Patents by Inventor Alban Francois LOUIS

Alban Francois LOUIS 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).

  • Inlet cone for an aircraft turbomachine
    Patent number: 12104498
    Abstract: An inlet cone for an aircraft turbomachine, having at least one first portion made of a first material, referred to as rigid material, and at least one second portion made of a second material which has a hardness less than that of said first material and which is referred to as flexible material, these second portions being configured to deform elastically in the radial direction with respect to the axis when the cone is being driven to rotate.
    Type: Grant
    Filed: March 23, 2022
    Date of Patent: October 1, 2024
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Alban Francois Louis, Jean-Yves Picart, Morgan Balland, Florent Robert Andre Godin, Baghdad Achbari
  • INLET CONE FOR AN AIRCRAFT TURBOMACHINE
    Publication number: 20240167394
    Abstract: An inlet cone for an aircraft turbomachine, having at least one first portion made of a first material, referred to as rigid material, and at least one second portion made of a second material which has a hardness less than that of said first material and which is referred to as flexible material, these second portions being configured to deform elastically in the radial direction with respect to the axis when the cone is being driven to rotate.
    Type: Application
    Filed: March 23, 2022
    Publication date: May 23, 2024
    Inventors: Alban Francois LOUIS, Jean-Yves PICART, Morgan BALLAND, Florent Robert Andre GODIN, Baghdad ACHBARI
  • Inlet cone for an aircraft turbine engine and associated aircraft turbine engine
    Patent number: 11761346
    Abstract: The present invention thus proposes an inlet cone for an aircraft turbine engine, comprising a frustoconical body and a tip made from elastically deformable material fixed to an end of smaller diameter of said body, the tip comprising a top configured to be situated on an axis of rotation of the cone and a fastening base for attachment on said end of said body. Said base extends in a connecting plane P. Said connecting plane P is inclined relative to said axis of rotation. Said base has a generally circular or oval shape. According to the invention, said connecting plane P is inclined relative to a transverse plane T perpendicular to said axis of rotation.
    Type: Grant
    Filed: June 4, 2020
    Date of Patent: September 19, 2023
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Baptiste Rene Roger Batonnet, Alban Francois Louis
  • INLET CONE FOR AN AIRCRAFT TURBINE ENGINE AND ASSOCIATED AIRCRAFT TURBINE ENGINE
    Publication number: 20220235670
    Abstract: The present invention thus proposes an inlet cone for an aircraft turbine engine, comprising a frustoconical body and a tip made from elastically deformable material fixed to an end of smaller diameter of said body, the tip comprising a top configured to be situated on an axis of rotation of the cone and a fastening base for attachment on said end of said body. Said base extends in a connecting plane P. Said connecting plane P is inclined relative to said axis of rotation. Said base has a generally circular or oval shape. According to the invention, said connecting plane P is inclined relative to a transverse plane T perpendicular to said axis of rotation.
    Type: Application
    Filed: June 4, 2020
    Publication date: July 28, 2022
    Inventors: Baptiste Rene Roger BATONNET, Alban Francois LOUIS