Patents by Inventor Samir El Hammami

Samir El Hammami 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).

  • Engine assembly for aircraft comprising an engine and a mounting device for such an engine
    Patent number: 7677493
    Abstract: The invention relates to an aircraft engine assembly (1) including an engine (6) and an engine mounting device (4), the mounting device being designed to be inserted between a wing of the aircraft and the engine, and comprising a rigid structure (8) and means of mounting the engine onto the rigid structure, the mounting means comprising a forward fastener (10) and an aft fastener (12). According to the invention, the aft fastener comprises two aft half-fasteners (12a) that will each resist at least the forces applied along a longitudinal direction (X) of the engine, and the two aft half-fasteners are arranged so that a horizontal plane (P) passing through a longitudinal axis (5) of the engine passes through each of them.
    Type: Grant
    Filed: June 21, 2006
    Date of Patent: March 16, 2010
    Assignee: Airbus France
    Inventors: Lionel Diochon, Samir El Hammami, Julie Le Louvetel-Poilly, Jean-Baptiste Dumas, Nicolas Koenig
  • Engine assembly for aircraft comprising an engine and a mounting device for such an engine
    Publication number: 20070108341
    Abstract: The invention relates to an aircraft engine assembly (1) including an engine (6) and an engine mounting device (4), the mounting device being designed to be inserted between a wing of the aircraft and the engine, and comprising a rigid structure (8) and means of mounting the engine onto the rigid structure, the mounting means comprising a forward fastener (10) and an aft fastener (12). According to the invention, the aft fastener comprises two aft half-fasteners (12a) that will each resist at least the forces applied along a longitudinal direction (X) of the engine, and the two aft half-fasteners are arranged so that a horizontal plane (P) passing through a longitudinal axis (5) of the engine passes through each of them.
    Type: Application
    Filed: June 21, 2006
    Publication date: May 17, 2007
    Applicant: Airbus France
    Inventors: Lionel Diochon, Samir El Hammami, Julie Le Louvetel-Poilly, Jean-Baptiste Dumas, Nicolas Koenig