Patents by Inventor Sylvain DOUSSEAUD

Sylvain DOUSSEAUD 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).

  • Part to modify the profile of an aerodynamic jet
    Patent number: 9982546
    Abstract: A part to modify the profile of an aerodynamic jet, including: a first face configured to be secured on the aerodynamic jet, and a second face defining a modified aerodynamic jet profile, configured to modify an initial profile of the aerodynamic jet.
    Type: Grant
    Filed: July 24, 2013
    Date of Patent: May 29, 2018
    Assignee: SNECMA
    Inventors: Gregory Nicolas Gerald Gillant, Sylvain Dousseaud, Stephane Clemot
  • Insert with an external surface which is part of at least one aerodynamic profile of a turbomachine test blade
    Patent number: 9695693
    Abstract: The invention relates to an insert for a turbine engine test vane including the insert and a vane body. The insert includes at least two external surfaces. The insert is configured to fit into the vane body, such that the external surfaces are vane aerodynamic surfaces each forming part of a vane aerodynamic profile.
    Type: Grant
    Filed: July 2, 2014
    Date of Patent: July 4, 2017
    Assignee: SNECMA
    Inventors: Sylvain Dousseaud, Gregory Nicolas Gerald Gillant
  • PART TO MODIFY THE PROFILE OF AN AERODYNAMIC JET
    Publication number: 20150176419
    Abstract: A part to modify the profile of an aerodynamic jet, including: a first face configured to be secured on the aerodynamic jet, and a second face defining a modified aerodynamic jet profile, configured to modify an initial profile of the aerodynamic jet.
    Type: Application
    Filed: July 24, 2013
    Publication date: June 25, 2015
    Applicant: SNECMA
    Inventors: Gregory Nicolas Gerald Gillant, Sylvain Dousseaud, Stephane Clemot
  • INSERT WITH AN EXTERNAL SURFACE WHICH IS PART OF AT LEAST ONE AERODYNAMIC PROFILE OF A TURBOMACHINE TEST BLADE
    Publication number: 20150017005
    Abstract: The invention relates to an insert for a turbine engine test vane including the insert and a vane body. The insert includes at least two external surfaces. The insert is configured to fit into the vane body, such that the external surfaces are vane aerodynamic surfaces each forming part of a vane aerodynamic profile.
    Type: Application
    Filed: July 2, 2014
    Publication date: January 15, 2015
    Applicant: SNECMA
    Inventors: Sylvain DOUSSEAUD, Gregory Nicolas, Gerald Gillant