Patents by Inventor Olivier Chantoiseau

Olivier Chantoiseau 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: 10337527
    Abstract: The invention relates to a turbomachine blade comprising a vane. The vane comprises a leading edge, a trailing edge, a pressure face and a suction face spaced apart from each other and connecting the leading edge to the trailing edge. The vane further comprises at least one internal cavity between the pressure face and the suction face, wherein air is intended to flow. The vane comprises intersecting transverse partitions, downstream of the cavity, so that air can flow from the cavity in the direction of the trailing edge between the intersecting partitions.
    Type: Grant
    Filed: November 23, 2015
    Date of Patent: July 2, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Stéphane Mahias, Olivier Chantoiseau, Laurent Gilles Dezouche
  • Patent number: 9707718
    Abstract: A method provides a device having a feeder vessel, a building vessel with a bottom and a fabrication plate that is movable in vertical translation, a transfer system suitable for depositing powder from the feeder vessel to the building vessel as a powder layer of constant thickness, and a high energy beam optical system suitable for scanning the surface of the deposited powder layer. A powder is placed in the feeder vessel. A first series of powder layers is deposited on the fabrication plate. The particles of powder are melted or sintered to form a plurality of columns of material that are separated from one another by particles of powder. A second series of layers of powder is deposited on the first series of layers of powder particles to form a single-piece element. A thermal insulation platform is formed between the fabrication plate and said single-piece element.
    Type: Grant
    Filed: June 3, 2013
    Date of Patent: July 18, 2017
    Assignee: SNECMA
    Inventors: Thomas Vilaro, Olivier Chantoiseau, Sebastien Rix
  • Publication number: 20160153467
    Abstract: The invention relates to a turbomachine blade comprising a vane. The vane comprises a leading edge, a trailing edge, a pressure face and a suction face spaced apart from each other and connecting the leading edge to the trailing edge. The vane further comprises at least one internal cavity between the pressure face and the suction face, wherein air is intended to flow. The vane comprises intersecting transverse partitions, downstream of the cavity, so that air can flow from the cavity in the direction of the trailing edge between the intersecting partitions.
    Type: Application
    Filed: November 23, 2015
    Publication date: June 2, 2016
    Inventors: Stéphane Mahias, Olivier Chantoiseau, Laurent Gilles Dezouche
  • Patent number: 8684069
    Abstract: A method of fabricating a metal part by selectively melting a powder, the method including: building up layer by layer on a plate and simultaneously with the part, at least one holder and support element for the part, the element being spaced apart and distinct from the part and being separated therefrom by a gap filled with non-melted powder; after the part has been made completely, removing at least some of the powder remaining in the gap between the part and the element, for example by suction, blowing, or vibration; and separating the part from the plate.
    Type: Grant
    Filed: July 1, 2011
    Date of Patent: April 1, 2014
    Assignee: SNECMA
    Inventors: Jean-Baptiste Mottin, Beryl Cassandre Anne Mereaux, Sophie Martine Jobez, Olivier Chantoiseau, Bruno Le Razer
  • Publication number: 20130341838
    Abstract: A method provides a device having a feeder vessel, a building vessel with a bottom and a fabrication plate that is movable in vertical translation, a transfer system suitable for depositing powder from the feeder vessel to the building vessel as a powder layer of constant thickness, and a high energy beam optical system suitable for scanning the surface of the deposited powder layer. A powder is placed in the feeder vessel. A first series of powder layers is deposited on the fabrication plate. The particles of powder are melted or sintered to form a plurality of columns of material that are separated from one another by particles of powder. A second series of layers of powder is deposited on the first series of layers of powder particles to form a single-piece element. A thermal insulation platform is formed between the fabrication plate and said single-piece element.
    Type: Application
    Filed: June 3, 2013
    Publication date: December 26, 2013
    Inventors: Thomas VILARO, Olivier CHANTOISEAU, Sebastien RIX
  • Publication number: 20130112366
    Abstract: A method of fabricating a metal part by selectively melting a powder, the method including: building up layer by layer on a plate and simultaneously with the part, at least one holder and support element for the part, the element being spaced apart and distinct from the part and being separated therefrom by a gap filled with non-melted powder; after the part has been made completely, removing at least some of the powder remaining in the gap between the part and the element, for example by suction, blowing, or vibration; and separating the part from the plate.
    Type: Application
    Filed: July 1, 2011
    Publication date: May 9, 2013
    Applicant: SNECMA
    Inventors: Jean-Baptiste Mottin, Beryl Cassandre, Anne Mereaux, Sophie Martine Jobez, Olivier Chantoiseau, Bruno Le Razer