Patents by Inventor Adrienne RETIVEAU-LECA

Adrienne RETIVEAU-LECA 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: 12221726
    Abstract: A fibrous structure intended to form the fibrous reinforcement of a part made of composite material includes a fibrous reinforcement densified by a matrix, the fibrous structure having a three-dimensional or multilayer weave between a plurality of layers of warp yarns and a plurality of layers of weft yarns. The fibrous structure includes at least a first portion having a first type of weave and a second portion, continuing on from the first portion, having a second type of weave, the warp yarns and the weft yarns having a degree of interweaving in the first type of weave that is greater than the degree of interweaving of the warp yarns and the weft yarns in the second type of weave.
    Type: Grant
    Filed: February 24, 2022
    Date of Patent: February 11, 2025
    Assignee: SAFRAN
    Inventors: Dominique Marie Christian Coupe, Célline Kribs, Adrienne Retiveau-Leca
  • Patent number: 12129761
    Abstract: A casing of an aircraft turbomachine includes an annular shell extending around an axis A and made of a composite material having fibers that which are woven and embedded in a resin. An annular layer made of abradable material extends inside the shell, around axis A and is obtained by spreading and polymerizing a paste. Support panels extend around axis A and are interposed between the shell and the abradable layer.
    Type: Grant
    Filed: January 26, 2021
    Date of Patent: October 29, 2024
    Assignees: SAFRAN AIRCRAFT ENGINES, SAFRAN AEROSPACE COMPOSITES
    Inventors: Meredith Roberts, Chris Anderson, Nicolas François Paul Broussais-Colella, Ambroise Nicolas Marie Malfroy, Foster Alexander Maxwell, Paul Myslinski, Adrienne Retiveau-Leca
  • Patent number: 12037915
    Abstract: The invention relates to a casing (3) of an aircraft turbomachine, said casing comprising: —an annular shell (9) extending around an axis A and made of a composite material comprising fibres which are woven and embedded in a resin, —an annular layer (4) made of abradable material extending inside the shell, around axis A, and obtained by spreading and polymerising a paste, and—support panels (10) which extend around axis A and are interposed between the shell and the abradable layer.
    Type: Grant
    Filed: January 22, 2021
    Date of Patent: July 16, 2024
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Ambroise Nicolas Marie Malfroy, Nicolas Francois Paul Broussais-Colella, Matthieu Patrick Jean Roger Perlin, Adrienne Retiveau-Leca
  • Publication number: 20240229307
    Abstract: A fibrous structure intended to form the fibrous reinforcement of a part made of composite material includes a fibrous reinforcement densified by a matrix, the fibrous structure having a three-dimensional or multilayer weave between a plurality of layers of warp yarns and a plurality of layers of weft yarns. The fibrous structure includes at least a first portion having a first type of weave and a second portion, continuing on from the first portion, having a second type of weave, the warp yarns and the weft yarns having a degree of interweaving in the first type of weave that is greater than the degree of interweaving of the warp yarns and the weft yarns in the second type of weave.
    Type: Application
    Filed: February 24, 2022
    Publication date: July 11, 2024
    Inventors: Dominique Marie Christian COUPE, Célline KRIBS, Adrienne RETIVEAU-LECA
  • Publication number: 20240133084
    Abstract: A fibrous structure intended to form the fibrous reinforcement of a part made of composite material includes a fibrous reinforcement densified by a matrix, the fibrous structure having a three-dimensional or multilayer weave between a plurality of layers of warp yarns and a plurality of layers of weft yarns. The fibrous structure includes at least a first portion having a first type of weave and a second portion, continuing on from the first portion, having a second type of weave, the warp yarns and the weft yarns having a degree of interweaving in the first type of weave that is greater than the degree of interweaving of the warp yarns and the weft yarns in the second type of weave.
    Type: Application
    Filed: February 24, 2022
    Publication date: April 25, 2024
    Inventors: Dominique Marie Christian COUPE, Célline KRIBS, Adrienne RETIVEAU-LECA
  • Publication number: 20230075984
    Abstract: A casing of an aircraft turbomachine includes an annular shell extending around an axis A and made of a composite material having fibers that which are woven and embedded in a resin. An annular layer made of abradable material extends inside the shell, around axis A and is obtained by spreading and polymerizing a paste. Support panels extend around axis A and are interposed between the shell and the abradable layer.
    Type: Application
    Filed: January 26, 2021
    Publication date: March 9, 2023
    Applicants: SAFRAN AIRCRAFT ENGINES, SAFRAN AEROSPACE COMPOSITES
    Inventors: Meredith ROBERTS, Chris ANDERSON, Nicolas François Paul BROUSSAIS-COLELLA, Ambroise Nicolas Marie MALFROY, Foster Alexander MAXWELL, Paul MYSLINSKI, Adrienne RETIVEAU-LECA
  • Publication number: 20230046918
    Abstract: The invention relates to a casing (3) of an aircraft turbomachine, said casing comprising:—an annular shell (9) extending around an axis A and made of a composite material comprising fibres which are woven and embedded in a resin,—an annular layer (4) made of abradable material extending inside the shell, around axis A, and obtained by spreading and polymerising a paste, and—support panels (10) which extend around axis A and are interposed between the shell and the abradable layer.
    Type: Application
    Filed: January 22, 2021
    Publication date: February 16, 2023
    Inventors: Ambroise Nicolas Marie MALFROY, Nicolas Francois Paul BROUSSAIS-COLELLA, Matthieu Patrick Jean Roger PERLIN, Adrienne RETIVEAU-LECA