Patents by Inventor Julie Vaudour

Julie Vaudour 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: 10807315
    Abstract: A method for manufacturing a composite part with continuous fiber reinforcement and a polymer matrix from a composite preform. On one of the faces of the composite preform, a demarcated layer of thermoplastic polymer is deposited using an additive manufacturing method.
    Type: Grant
    Filed: December 31, 2015
    Date of Patent: October 20, 2020
    Assignee: DAHER AEROSPACE
    Inventors: Stéphanie Portet, Julie Vaudour
  • Patent number: 10773470
    Abstract: A method for the hot stamping of a composite part with continuous fiber reinforcement in a thermoplastic matrix. A blank including a laminated structure of plies consisting in unidirectional tapes of fibers pre-impregnated with thermoplastic polymer is obtained. The blank is heated in the open to a temperature greater than or equal to the melting temperature of the polymer making up the matrix. The blank is then stamped.
    Type: Grant
    Filed: December 24, 2014
    Date of Patent: September 15, 2020
    Assignee: DAHER AEROSPACE
    Inventors: Julie Vaudour, Alexandre Pelard
  • Patent number: 10486376
    Abstract: A method for making a first ply for laying up a fibrous preform on a tool. An attachment zone is made on the laying up surface of the tool. The zone is integral with the laying up surface of the tool. A polymer is deposited by additive manufacturing on the surface of the tool. The polymer deposit passes on the attachment zone. The first ply is laid up by activating the tackiness of the polymer deposited using additive manufacturing, so as to make the deposited fibers adhere to the material deposited by additive manufacturing.
    Type: Grant
    Filed: December 21, 2015
    Date of Patent: November 26, 2019
    Assignee: DAHER AEROSPACE
    Inventors: Stéphanie Portet, Julie Vaudour
  • Publication number: 20180319102
    Abstract: A method for manufacturing a curved part made of a stack of plies of continuous fibers in a thermoplastic polymer matrix. The part having at least one in-plane curved ply in one of the flanges, where the fibers are aligned with the curvature. The fiber placement parameters are determined to obtain welding of the fibers on a pre-deposited ply without diffusion of segments of the polymer's molecular chains through the interface between the fibers and the pre-deposited ply. An in-plane curved flat blank is produced by automated fiber placement using the parameters. The blank comprises at least one ply where fibers are aligned with the curvature and having an overall porosity content lower than 1%. The blank heated to a temperature greater than the melting temperature of the polymer is hot stamped and consolidated to provide the curved composite part with continuous fiber reinforcement having at least two flanges.
    Type: Application
    Filed: July 10, 2018
    Publication date: November 8, 2018
    Inventors: DIDIER KURTZ, JULIE VAUDOUR
  • Patent number: 10016931
    Abstract: A method for forming a thermoplastic composite material with continuous fiber reinforcement by stamping. A flat blank comprising a pre-consolidated stack of plies by automatic fiber placement of fibers referred to as the thermoplastic pre-impregnated fibers is obtained. The flat blank is reheated to a temperature greater than or equal to the melting temperature of the thermoplastic polymer making up the matrix of the thermoplastic pre-impregnated fibers. The reheated flat blank is hot stamped and the part formed between the stamping punch and die is consolidated.
    Type: Grant
    Filed: February 28, 2013
    Date of Patent: July 10, 2018
    Assignee: DAHER AEROSPACE
    Inventors: Didier Kurtz, Julie Vaudour
  • Patent number: 9919504
    Abstract: A device for welding the bottom flange of a stiffener on the side of a skin. The stiffener and the skin are made of a composite comprising a thermoplastic polymer matrix. The device comprises a punch, an anvil and a press to make a clamping between the punch and the anvil. The punch comprises a part forming a pressure table with a cross-section width less than or equal to the width of the stiffener bottom flange and a heating element with width less than the width of the pressure table. The anvil comprises a cooling component and has a cross-section width smaller than the width of the skin. A method for implementing the device.
    Type: Grant
    Filed: February 28, 2013
    Date of Patent: March 20, 2018
    Assignee: DAHER AEROSPACE
    Inventors: Didier Kurtz, Julie Vaudour
  • Publication number: 20170348922
    Abstract: A method for making a first ply for laying up a fibrous preform on a tool. An attachment zone is made on the laying up surface of the tool. The zone is integral with the laying up surface of the tool. A polymer is deposited by additive manufacturing on the surface of the tool. The polymer deposit passes on the attachment zone. The first ply is laid up by activating the tackiness of the polymer deposited using additive manufacturing, so as to make the deposited fibers adhere to the material deposited by additive manufacturing.
