Patents by Inventor Adrien Biscay

Adrien Biscay 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).

  • Airplane turbojet fan blade of cambered profile in its root sections
    Patent number: 11333164
    Abstract: A fan blade for an airplane turbojet, the blade including an airfoil extending axially between a leading edge and a trailing edge and including a plurality of airfoil sections stacked radially between a root section and a tip section. All of the airfoil sections situated between the root section and an airfoil section situated at a radial height corresponding to 30% of a total radial height of the airfoil possess a skeleton curve having a point of inflection.
    Type: Grant
    Filed: May 23, 2013
    Date of Patent: May 17, 2022
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Hanna Reiss, Adrien Biscay, Benoit Fayard, Laurent Jablonski, Damien Merlot
  • AIRPLANE TURBOJET FAN BLADE OF CAMBERED PROFILE IN ITS ROOT SECTIONS
    Publication number: 20150152880
    Abstract: A fan blade for an airplane turbojet, the blade including an airfoil extending axially between a leading edge and a trailing edge and including a plurality of airfoil sections stacked radially between a root section and a tip section. All of the airfoil sections situated between the root section and an airfoil section situated at a radial height corresponding to 30% of a total radial height of the airfoil possess a skeleton curve having a point of inflection.
    Type: Application
    Filed: May 23, 2013
    Publication date: June 4, 2015
    Applicant: SNECMA
    Inventors: Hanna Reiss, Adrien Biscay, Benoit Fayard, Laurent Jablonski, Damien Merlot