Patents by Inventor Simone Iurlaro

Simone Iurlaro 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: 11982201
    Abstract: An engine assembly defining an axial direction (A) and including a gearbox, an engine core including at least one rotor, and a flexible coupling shaft having a first end and a second end along the axial direction (A). The first end of the flexible coupling shaft is connected to the engine core and the second end of the flexible coupling shaft is connected to the gearbox. A damper system is positioned at the second end of the flexible coupling shaft. The damper system is configured to reduce vibrations to the flexible coupling shaft during operation of the engine assembly.
    Type: Grant
    Filed: December 15, 2021
    Date of Patent: May 14, 2024
    Assignee: GE AVIO S.R.L.
    Inventors: Marco Garabello, Simone Iurlaro, Salvatore Garofalo, Alessio Gargioli, Giuseppe Argentieri
  • Publication number: 20230121607
    Abstract: An aircraft engine component (100) may include a wall (200) comprising an aluminum alloy and/or a magnesium alloy, and a protective coating (108) covering the wall (200). The protective coating (108) may include a prime layer (206), a silicone elastomer layer (208), and an abrasion resistant layer (210). The prime layer (206) may at least partially cover a surface (202) of the wall (200). The prime layer (206) may include a silane coupling agent and an organic titanate. The silicone elastomer layer (208) may at least partially cover the prime layer (206). The silicone elastomer layer (208) may include one or more filler materials dispersed in a matrix of cross-linked silicone polymers. The abrasion resistant layer (210) may at least partially cover the silicone elastomer layer (208). The abrasion resistant layer (210) may include a fiber-reinforced elastomeric material.
    Type: Application
    Filed: December 30, 2021
    Publication date: April 20, 2023
    Inventors: Simone Iurlaro, Alessio Gargioli, Marco Garabello, Salvatore Garofalo, Enrica Gilardi, Ottavia Pica, Giuseppe Argentieri
  • Publication number: 20230019363
    Abstract: An engine assembly defining an axial direction (A) and including a gearbox, an engine core including at least one rotor, and a flexible coupling shaft having a first end and a second end along the axial direction (A). The first end of the flexible coupling shaft is connected to the engine core and the second end of the flexible coupling shaft is connected to the gearbox. A damper system is positioned at the second end of the flexible coupling shaft. The damper system is configured to reduce vibrations to the flexible coupling shaft during operation of the engine assembly.
    Type: Application
    Filed: December 15, 2021
    Publication date: January 19, 2023
    Inventors: Marco Garabello, Simone Iurlaro, Salvatore Garofalo, Alessio Gargioli, Giuseppe Argentieri