Patents by Inventor Dominique Bailly

Dominique Bailly 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: 11916492
    Abstract: The present description concerns a device for delivering a voltage from an AC voltage, comprising a capacitive element (120), two switches (132H, 132L) in a half-bridge between terminals of the capacitive element (120); terminals (102, 104) of application of the AC voltage; a transformer (160), comprising a first winding (162) coupling to a junction node (136) between the switches (132H, 132L) one of the terminals (104) of application of the AC voltage; and one or a plurality of circuits (170, 180, 140), configured to switch the switches (132H, 132L) and receive an AC current (I164) flowing through a second winding (164) of the transformer (160) and regulate the voltage delivered by the device by acting on a frequency of said AC current and/or on a phase shift of said AC current with respect to its reception.
    Type: Grant
    Filed: June 16, 2020
    Date of Patent: February 27, 2024
    Assignee: Commissariat à l'Energie Atomique et aux Energies Alternatives
    Inventors: Alain Bailly, Dominique Bergogne, Thierry Bouchet
  • Patent number: 10350830
    Abstract: A method for assembling a box structure includes elementary parts assembled along an understructure of stiffeners and skins. The understructure and skins are made of composite material with a polymer matrix. The method includes sizing the box structure for the loads to which it is subjected and for a glued assembly. A map of the loads on the structure is obtained and a first load limit is defined depending on the probability of the structure being damaged. The understructure and the skins are assembled by gluing them. An additional layer is applied that covers the assembled elementary parts to areas of the assembled box structure where the first load limit is reached.
    Type: Grant
    Filed: June 10, 2015
    Date of Patent: July 16, 2019
    Assignee: DAHER AEROSPACE
    Inventors: Dominique Bailly, Cédric Blanchegorge, Elric Minard
  • Publication number: 20170232662
    Abstract: A method for assembling a box structure includes elementary parts assembled along an understructure of stiffeners and skins. The understructure and skins are made of composite material with a polymer matrix. The method includes sizing the box structure for the loads to which it is subjected and for a glued assembly. A map of the loads on the structure is obtained and a first load limit is defined depending on the probability of the structure being damaged. The understructure and the skins are assembled by gluing them. An additional layer is applied that covers the assembled elementary parts to areas of the assembled box structure where the first load limit is reached.
    Type: Application
    Filed: June 10, 2015
    Publication date: August 17, 2017
    Inventors: DOMINIQUE BAILLY, CÉDRIC BLANCHEGEORGE, ELRIC MINARD
  • Patent number: 9731487
    Abstract: A method for assembling a skin and a flange of a stiffener. The periphery of the contact between the skin and the flange of the stiffener is sealed by applying a bead of adhesive on the flange of the stiffener in contact with the skin. A first and second orifices are made in the skin. The orifices open at the interface between the skin and the flange of the stiffener. The adhesive is injected through the first orifice at the interface between the skin and the flange of the stiffener while keeping the skin in contact with the stiffener until the interface between the skin and the stiffener is completely filled with the adhesive.
    Type: Grant
    Filed: September 17, 2012
    Date of Patent: August 15, 2017
    Assignee: DAHER AEROSPACE
    Inventors: Dominique Bailly, Mathieu Hottin
  • Patent number: 9475586
    Abstract: A method for making a structural element comprising a panel in composite material with fiber reinforcement in an organic matrix obtained by laying up and curing. The panel comprises a side likely to be exposed to contact with hydrocarbons. The required layer structure is obtained by laying up the plies of fibers pre-impregnated with resin having a curing temperature T1. A ply made of a thin film of polymer that can withstand hydrocarbons and the curing temperature T1, referred to as the protective film, is applied on the side exposed to hydrocarbons. The entire layered structure is cured under pressure at the temperature T1.
    Type: Grant
    Filed: October 29, 2012
    Date of Patent: October 25, 2016
    Assignee: Daher Aerospace
    Inventors: Mathieu Hottin, Dominique Bailly
  • Publication number: 20140346179
    Abstract: A method for assembling a skin and a flange of a stiffener. The periphery of the contact between the skin and the flange of the stiffener is sealed by applying a bead of adhesive on the flange of the stiffener in contact with the skin. A first and second orifices are made in the skin. The orifices open at the interface between the skin and the flange of the stiffener. The adhesive is injected through the first orifice at the interface between the skin and the flange of the stiffener while keeping the skin in contact with the stiffener until the interface between the skin and the stiffener is completely filled with the adhesive.
    Type: Application
    Filed: September 17, 2012
    Publication date: November 27, 2014
    Inventors: Dominique Bailly, Mathieu Hottin
  • Publication number: 20140239122
    Abstract: A method for making a structural element comprising a panel in composite material with fiber reinforcement in an organic matrix obtained by laying up and curing. The panel comprises a side likely to be exposed to contact with hydrocarbons. The required layer structure is obtained by laying up the plies of fibers pre-impregnated with resin having a curing temperature T1. A ply made of a thin film of polymer that can withstand hydrocarbons and the curing temperature T1, referred to as the protective film, is applied on the side exposed to hydrocarbons. The entire layered structure is cured under pressure at the temperature T1.
    Type: Application
    Filed: October 29, 2012
    Publication date: August 28, 2014
    Applicant: Daher Aerospace
    Inventors: Mathieu Hottin, Dominique Bailly
  • Publication number: 20080116687
    Abstract: A device adapted to join two sleeves (1, 3) in a sealed manner by at least one of their respective ends provided each with fastening means (4, 7) adapted to cooperate with joining means (10), characterized in that the said joining means (10) are comprised of and/or include at least one adjusting member (11) allowing at least one degree of freedom to a sleeve (1, 3) in relation to the other in the joined position. Specifically, the said joining means (10) are formed by at least one mobile connecting member (12) and at least one adjusting member (11) adapted to cooperate with the said fastening means (4, 7) provided at least at one end of a sleeve (1,3). The said at least one adjusting member (11) is at least a means for radial and/or axial and/or angular adjustment.
    Type: Application
    Filed: November 21, 2007
    Publication date: May 22, 2008
    Inventors: Georges Filippi, Dominique Bailly