Patents by Inventor Nicolas Grosseau

Nicolas Grosseau 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: 10183756
    Abstract: An aircraft engine mount which comprises first and second parts connected by connecting elements and wherein one of the two connected parts comprises at least one transverse hole opening onto an access face of the part and into which there open at least two passage holes each intended to house a threaded shank of one of the connecting elements. The engine mount comprises a transverse nut which comprises at least two bodies joined together each having a tapped hole configured to engage with one of the threaded shanks.
    Type: Grant
    Filed: July 5, 2017
    Date of Patent: January 22, 2019
    Assignee: Airbus Operations SAS
    Inventors: Frederic Journade, Eric Bouchet, Nicolas Grosseau, Antoine Mutin
  • Publication number: 20180009543
    Abstract: An aircraft engine mount which comprises first and second parts connected by connecting elements and wherein one of the two connected parts comprises at least one transverse hole opening onto an access face of the part and into which there open at least two passage holes each intended to house a threaded shank of one of the connecting elements. The engine mount comprises a transverse nut which comprises at least two bodies joined together each having a tapped hole configured to engage with one of the threaded shanks.
    Type: Application
    Filed: July 5, 2017
    Publication date: January 11, 2018
    Inventors: Frederic JOURNADE, Eric BOUCHET, Nicolas GROSSEAU, Antoine MUTIN
  • Patent number: 9216828
    Abstract: An interface device for attaching mobile equipment (1) to an aircraft structure (5) comprises at least an attachment arm (6) and is subject to traction along a main axis of said equipment. The interface device comprises at least one fitting (2) secured to the structure (5), the fitting (2) and the attachment arm (6) having attachment means that coordinate together to offset the tensile stress and that comprise: means to hook a first end of the arm (7) to a first end of the fitting (8), a locking device (9) that coordinates with the hooking means to lock the first end of the arm (7) to said first end of the fitting (8), attachment means to attach a second end of the arm (10) to a second end of the fitting (11).
    Type: Grant
    Filed: October 11, 2011
    Date of Patent: December 22, 2015
    Assignee: Airbus Operations S.A.S.
    Inventors: Christophe Mialhe, Nicolas Grosseau
  • Publication number: 20120102719
    Abstract: An interface device for attaching mobile equipment (1) to an aircraft structure (5) comprises at least an attachment arm (6) and is subject to traction along a main axis of said equipment. The interface device comprises at least one fitting (2) secured to the structure (5), the fitting (2) and the attachment arm (6) having attachment means that coordinate together to offset the tensile stress and that comprise: means to hook a first end of the arm (7) to a first end of the fitting (8), a locking device (9) that coordinates with the hooking means to lock the first end of the arm (7) to said first end of the fitting (8), attachment means to attach a second end of the arm (10) to a second end of the fitting (11).
    Type: Application
    Filed: October 11, 2011
    Publication date: May 3, 2012
    Applicant: Airbus Operations (S.A.S.)
    Inventors: Christophe Mialhe, Nicolas Grosseau