Patents by Inventor Jean-Philippe Huynh

Jean-Philippe Huynh 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).

  • Device for aiding the navigation and guidance of an aircraft, and system comprising such a device
    Patent number: 8447520
    Abstract: Device for aiding the navigation and guidance of an aircraft, and system comprising such a device. The device (1) comprises at least three independent channels and it comprises at least one computer (2) which contains means (4) for storing and means (6, 7) for calculating positions and deviations.
    Type: Grant
    Filed: April 30, 2009
    Date of Patent: May 21, 2013
    Assignee: Airbus Operations (SAS)
    Inventors: Josep Gine I Cortiella, Jean-Philippe Huynh
  • Method and device for determining a reliable position of an aircraft
    Patent number: 8244467
    Abstract: The invention relates to a method and device for determining a reliable position of an aircraft. The device (1) includes means (3, 10) for determining different aircraft position values and means (8, 16, 18) for deducing a reliable position therefrom, using coherence tests and a consolidation method.
    Type: Grant
    Filed: June 16, 2008
    Date of Patent: August 14, 2012
    Assignee: Airbus Operations SAS
    Inventors: Jean-Philippe Huynh, Alain Guillet, Stéphane Dattler, Grégory Ortet
  • Device for aiding the piloting of an aircraft during an approach phase for the purpose of landing
    Patent number: 8112188
    Abstract: Disclosed is a device for aiding the piloting of an aircraft in an approach phase during landing. The device includes a guidance system for aiding guidance of the aircraft. Controllers can be actuated by the system during an initial phase in accordance with a first guidance mode and during a terminal phase in accordance with a second guidance mode. The transition between the first and second guidance modes can be achieved automatically by the guidance system.
    Type: Grant
    Filed: February 14, 2007
    Date of Patent: February 7, 2012
    Assignee: Airbus Operation SAS
    Inventors: Patrice Rouquette, Jean-Philippe Huynh
  • Method and device for monitoring a position indication of an aircraft
    Patent number: 7908046
    Abstract: A device and method calculate a global error relating to a position indication of an aircraft and compare the global error with a threshold value, which depends on flight constraints.
    Type: Grant
    Filed: May 19, 2008
    Date of Patent: March 15, 2011
    Assignee: Airbus France
    Inventors: Jean-Philippe Huynh, Alain Guillet, Stephane Dattler, Gregory Ortet
  • DEVICE FOR AIDING THE NAVIGATION AND GUIDANCE OF AN AIRCRAFT, AND SYSTEM COMPRISING SUCH A DEVICE
    Publication number: 20110060483
    Abstract: Device for aiding the navigation and guidance of an aircraft, and system comprising such a device. The device (1) comprises at least three independent channels and it comprises at least one computer (2) which contains means (4) for storing and means (6, 7) for calculating positions and deviations.
    Type: Application
    Filed: April 30, 2009
    Publication date: March 10, 2011
    Applicant: AIRBUS OPERATIONS (SAS)
    Inventors: Josep Gine I Cortiella, Jean-Philippe Huynh
  • Device for monitoring aircraft control information
    Patent number: 7899585
    Abstract: A device includes a computer for computing the difference between at least two items of control information that are generated by at least two different flight management systems of an aircraft, and a system for generating a warning signal if the difference is greater than a threshold value.
    Type: Grant
    Filed: June 5, 2007
    Date of Patent: March 1, 2011
    Assignee: Airbus France
    Inventors: Patrice Rouquette, Jean-Philippe Huynh
  • METHOD AND DEVICE FOR DETERMINING A RELIABLE POSITION OF AN AIRCRAFT
    Publication number: 20100169014
    Abstract: The invention relates to a method and device for determining a reliable position of an aircraft. The device (1) includes means (3, 10) for determining different aircraft position values and means (8, 16, 18) for deducing a reliable position therefrom, using coherence tests and a consolidation method.
    Type: Application
    Filed: June 16, 2008
    Publication date: July 1, 2010
    Applicant: Airbus Operations (SAS)
    Inventors: Jean-Philippe Huynh, Alain Guillet, Stéphane Dattler, Grégory Ortet
  • DEVICE FOR AIDING THE PILOTING OF AN AIRCRAFT DURING AN APPROACH PHASE FOR THE PURPOSE OF LANDING
    Publication number: 20090024261
    Abstract: Device for aiding the piloting of an aircraft during an approach phase for the purpose of landing. The device (1) comprises a guidance system (8) for aiding guidance of the aircraft, in the event of the actuation of a control means (11A, 11B, 11n), both during an initial phase in accordance with a first guidance mode and during a terminal phase in accordance with a second guidance mode, the transition between these first and second guidance modes being achieved automatically by the guidance system (8).
    Type: Application
    Filed: February 14, 2007
    Publication date: January 22, 2009
    Applicant: Airbus France
    Inventors: Patrice Rouquette, Jean-Philippe Huynh
  • METHOD AND DEVICE FOR MONITORING A POSITION INDICATION OF AN AIRCRAFT
    Publication number: 20080294306
    Abstract: The device (1) comprises means (8, 9, 10) for calculating a global error relating to a position indication of the aircraft, means (13) for comparing this global error with a threshold value which depends on the flight constraints, and alarm means (15).
    Type: Application
    Filed: May 19, 2008
    Publication date: November 27, 2008
    Applicant: AIRBUS France
    Inventors: Jean-Philippe Huynh, Alain Guillet, Stephane Dattler, Gregory Ortet
  • DEVICE FOR MONITORING AIRCRAFT CONTROL INFORMATION
    Publication number: 20070299568
    Abstract: The device (1) comprises a computer (9) for computing the difference between at least two items of control information that are generated by at least two different flight management systems of the aircraft, and a system (12) for generating a warning signal if this difference is greater than a threshold value.
    Type: Application
    Filed: June 5, 2007
    Publication date: December 27, 2007
    Applicant: AIRBUS FRANCE
    Inventors: Patrice Rouquette, Jean-Philippe Huynh