Patents by Inventor Christophe Devillers

Christophe Devillers 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: 11643192
    Abstract: A bogey undercarriage having at least two axles, each carrying at least two wheels, wherein at least one of the axles carries a wheel fitted with a rotary drive device and no brake device, while the other wheels are provided with brake devices and no movement devices is provided. A braking method applied to such an undercarriage is also provided.
    Type: Grant
    Filed: March 28, 2019
    Date of Patent: May 9, 2023
    Assignee: SAFRAN LANDING SYSTEMS
    Inventors: Jérôme Gui, Jean-Yves Ravel, Christophe Devillers
  • Publication number: 20190300161
    Abstract: A bogey undercarriage having at least two axles, each carrying at least two wheels, wherein at least one of the axles carries a wheel fitted with a rotary drive device and no brake device, while the other wheels are provided with brake devices and no movement devices is provided. A braking method applied to such an undercarriage is also provided.
    Type: Application
    Filed: March 28, 2019
    Publication date: October 3, 2019
    Applicant: SAFRAN LANDING SYSTEMS
    Inventors: Jérôme Gui, Jean-Yves Ravel, Christophe Devillers
  • Patent number: 8955799
    Abstract: A stop pad (11) for an aircraft landing gear arranged to provide protection against impact between first and second elements of the landing gear, the stop pad being arranged to provide an indication that it is been subject to an impact against one of the first or second landing gear elements, the impact having an impact load above a predetermined threshold level.
    Type: Grant
    Filed: February 16, 2011
    Date of Patent: February 17, 2015
    Assignee: Messier-Dowty Limited
    Inventors: Christophe Devillers, Ben Hodgkinson
  • Publication number: 20130264417
    Abstract: A stop pad (11) for an aircraft landing gear arranged to provide protection against impact between first and second elements of the landing gear, the stop pad being arranged to provide an indication that it is been subject to an impact against one of the first or second landing gear elements, the impact having an impact load above a predetermined threshold level.
    Type: Application
    Filed: February 16, 2011
    Publication date: October 10, 2013
    Inventors: Christophe Devillers, BEN Hodgkinson