Patents by Inventor Francois Conte

Francois Conte 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).

  • Bypass turbojet engine nacelle
    Patent number: 8523516
    Abstract: The nacelle (1) comprises an air intake (5) upstream of the turbojet engine (2), a middle section (6) an internal casing (6a) of which is intended to surround a fan (3) of the turbojet engine (2), and a downstream section (7) comprising an external structure (7a)which is rigidly connected to a downstream part of the casing (6a) of the fan (3) so as to support the turbojet engine (2) and has means of attachment to a strut (12) intended to be connected to a fixed structure (13) of an aeroplane.
    Type: Grant
    Filed: October 5, 2007
    Date of Patent: September 3, 2013
    Assignee: Aircelle
    Inventors: Guy Bernard Vauchel, Jerome Collier, Patrice Dhainault, Francois Conte, Nicolas Hillereau, Pierre-Alain Chouard, Guillaume Lefort
  • ATTACHMENT STRUCTURE FOR A TURBOJET ENGINE
    Publication number: 20110308257
    Abstract: The present invention relates to an attachment structure (1) for attaching a turbojet engine (2) to a fixed structure of an airplane via an attachment pylon, characterized in that it comprises a one-piece box section intended to extend at least partially on each side of a fan casing (3) of the turbojet engine about a substantially longitudinal axis thereof and comprising, on the one hand, means of attachment to the pylon and, on the other hand, means of attachment of the engine (4) which are positioned on the box section on each side of a substantially longitudinal axis of the turbojet engine and are intended to be connected to part of the turbojet engine in such a way as to react the forces applied thereto.
    Type: Application
    Filed: January 9, 2009
    Publication date: December 22, 2011
    Applicant: AIRCELLE
    Inventors: Guy Bernard Vauchel, Andre Baillard, Francois Conte
  • BYPASS TURBOJET ENGINE NACELLE
    Publication number: 20100040466
    Abstract: The nacelle (1) comprises an air intake (5) upstream of the turbojet engine (2), a middle section (6) an internal casing (6a) of which is intended to surround a fan (3) of the turbojet engine (2), and a downstream section (7) comprising an external structure (7a)which is rigidly connected to a downstream part of the casing (6a) of the fan (3) so as to support the turbojet engine (2) and has means of attachment to a strut (12) intended to be connected to a fixed structure (13) of an aeroplane.
    Type: Application
    Filed: October 5, 2007
    Publication date: February 18, 2010
    Applicant: AIRCELLE
    Inventors: Guy Bernard Vauchel, Jerome Collier, Patrice Dhainault, Francois Conte, Nicolas Hillereau, Pierre-Alain Chouard, Guillaume Lefort