Patents by Inventor Nathalie Raimbault

Nathalie Raimbault 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).

  • Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system
    Patent number: 8473121
    Abstract: A fly-by-wire control system for an aircraft including detection of pilot induced oscillations and a mobile control unit for such a system. According to the invention, provision is made for the pivotings of the mobile control unit to be damped by a controllable damper controlled by a detector that detects oscillations corresponding to pilot induced oscillations.
    Type: Grant
    Filed: April 22, 2010
    Date of Patent: June 25, 2013
    Assignee: Airbus Operations SAS
    Inventors: Nathalie Raimbault, Jean-Pierre Gautier, Alain Sagansan, Pierre Fabre
  • FLY-BY-WIRE CONTROL SYSTEM FOR AN AIRCRAFT COMPRISING DETECTION OF PILOT INDUCED OSCILLATIONS AND A CONTROL FOR SUCH A SYSTEM
    Publication number: 20100200701
    Abstract: A fly-by-wire control system for an aircraft including detection of pilot induced oscillations and a mobile control unit for such a system, According to the invention, provision is made for the pivotings of the mobile control unit to be damped by a controllable damper controlled by a detector that detects oscillations corresponding to pilot induced oscillations.
    Type: Application
    Filed: April 22, 2010
    Publication date: August 12, 2010
    Applicant: AIRBUS FRANCE
    Inventors: Nathalie RAIMBAULT, Jean-Pierre Gautier, Alain Sagansan, Pierre Fabre
  • Method and device for detecting pilot induced oscillations in an aircraft
    Patent number: 7225061
    Abstract: A method and device for detecting pilot induced oscillations in an aircraft may detect signals having frequencies of between 0.3 Hz and 0.6 Hz within commands signals generated by a pilot for controlling an aerodynamic surface of the aircraft. The energy of the detected signals is analyzed to determine whether significant pilot induced oscillations are present within the command signals, and an indication of the degree of the oscillations is generated for use by the pilot.
    Type: Grant
    Filed: November 12, 2003
    Date of Patent: May 29, 2007
    Assignee: Airbus France
    Inventors: Nathalie Raimbault, Pierre Fabre
  • Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system
    Publication number: 20050021193
    Abstract: Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system. According to the invention, provision is made for the pivotings of said control (2) to be damped by controllable damping means (15, 16) controlled by means (7) detecting oscillations corresponding to pilot induced oscillations.
    Type: Application
    Filed: November 10, 2003
    Publication date: January 27, 2005
    Inventors: Nathalie Raimbault, Jean-Pierre Gautier, Alain Sagansan, Pierre Fabre
  • Method and device for detecting pilot induced oscillations in an aircraft
    Publication number: 20040098176
    Abstract: Method and device for detecting pilot induced oscillations in an aircraft.
    Type: Application
    Filed: November 12, 2003
    Publication date: May 20, 2004
    Inventors: Nathalie Raimbault, Pierre Fabre