brou De Cuissart, Serge Fargeas, Marc Soisson, Anthony Texier, Valéry Piaton
  • Method for producing turbine engine parts, and resulting blank and mould
    Patent number: 9844843
    Abstract: The invention relates to a method for producing multiple metal turbine engine parts, comprising steps consisting in: a) casting a metal alloy in a mold in order to produce a blank (3); and b) machining the blank in order to produce the parts, characterized in that the blank obtained by casting is a solid polyhedron with two generally trapezoidal opposing sides (30a, 30b), and the parts are machined in the blank.
    Type: Grant
    Filed: December 9, 2014
    Date of Patent: December 19, 2017
    Assignee: SNECMA
    Inventors: Patrick Emilien Paul Emile Huchin, Karine Deschandol, Sébastien Digard Brou De Cuissart, Serge Fargeas, Marc Soisson, Anthony Texier, Valéry Piaton
  • Method for producing turbine engine parts, and resulting mould and blank compromising stacked parts
    Patent number: 9796058
    Abstract: The invention relates to a method for producing multiple metal turbine engine parts, comprising steps consisting in: a) casting a metal alloy in a mould in order to produce a blank (3); and b) machining the blank in order to produce the parts, characterized in that the blank obtained by casting is a solid polyhedron with two generally trapezoidal opposing sides (30a, 30b), and the parts are machined in the blank.
    Type: Grant
    Filed: December 12, 2014
    Date of Patent: October 24, 2017
    Assignee: SNECMA
    Inventors: Patrick Emilien Paul Emile Huchin, Karine Deschandol, Sébastien Digard Brou De Cuissart, Serge Fargeas, Marc Soisson, Anthony Texier, Valéry Piaton
  • METHOD FOR PRODUCING TURBINE ENGINE PARTS, AND RESULTING BLANK AND MOULD
    Publication number: 20160375530
    Abstract: The invention relates to a method for producing multiple metal turbine engine parts, comprising steps consisting in: a) casting a metal alloy in a mould in order to produce a blank (3); and b) machining the blank in order to produce the parts, characterized in that the blank obtained by casting is a solid polyhedron with two generally trapezoidal opposing sides (30a, 30b), and the parts are machined in the blank.
    Type: Application
    Filed: December 9, 2014
    Publication date: December 29, 2016
    Applicant: Snecma
    Inventors: Patrick Emilien Paul Emile Huchin, Sébastien Deschandol, Sébastien Digard Brou De Cuissart, Serge Fargeas, Marc Soisson, Anthony Texier, Valéry Piaton
  • METHOD FOR PRODUCING TURBINE ENGINE PARTS, AND RESULTING MOULD AND BLANK COMPROMISING STACKED PARTS
    Publication number: 20160318137
    Abstract: The invention relates to a method for producing multiple metal turbine engine parts, comprising steps consisting in: a) casting a metal alloy in a mould in order to produce a blank (3); and b) machining the blank in order to produce the parts, characterized in that the blank obtained by casting is a solid polyhedron with two generally trapezoidal opposing sides (30a, 30b), and the parts are machined in the blank.
    Type: Application
    Filed: December 12, 2014
    Publication date: November 3, 2016
    Inventors: Patrick Emilien Paul Emile Huchin, Karine Deschandol, Sébastien Digard Brou De Cuissart, Serge Fargeas, Marc Soisson, Anthony Texier, Valéry Piaton
  • METHOD FOR PRODUCING A TURBINE ENGINE PART, AND RESULTING MOULD AND INTERMEDIATE BLANK
    Publication number: 20160318136
    Abstract: The invention relates to a method for producing multiple metal turbine engine parts, comprising steps consisting in: a) casting a metal alloy in a mould in order to produce a blank (3); and b) machining the blank in order to produce the parts, characterized in that the blank obtained by casting is a solid polyhedron having first and second sides (30a, 30b) and third and fourth sides (30c, 30d), in which the third and fourth sides extend between the first and second sides, flaring apart from the first side towards the second side, first at a first angle and subsequently at a second larger angle, and said at least one part is machined in the blank.
    Type: Application
    Filed: December 9, 2014
    Publication date: November 3, 2016
    Applicant: Snecma
    Inventors: Patrick Emilien Paul Emile Huchin, Karine Deschandol, Sebastien Digard Brou De Cuissart, Serge Fargeas, Marc Soisson, Anthony Texier, Valery Piaton
  • METHOD FOR MANUFACTURING AT LEAST ONE METAL TURBINE ENGINE PART
    Publication number: 20150231746
    Abstract: A method of fabricating at least one metal part for a turbine engine, the method including the steps of casting a metal alloy by centrifuging into a permanent metal mold for making a blank; obtaining a cast blank of elongate shape and of section that is circular or polygonal; and machining the blank to make the part.
    Type: Application
    Filed: October 9, 2013
    Publication date: August 20, 2015
    Applicant: SNECMA
    Inventors: Celine Jeanne Marcillaud, Sebastien Digard Brou De Cuissart, Marie Mineur-Panigeon, Anthony Texier
  • INSTALLATION FOR BREAKING AN EDGE ON A METAL PIECE
    Publication number: 20130153409
    Abstract: An electrode for breaking an edge of a part by electrochemical machining, the electrode including at least one conductive zone configured to be arranged facing an edge of the part that is to be broken. The conductive zone is of a shape that is complementary to the shape of the broken edge to be produced and is arranged between a first portion forming an insulating extra thickness and an insulating second portion for positioning the conductive zone so that it faces the edge to be broken.
    Type: Application
    Filed: September 2, 2011
    Publication date: June 20, 2013
    Applicant: SNECMA
    Inventors: Nicolas Batista, Damien Hebuterne, Anthony Texier