Patents by Inventor FRANÇOIS BAUVIR

FRANÇOIS BAUVIR 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).

  • Leading edge slat with optimized structure
    Patent number: 11260956
    Abstract: A leading edge slat of a wing element of an aircraft. The aircraft defining a mark including a main fuselage axis x and a spanwise axis y. The wing procuring a lift along an axis z. The wing element having a skin forming the leading edge slat, a spar linked to the skin and a stiffening structure linked on the leading edge side to the spar and to the skin. The stiffening structure being formed from a formed sheet metal having a plurality of bosses distributed according to the length of the leading edge. The bosses extending between the spar and the inner face of the skin.
    Type: Grant
    Filed: December 26, 2019
    Date of Patent: March 1, 2022
    Assignee: DAHER AEROSPACE
    Inventors: Pascal Hermel, Luc Gautrand, François Bauvir, Arnaud Cazelles, David Clech
  • LEADING EDGE SLAT WITH OPTIMIZED STRUCTURE
    Publication number: 20200207458
    Abstract: A leading edge slat of a wing element of an aircraft. The aircraft defining a mark including a main fuselage axis x and a spanwise axis y. The wing procuring a lift along an axis z. The wing element having a skin forming the leading edge slat, a spar linked to the skin and a stiffening structure linked on the leading edge side to the spar and to the skin. The stiffening structure being formed from a formed sheet metal having a plurality of bosses distributed according to the length of the leading edge. The bosses extending between the spar and the inner face of the skin.
    Type: Application
    Filed: December 26, 2019
    Publication date: July 2, 2020
    Inventors: PASCAL HERMEL, LUC GAUTRAND, FRANÇOIS BAUVIR, ARNAUD CAZELLES, DAVID CLECH