Patents by Inventor Clément Georges Henri GORCE

Clément Georges Henri GORCE 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).

  • Patent number: 11981312
    Abstract: Method for monitoring the braking of the wheels of an aircraft in which the braking of the wheels of the aircraft is controlled by a wheel braking controller actuating the wheel brakes of the aircraft based on both a deceleration regulation request and a thrust reverser deployment request.
    Type: Grant
    Filed: March 13, 2020
    Date of Patent: May 14, 2024
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventor: Clément Georges Henri Gorce
  • Patent number: 11946385
    Abstract: A method for controlling the bending deformation of a turbomachine shaft at rest subjected to the residual heat of operation of the turbomachine, wherein the shaft is rotated at a rotation speed between 0.1 and 50 revolutions per minute depending on the bending deformation deflection of the shaft when the turbomachine is at rest.
    Type: Grant
    Filed: January 29, 2020
    Date of Patent: April 2, 2024
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Clément Georges Henri Gorce, Emelian Charles François Vsevolod Evqueny Tichtchenko
  • Publication number: 20220169216
    Abstract: Method for monitoring the braking of the wheels of an aircraft in which the braking of the wheels of the aircraft is controlled by a wheel braking controller actuating the wheel brakes of the aircraft based on both a deceleration regulation request and a thrust reverser deployment request.
    Type: Application
    Filed: March 13, 2020
    Publication date: June 2, 2022
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventor: Clément Georges Henri GORCE
  • Publication number: 20220098997
    Abstract: A method for controlling the bending deformation of a turbomachine shaft at rest subjected to the residual heat of operation of the turbomachine, wherein the shaft is rotated at a rotation speed between 0.1 and 50 revolutions per minute depending on the bending deformation deflection of the shaft when the turbomachine is at rest.
    Type: Application
    Filed: January 29, 2020
    Publication date: March 31, 2022
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Clément Georges Henri GORCE, Emelian Charles François Vsevolod Evqueny TICHTCHENKO