Patents by Inventor Jean-Luc Bour

Jean-Luc Bour 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: 9707640
    Abstract: A vibration dampening device for the manufacture by rotational friction welding of a turbomachine rotor including a first disc and a second disc each having a hub with an internal surface is provided. The device includes a first clamping device configured to be positioned coaxially to the hub of the first disc and having a pair of radially opposite jaws suited to come into contact with the internal surface of the hub of the first disc.
    Type: Grant
    Filed: December 6, 2013
    Date of Patent: July 18, 2017
    Assignee: SNECMA
    Inventor: Jean-Luc Bour
  • Patent number: 9498841
    Abstract: A belt including notches alternating with bushings on its inside surface is arranged around a disk, so as to encase it and to squeeze its periphery, the bushings penetrating into slot necks designed to house blade roots, so as to apply an elastic tightening force on the teeth and prevent fatigue cracks from forming during inertial friction welding of the disk with other parts of the rotor, these cracks possibly appearing at fillet connections of the teeth to the central part of the disk. The belt is made from elastic polymer with good internal viscosity, and damping properties.
    Type: Grant
    Filed: January 29, 2014
    Date of Patent: November 22, 2016
    Assignee: SNECMA
    Inventor: Jean-Luc Bour
  • Publication number: 20150343556
    Abstract: A belt including notches alternating with bushings on its inside surface is arranged around a disk, so as to encase it and to squeeze its periphery, the bushings penetrating into slot necks designed to house blade roots, so as to apply an elastic tightening force on the teeth and prevent fatigue cracks from forming during inertial friction welding of the disk with other parts of the rotor, these cracks possibly appearing at fillet connections of the teeth to the central part of the disk. The belt is made from elastic polymer with good internal viscosity, and damping properties.
    Type: Application
    Filed: January 29, 2014
    Publication date: December 3, 2015
    Inventor: Jean-Luc BOUR
  • Publication number: 20140158750
    Abstract: The invention relates to a vibration dampening device (1) for the manufacture by rotational friction welding of a turbomachine rotor, said rotor comprising at least one first disc (2a) and a second disc (2b) each comprising a hub (3a, 3b) having an internal surface (4a, 4b), with the device (1) comprising at least one first clamping device (10a) configured to be positioned coaxially to the hub (3a) of the first disc (2a), comprising a pair of radially opposite jaws (11a) suited to come into contact with the internal surface (4a) of said hub (3a) of the first disc (2a).
    Type: Application
    Filed: December 6, 2013
    Publication date: June 12, 2014
    Applicant: SNECMA
    Inventor: Jean-Luc BOUR
  • Patent number: 7021899
    Abstract: A turbomachine blade includes a metal alloy airfoil having a cavity closed off by a cover on a hollowed side, the cover providing aerodynamic continuity of the hollowed side and being bonded via an edge thereof to the rest of the airfoil by a weld bead. The weld bead emerges on the hollowed side and penetrates into the airfoil to a depth P at least equal to the thickness EC of the edge of the cover so as to provide continuity of material between the edge of the cover and the rest of the airfoil over a depth at least equal to the thickness EC of the edge of the cover. A process for manufacturing such a blade is also disclosed.
    Type: Grant
    Filed: March 24, 2004
    Date of Patent: April 4, 2006
    Assignee: Snecma Moteurs
    Inventors: Jean-Pierre Ferte, Jean-Luc Bour, Denis Larrouquere
  • Publication number: 20060039792
    Abstract: A turbomachine blade includes a metal alloy airfoil having a cavity closed off by a cover on a hollowed side, the cover providing aerodynamic continuity of the hollowed side and being bonded via an edge thereof to the rest of the airfoil by a weld bead. The weld bead emerges on the hollowed side and penetrates into the airfoil to a depth P at least equal to the thickness EC of the edge of the cover so as to provide continuity of material between the edge of the cover and the rest of the airfoil over a depth at least equal to the thickness EC of the edge of the cover. A process for manufacturing such a blade is also disclosed.
    Type: Application
    Filed: March 24, 2004
    Publication date: February 23, 2006
    Applicant: SNECMA MOTEURS
    Inventors: Jean-Pierre Ferte, Jean-Luc Bour, Denis Larrouquere
  • Patent number: 6452670
    Abstract: The invention provides a process for checking the bonding of the cellular core of a honeycomb to a skin, said process comprising the steps of: using a light source to illuminate a so-called illuminated zone on the free surface of the honeycomb so as to illuminate the interior of the cells opening out into said illuminated zone, and detecting the emergent light exiting the cells in a so-called observed zone. The minimum distance between said illuminated zone and said observed zone is denoted E and defines a direction D, the distance E being at least equal to the width L1 of the cell mouths measured in the direction D, so as to make it impossible for the illuminated zone and the observed zone to be simultaneously above the mouth of one and the same cell. The invention also provides an instrument for implementing the process.
    Type: Grant
    Filed: October 28, 1999
    Date of Patent: September 17, 2002
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation “Snecma”
    Inventors: Jean-Luc Bour, Gérard Weiss