Patents by Inventor Stéphane Boissenin

Stéphane Boissenin 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).

  • Alarm method for avoiding inappropriate rudder bar actuation
    Patent number: 9441655
    Abstract: A method for producing a connector, in particular for repair, in particular in the field of aviation and aerospace, including the steps of: providing a base layer; attaching a first layer of fiber composite material having a first rigidity to the base layer; attaching a second layer of fiber composite material having a second rigidity to the first layer, offset therefrom, the second rigidity being greater than the first rigidity; and riveting the first layer to the base layer and riveting the second layer to the first layer and to the base layer.
    Type: Grant
    Filed: September 24, 2013
    Date of Patent: September 13, 2016
    Assignee: AIRBUS OPERATIONS (SAS)
    Inventors: Bernard Honnons, Stephane Boissenin
  • Alarm method for avoiding inappropriate rudder bar actuation
    Publication number: 20140234019
    Abstract: A method for producing a connector, in particular for repair, in particular in the field of aviation and aerospace, including the steps of: providing a base layer; attaching a first layer of fibre composite material having a first rigidity to the base layer; attaching a second layer of fibre composite material having a second rigidity to the first layer, offset therefrom, the second rigidity being greater than the first rigidity; and riveting the first layer to the base layer and riveting the second layer to the first layer and to the base layer.
    Type: Application
    Filed: September 24, 2013
    Publication date: August 21, 2014
    Inventors: Bernard Honnons, Stephane Boissenin
  • Procedure and device for improving the maneuverability of an aircraft during the approach to landing and flare-out phases
    Patent number: 7896293
    Abstract: The process improves the maneuverability of an aircraft during the approach to landing and then flare-out phases, the aircraft being equipped with air brakes. According to the process, the air brakes are put in a first deployed position during the approach phase, and as a function of a representative parameter of a given altitude and in case of a steep angle approach, they are actuated to transition to a second more retracted position than the first position so as to achieve a flare-out allowing to essentially maintain the same angle of incidence, corresponding in case of a steep angle approach to achieve a flare-out with habitual exterior piloting references during the flare-out phase.
    Type: Grant
    Filed: June 11, 2008
    Date of Patent: March 1, 2011
    Assignee: Airbus
    Inventors: Stéphane Boissenin, Jacques Rosay
  • PROCEDURE AND DEVICE FOR IMPROVING THE MANEUVERABILITY OF AN AIRCRAFT DURING THE APPROACH TO LANDING AND FLARE-OUT PHASES
    Publication number: 20090314897
    Abstract: The process improves the maneuverability of an aircraft during the approach to landing and then flare-out phases, the aircraft being equipped with air brakes. According to the process, the air brakes are put in a first deployed position during the approach phase, and as a function of a representative parameter of a given altitude and in case of a steep angle approach, they are actuated to transition to a second more retracted position than the first position so as to achieve a flare-out allowing to essentially maintain the same angle of incidence, corresponding in case of a steep angle approach to achieve a flare-out with habitual exterior piloting references during the flare-out phase.
    Type: Application
    Filed: June 11, 2008
    Publication date: December 24, 2009
    Applicant: Airbus France
    Inventors: Stephane Boissenin, Jacques Rosay
  • Procedure and device for improving the maneuverability of an aircraft during the approach to landing and flare-out phases
    Patent number: 7614587
    Abstract: The process improves the maneuverability of an aircraft during the approach to landing and then flare-out phases, the aircraft being equipped with air brakes. According to the process, the air brakes are put in a first deployed position during the approach phase, and as a function of a representative parameter of a given altitude and in case of a steep angle approach, they are actuated to transition to a second more retracted position than the first position so as to achieve a flare-out allowing to essentially maintain the same angle of incidence, corresponding in case of a steep angle approach to achieve a flare-out with habitual exterior piloting references during the flare-out phase.
    Type: Grant
    Filed: July 18, 2005
    Date of Patent: November 10, 2009
    Assignee: Airbus
    Inventors: Stéphane Boissenin, Jacques Rosay
  • Procedure and device for improving the maneuverability of an aircraft during the approach to landing and flare-out phases
    Publication number: 20070057114
    Abstract: The process improves the maneuverability of an aircraft during the approach to landing and then flare-out phases, the aircraft being equipped with air brakes. According to the process, the air brakes are put in a first deployed position during the approach phase, and as a function of a representative parameter of a given altitude and in case of a steep angle approach, they are actuated to transition to a second more retracted position than the first position so as to achieve a flare-out allowing to essentially maintain the same angle of incidence, corresponding in case of a steep angle approach to achieve a flare-out with habitual exterior piloting references during the flare-out phase.
    Type: Application
    Filed: July 18, 2005
    Publication date: March 15, 2007
    Applicant: Airbus France
    Inventors: Stéphane Boissenin, Jacques Rosay