Patents by Inventor Guillaume Jose RODRIGUES

Guillaume Jose RODRIGUES 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).

  • Device for measuring at least one parameter of an aerodynamic flow of a turbine engine equipped with a vibratory damping means and turbine engine duct equipped with such a device
    Patent number: 10907507
    Abstract: A measuring device for measuring at least one parameter of an aerodynamic flow of a turbine engine. The device operates to collect parameters of the flow. A body extends along a radial axis (L). A connecting part is fastened to a first end of the body and designed to secure the measuring device to a radially outer wall of the turbine engine. A stud is inserted and mounted on a second end of the body radially opposite the first end. The stud includes at least a portion of a rubberlike material designed to come into contract with a radially inner wall of the turbine engine.
    Type: Grant
    Filed: October 8, 2018
    Date of Patent: February 2, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Jeremy Giordan, Thibault Xavier Alexis Berranger, Guillaume Jose Rodrigues, Stephane Rousselin, Mathieu Raymond Paul Sezeur
  • DEVICE FOR MEASURING AT LEAST ONE PARAMETER OF AN AERODYNAMIC FLOW OF A TURBINE ENGINE EQUIPPED WITH A VIBRATORY DAMPING MEANS AND TURBINE ENGINE DUCT EQUIPPED WITH SUCH A DEVICE
    Publication number: 20190107008
    Abstract: A measuring device for measuring at least one parameter of an aerodynamic flow of a turbine engine. The device operates to collect parameters of the flow. A body extends along a radial axis (L). A connecting part is fastened to a first end of the body and designed to secure the measuring device to a radially outer wall of the turbine engine. A stud is inserted and mounted on a second end of the body radially opposite the first end. The stud includes at least a portion of a rubberlike material designed to come into contract with a radially inner wall of the turbine engine.
    Type: Application
    Filed: October 8, 2018
    Publication date: April 11, 2019
    Inventors: Jeremy GIORDAN, Thibault Xavier Alexis BERRANGER, Guillaume Jose RODRIGUES, Stephane ROUSSELIN, Mathieu Raymond Paul SEZEUR