Patents by Inventor William Bras

William Bras 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).

  • PANEL AND METHODS FOR POLYNUCLEOTIDE DETECTION
    Publication number: 20240141441
    Abstract: This invention relates to molecular systems for detecting a target polynucleotide sequence in a given nucleic acid analyte and methods of use thereof.
    Type: Application
    Filed: February 16, 2022
    Publication date: May 2, 2024
    Inventors: Magdalena STOLAREK-JANUSZKIEWICZ, Ana Luisa Bras Dos Santos Ribeiro DA SILVA-WEATHERLEY, Barnaby William BALMFORTH
  • Device for connecting an aircraft engine and a primary structure of an aircraft pylon comprising a rudder and a system for limiting the displacement of the rudder incorporating a double stop, aircraft comprising such a device
    Patent number: 11679886
    Abstract: A linking device connecting an aircraft engine and a primary structure of an aircraft pylon, comprising a support connected to the primary structure, a spreader having a central part connected to the support and a first and a second end that are connected to thrust rods, at least one limiting system for limiting the travel of the spreader having an upper and a lower stop between which is positioned the first or second end of the spreader, the upper and the lower stop being connected to one another so as to form a single part connected to a fitting secured to the support.
    Type: Grant
    Filed: April 21, 2022
    Date of Patent: June 20, 2023
    Assignee: Airbus Operations SAS
    Inventors: Michael Berjot, Rémi Lansiaux, William Bras, Germain Gueneau, Sébastien Van Arendonk, Jacques Demange, Sébastien Commenge
  • Assembly of an engine with an aircraft pylon
    Patent number: 11519300
    Abstract: An assembly of an engine with a pylon, including a force reacting assembly having a connection device and two rods, the connection device including a shoe. A spreader extends between first and second ends and has a central part connected to the shoe by a main connection including a main rotation pin and axis in a plane of symmetry of the connection device. Two fittings are on either side of the plane of symmetry each having two arms between which the spreader is positioned. A first, respectively second, rod includes a front end fastened to the engine and a rear end fastened to the first, respectively second, end of the spreader and to the first, respectively second, fitting by a secondary connection. Two extensions of the spreader are each associated with a pair of elastic stops. For the first, respectively second, end of the spreader, each stop is between an arm of the first, respectively second, fitting and the extension.
    Type: Grant
    Filed: September 20, 2021
    Date of Patent: December 6, 2022
    Assignee: Airbus Operations (S.A.S.)
    Inventors: Michael Berjot, Rémi Lansiaux, William Bras, Germain Gueneau
  • DEVICE FOR CONNECTING AN AIRCRAFT ENGINE AND A PRIMARY STRUCTURE OF AN AIRCRAFT PYLON COMPRISING A RUDDER AND A SYSTEM FOR LIMITING THE DISPLACEMENT OF THE RUDDER INCORPORATING A DOUBLE STOP, AIRCRAFT COMPRISING SUCH A DEVICE
    Publication number: 20220340293
    Abstract: A linking device connecting an aircraft engine and a primary structure of an aircraft pylon, comprising a support connected to the primary structure, a spreader having a central part connected to the support and a first and a second end that are connected to thrust rods, at least one limiting system for limiting the travel of the spreader having an upper and a lower stop between which is positioned the first or second end of the spreader, the upper and the lower stop being connected to one another so as to form a single part connected to a fitting secured to the support.
    Type: Application
    Filed: April 21, 2022
    Publication date: October 27, 2022
    Inventors: Michael BERJOT, Rémi LANSIAUX, William BRAS, Germain GUENEAU, Sébastien VAN ARENDONK, Jacques DEMANGE, Sébastien COMMENGE
  • ASSEMBLY OF AN ENGINE WITH AN AIRCRAFT PYLON
    Publication number: 20220090518
    Abstract: An assembly of an engine with a pylon, including a force reacting assembly having a connection device and two rods, the connection device including a shoe. A spreader extends between first and second ends and has a central part connected to the shoe by a main connection including a main rotation pin and axis in a plane of symmetry of the connection device. Two fittings are on either side of the plane of symmetry each having two arms between which the spreader is positioned. A first, respectively second, rod includes a front end fastened to the engine and a rear end fastened to the first, respectively second, end of the spreader and to the first, respectively second, fitting by a secondary connection. Two extensions of the spreader are each associated with a pair of elastic stops. For the first, respectively second, end of the spreader, each stop is between an arm of the first, respectively second, fitting and the extension.
    Type: Application
    Filed: September 20, 2021
    Publication date: March 24, 2022
    Inventors: Michael Berjot, Rémi Lansiaux, William Bras, Germain Gueneau