Patents by Inventor Pierre DEBUSSCHERE

Pierre DEBUSSCHERE 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: 10023301
    Abstract: A system including a load factor control module for calculating a deflection order on manual actuation of a control column by a pilot of the aircraft and transmitting that deflection order to at least one elevator of the aircraft, a longitudinal attitude control module for maintaining the longitudinal attitude of the aircraft at a target attitude in the event of absence of manual actuation of the control column by the pilot during a flight, and a transition management module for determining and storing a present longitudinal attitude value of the aircraft at a recording moment and transmitting that longitudinal attitude value to the longitudinal attitude control module for the longitudinal attitude control module to use the longitudinal attitude value as the target attitude.
    Type: Grant
    Filed: April 12, 2016
    Date of Patent: July 17, 2018
    Assignee: Airbus Operations SAS
    Inventors: Mathieu Carton, Pierre Debusschere, Laurent Albugues
  • Patent number: 9663219
    Abstract: The system comprises at least one lift generator element that is able to modify directly the lift of the aircraft and means for defining a deflection instruction upon actuation by a pilot of the aircraft of a control column of the aircraft generating a vertical load factor control value and applying it to an elevator and simultaneously defining a command instruction and applying it to the lift generator element to generate a direct lift.
    Type: Grant
    Filed: July 23, 2015
    Date of Patent: May 30, 2017
    Assignee: AIRBUS OPERATIONS SAS
    Inventors: Mathieu Carton, Pierre Debusschere, David Chabe
  • Publication number: 20160304189
    Abstract: A system including a load factor control module for calculating a deflection order on manual actuation of a control column by a pilot of the aircraft and transmitting that deflection order to at least one elevator of the aircraft, a longitudinal attitude control module for maintaining the longitudinal attitude of the aircraft at a target attitude in the event of absence of manual actuation of the control column by the pilot during a flight, and a transition management module for determining and storing a present longitudinal attitude value of the aircraft at a recording moment and transmitting that longitudinal attitude value to the longitudinal attitude control module for the longitudinal attitude control module to use the longitudinal attitude value as the target attitude.
    Type: Application
    Filed: April 12, 2016
    Publication date: October 20, 2016
    Inventors: Mathieu Carton, Pierre Debusschere, Laurent Albugues
  • Publication number: 20160023749
    Abstract: The system comprises at least one lift generator element that is able to modify directly the lift of the aircraft and means for defining a deflection instruction upon actuation by a pilot of the aircraft of a control column of the aircraft generating a vertical load factor control value and applying it to an elevator and simultaneously defining a command instruction and applying it to the lift generator element to generate a direct lift.
    Type: Application
    Filed: July 23, 2015
    Publication date: January 28, 2016
    Inventors: Mathieu CARTON, Pierre DEBUSSCHERE, David CHABE