Patents by Inventor Jérémy Vielcanet

Jérémy Vielcanet 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).

  • Lubrication device for a turbine engine
    Patent number: 10677095
    Abstract: The invention relates to a lubrication device for a turbine engine, comprising an oil intake pipe (23) provided with a pump (24) for supplying oil and control means (25) located downstream from the supply pump (24), a supply pipe (26) intended for supplying oil to a member to be lubricated and a recirculation pipe (27), the control means (25) making it possible to direct all or part of the flow of oil from the intake pipe (23) towards the supply pipe (26) and/or towards the recirculation pipe (27), the pump (24) being driven by at least one rotary member of an accessory gearbox of the turbine engine.
    Type: Grant
    Filed: June 11, 2015
    Date of Patent: June 9, 2020
    Assignee: Safran Aircraft Engines
    Inventors: Jérémy Vielcanet, Caroline Frantz, David Simon
  • Lubrication device for a turbine engine
    Patent number: 10273826
    Abstract: The invention relates to a lubrication device for a turbine engine, comprising an oil intake pipe (23) provided with a pump (24) for supplying oil and control means (30) located downstream from the supply pump (24), a supply pipe (26) intended for supplying oil to a member to be lubricated and a recirculation pipe (27) connected upstream from the supply pump (24), the control means (30) making it possible to direct all or part of the flow of oil from the intake pipe (23) towards the supply pipe (26) and/or towards the recirculation pipe (27).
    Type: Grant
    Filed: November 7, 2014
    Date of Patent: April 30, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Jérémy Vielcanet, Caroline Frantz, Antoine Laigle
  • LUBRICATION DEVICE FOR A TURBINE ENGINE
    Publication number: 20170198605
    Abstract: The invention relates to a lubrication device for a turbine engine, comprising an oil intake pipe (23) provided with a pump (24) for supplying oil and control means (25) located downstream from the supply pump (24), a supply pipe (26) intended for supplying oil to a member to be lubricated and a recirculation pipe (27), the control means (25) making it possible to direct all or part of the flow of oil from the intake pipe (23) towards the supply pipe (26) and/or towards the recirculation pipe (27), the pump (24) being driven by at least one rotary member of an accessory gearbox of the turbine engine.
    Type: Application
    Filed: June 11, 2015
    Publication date: July 13, 2017
    Applicant: Safran Aircraft Engines
    Inventors: Jérémy VIELCANET, Caroline FRANTZ, David SIMON
  • LUBRICATION DEVICE FOR A TURBINE ENGINE
    Publication number: 20160290162
    Abstract: The invention relates to a lubrication device for a turbine engine, comprising an oil intake pipe (23) provided with a pump (24) for supplying oil and control means (30) located downstream from the supply pump (24), a supply pipe (26) intended for supplying oil to a member to be lubricated and a recirculation pipe (27) connected upstream from the supply pump (24), the control means (30) making it possible to direct all or part of the flow of oil from the intake pipe (23) towards the supply pipe (26) and/or towards the recirculation pipe (27).
    Type: Application
    Filed: November 7, 2014
    Publication date: October 6, 2016
    Applicant: Snecma
    Inventors: Jérémy Vielcanet, Caroline Frantz, Antoine Laigle