Patents by Inventor Thomas Chauveau

Thomas Chauveau 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).

  • Fuel filter having high resistance to icing
    Patent number: 10946317
    Abstract: A cartridge for a filtering device, includes a cylindrically arranged pleated cloth, the pleats being parallel to the generatrix of the cylinder, wherein the cylinder includes a non-pleated region which is to be placed across from a fuel inlet into the filtering device.
    Type: Grant
    Filed: May 31, 2017
    Date of Patent: March 16, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Bellal Waissi, Thomas Chauveau, Philippe Vertenoeuil, José Rodrigues
  • Turbine engine provided with a lubrication unit
    Patent number: 10458422
    Abstract: A turbine engine includes two rotary shafts and a lubrication unit. The lubrication unit has at least one pump which a casing inside of which a rotor is mounted and driven by one of the rotary shafts. The pump casing is rotated by the other rotary shaft such that the actuation of the pump depends on the difference between rotational speeds of the shafts. The shafts are a drive shaft and a fan shaft, respectively, wherein the fan shaft is driven by the drive shaft by means of a reduction gear which is lubricated by the lubrication unit. The reduction gear is annular and the pump passes axially therethrough.
    Type: Grant
    Filed: February 5, 2015
    Date of Patent: October 29, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Benoît Jean Henri Gomanne, Michel Gilbert Roland Brault, Thomas Chauveau, Bellal Waissi
  • FUEL FILTER HAVING HIGH RESISTANCE TO ICING
    Publication number: 20190193002
    Abstract: A cartridge for a filtering device, includes a cylindrically arranged pleated cloth, the pleats being parallel to the generatrix of the cylinder, wherein the cylinder includes a non-pleated region which is to be placed across from a fuel inlet into the filtering device.
    Type: Application
    Filed: May 31, 2017
    Publication date: June 27, 2019
    Inventors: Bellal WAISSI, Thomas CHAUVEAU, Philippe VERTENOEUIL, José RODRIGUES
  • TURBINE ENGINE PROVIDED WITH A LUBRICATION UNIT
    Publication number: 20170009776
    Abstract: A turbine engine includes two rotary shafts and a lubrication unit. The lubrication unit has at least one pump which a casing inside of which a rotor is mounted and driven by one of the rotary shafts. The pump casing is rotated by the other rotary shaft such that the actuation of the pump depends on the difference between rotational speeds of the shafts. The shafts are a drive shaft and a fan shaft, respectively, wherein the fan shaft is driven by the drive shaft by means of a reduction gear which is lubricated by the lubrication unit. The reduction gear is annular and the pump passes axially therethrough.
    Type: Application
    Filed: February 5, 2015
    Publication date: January 12, 2017
    Applicant: Safran Aircraft Engines
    Inventors: Benoît Jean Henri Gomanne, Michel Gilbert Roland Brault, Thomas Chauveau, Bellal Waissi