Patents by Inventor Raphaël Medina

Raphaël Medina 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: 12504057
    Abstract: A kit of parts to provide a reconfigurable epicyclic gear system, The kit of parts includes at least one sun gear; a planet carrier; a plurality of sets of planet gears configured to be mounted on the planet carrier and to mesh with the at least one sun gear; and a plurality of ring gears configured to mesh with the plurality of sets of planet gears; wherein the at least one sun gear, the plurality of sets of planet gears and the plurality of ring gears all have the same modulus such that they can be arranged in different configurations that each produce a different output torque.
    Type: Grant
    Filed: January 8, 2024
    Date of Patent: December 23, 2025
    Assignee: GOODRICH ACTUATION SYSTEMS SAS
    Inventors: Raphaël Medina, Maxime Serrand, Thomas Moulon, Vincent Potel
  • Publication number: 20240229899
    Abstract: A kit of parts to provide a reconfigurable epicyclic gear system, The kit of parts includes at least one sun gear; a planet carrier; a plurality of sets of planet gears configured to be mounted on the planet carrier and to mesh with the at least one sun gear; and a plurality of ring gears configured to mesh with the plurality of sets of planet gears; wherein the at least one sun gear, the plurality of sets of planet gears and the plurality of ring gears all have the same modulus such that they can be arranged in different configurations that each produce a different output torque.
    Type: Application
    Filed: January 8, 2024
    Publication date: July 11, 2024
    Inventors: Raphaël Medina, Maxime Serrand, Thomas Moulon, Vincent Potel
  • Patent number: 11035445
    Abstract: A screw (20) assembly for an actuator (10) is described comprising: a screw (20); a nut (22) threaded on said screw (20), such that rotation of said screw (20) causes axial movement of said nut (22); a stop located at an end of said screw (20) and defining an axial limit of said nut (22); a first feature located on said nut (22); and a second feature located on said stop; wherein said first and second features are configured to cooperate with one another substantially upon contact of said nut (22) with said stop so as to indicate an amount of free movement between said nut (22) and said screw (20).
    Type: Grant
    Filed: December 1, 2014
    Date of Patent: June 15, 2021
    Assignee: GOODRICH ACTUATION SYSTEMS SAS
    Inventors: Thomas Moulon, Raphaël Medina
  • Publication number: 20170335931
    Abstract: A screw (20) assembly for an actuator (10) is described comprising: a screw (20); a nut (22) threaded on said screw (20), such that rotation of said screw (20) causes axial movement of said nut (22); a stop located at an end of said screw (20) and defining an axial limit of said nut (22); a first feature located on said nut (22); and a second feature located on said stop; wherein said first and second features are configured to cooperate with one another substantially upon contact of said nut (22) with said stop so as to indicate an amount of free movement between said nut (22) and said screw (20).
    Type: Application
    Filed: December 1, 2014
    Publication date: November 23, 2017
    Applicant: Goodrich Actuation Systems SAS
    Inventors: Thomas Moulon, Raphaël Medina
  • Patent number: 8944372
    Abstract: A device (13) for detecting the breakage of a primary path in a flight control actuator, said actuator having a primary path (1) comprising a rotary hollow screw (2), a secondary path (10) comprising a safety rod (3) that reacts the load passing through the screw (2), said device (13) being characterized in that it comprises a position sensor (15), connected to the screw (2), to measure information representative of the angular position thereof, and a disconnection system (17) able to disconnect the screw (2) position sensor (15) in the event of relative movement of the rod (3) with respect to the screw (2) if there is a break in the primary path (1).
    Type: Grant
    Filed: April 14, 2011
    Date of Patent: February 3, 2015
    Assignee: Goodrich Actuation Systems SAS
    Inventors: Thomas Moulon, Raphaël Medina
  • Publication number: 20130105623
    Abstract: A device (13) for detecting the breakage of a primary path in a flight control actuator, said actuator having a primary path (1) comprising a rotary hollow screw (2), a secondary path (10) comprising a safety rod (3) that reacts the load passing through the screw (2), said device (13) being characterized in that it comprises a position sensor (15), connected to the screw (2), to measure information representative of the angular position thereof, and a disconnection system (17) able to disconnect the screw (2) position sensor (15) in the event of relative movement of the rod (3) with respect to the screw (2) if there is a break in the primary path (1).
    Type: Application
    Filed: April 14, 2011
    Publication date: May 2, 2013
    Inventors: Thomas Moulon, Raphaël Medina
  • Patent number: 8052084
    Abstract: The assembly comprises a first and a second nut intended to cooperate with a screw in particular provided in an adjustable tailplane actuator for an aircraft, and a mechanical connection between the first and the second nut comprising means for fusible driving of the second nut by the first nut, in which the mechanical connection also comprises adjustable spacing means forming a wedge between the first and second nuts.
    Type: Grant
    Filed: May 9, 2008
    Date of Patent: November 8, 2011
    Assignee: Goodrich Actuation Systems SAS
    Inventors: Isabelle Port-Robach, Raphaël Medina, Christian Dorval, Rui Amaral