Patents by Inventor Gaëlle Inès Méganne MOREAUX

Gaëlle Inès Méganne MOREAUX 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).

  • Device for holding a cooling tube for a turbomachine casing
    Patent number: 11555405
    Abstract: A device for holding (101) at least one cooling tube (120) of a turbomachine casing (10) cooling system (100), the holding device including a fixing frame (104), a holding member (160) being configured to hold two cooling tubes (120), and a connection assembly (140) between the holding member (160) and a fixing frame (104), extending on either side of the frame, the connection assembly (160) comprising a connection part (150) extending through an opening (108) of the fixing frame from an outer portion (141) to the inner portion (142) of the connection assembly, the inner portion (142) being disposed between two cooling tubes (120) and secured to the holding member (160) while the outer portion (141) comprises a resilient return member (170) urged in compression towards the fixing frame by the connection part (150).
    Type: Grant
    Filed: December 5, 2019
    Date of Patent: January 17, 2023
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Simon Nicolas Morliere, Nicolas Jean-Marc Marcel Beauquin, Stéphane Pierre Guillaume Blanchard, Gaëlle Inès Méganne Moreaux
  • DEVICE FOR HOLDING A COOLING TUBE FOR A TURBOMACHINE CASING
    Publication number: 20200182058
    Abstract: A device for holding (101) at least one cooling tube (120) of a turbomachine casing (10) cooling system (100), the holding device including a fixing frame (104), a holding member (160) being configured to hold two cooling tubes (120), and a connection assembly (140) between the holding member (160) and a fixing frame (104), extending on either side of the frame, the connection assembly (160) comprising a connection part (150) extending through an opening (108) of the fixing frame from an outer portion (141) to the inner portion (142) of the connection assembly, the inner portion (142) being disposed between two cooling tubes (120) and secured to the holding member (160) while the outer portion (141) comprises a resilient return member (170) urged in compression towards the fixing frame by the connection part (150).
    Type: Application
    Filed: December 5, 2019
    Publication date: June 11, 2020
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Simon Nicolas MORLIERE, Nicolas Jean-Marc Marcel BEAUQUIN, Stéphane Pierre Guillaume BLANCHARD, Gaëlle Inès Méganne MOREAUX