    Type: Application
    Filed: December 21, 2015
    Publication date: December 7, 2017
    Inventors: STÉPHANIE PORTET, JULIE VAUDOUR
  • Publication number: 20170326817
    Abstract: A method for manufacturing a composite part with continuous fiber reinforcement and a polymer matrix from a composite preform. On one of the faces of the composite preform, a demarcated layer of thermoplastic polymer is deposited using an additive manufacturing method.
    Type: Application
    Filed: December 31, 2015
    Publication date: November 16, 2017
    Inventors: STÉPHANIE PORTET, JULIE VAUDOUR
  • Patent number: 9561627
    Abstract: A device for compacting and consolidating a stack of fibrous plies pre-impregnated with a thermoplastic polymer, configured to be placed in an oven. The device comprises containment blocks, a flexible compacting plate and a vacuum pump. The containment blocks are supported by a board and demarcate the perimeter of the stack. The containment blocks comprise open grooves that open into the perimeter of the stack. The flexible compacting plate has an area equal to that of the stack but is capable of being inserted inside the perimeter demarcated by the containment blocks. The vacuum pump applies a vacuum to the wrapped volume of the stack comprising a plurality of holes in the board that open outside the perimeter of the stack. A method for implementing the device for manufacturing a thick composite panel having a thermoplastic matrix.
    Type: Grant
    Filed: February 28, 2013
    Date of Patent: February 7, 2017
    Assignee: DAHER AEROSPACE
    Inventors: Didier Kurtz, Julie Vaudour
  • Publication number: 20170001383
    Abstract: A method for the hot stamping of a composite part with continuous fiber reinforcement in a thermoplastic matrix. A blank including a laminated structure of plies consisting in unidirectional tapes of fibers pre-impregnated with thermoplastic polymer is obtained. The blank is heated in the open to a temperature greater than or equal to the melting temperature of the polymer making up the matrix. The blank is then stamped.
    Type: Application
    Filed: December 24, 2014
    Publication date: January 5, 2017
    Inventors: JULIE VAUDOUR, ALEXANDRE PELARD
  • Publication number: 20150114550
    Abstract: A device for welding the bottom flange of a stiffener on the side of a skin. The stiffener and the skin are made of a composite comprising a thermoplastic polymer matrix. The device comprises a punch, an anvil and a press to make a clamping between the punch and the anvil. The punch comprises a part forming a pressure table with a cross-section width less than or equal to the width of the stiffener bottom flange and a heating element with width less than the width of the pressure table. The anvil comprises a cooling component and has a cross-section width smaller than the width of the skin. A method for implementing the device.
    Type: Application
    Filed: February 28, 2013
    Publication date: April 30, 2015
    Inventors: Didier Kurtz, Julie Vaudour
  • Publication number: 20150099091
    Abstract: A method for forming a thermoplastic composite material with continuous fiber reinforcement by stamping. A flat blank comprising a pre-consolidated stack of plies by automatic fiber placement of fibers referred to as the thermoplastic pre-impregnated fibers is obtained. The flat blank is reheated to a temperature greater than or equal to the melting temperature of the thermoplastic polymer making up the matrix of the thermoplastic pre-impregnated fibers. The reheated flat blank is hot stamped and the part formed between the stamping punch and die is consolidated.
    Type: Application
    Filed: February 28, 2013
    Publication date: April 9, 2015
    Inventors: Didier Kurtz, Julie Vaudour
  • Publication number: 20150099105
    Abstract: A device for compacting and consolidating a stack of fibrous plies pre-impregnated with a thermoplastic polymer, configured to be placed in an oven. The device comprises containment blocks, a flexible compacting plate and a vacuum pump. The containment blocks are supported by a board and demarcate the perimeter of the stack. The containment blocks comprise open grooves that open into the perimeter of the stack. The flexible compacting plate has an area equal to that of the stack but is capable of being inserted inside the perimeter demarcated by the containment blocks. The vacuum pump applies a vacuum to the wrapped volume of the stack comprising a plurality of holes in the board that open outside the perimeter of the stack. A method for implementing the device for manufacturing a thick composite panel having a thermoplastic matrix.
    Type: Application
    Filed: February 28, 2013
    Publication date: April 9, 2015
    Inventors: Didler Kurtz, Julie Vaudour