Patents by Inventor Stephane Bianco

Stephane Bianco 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: 8656593
    Abstract: A method for assembling a part of a metal material and a part of a composite material, the junction of the two parts being achieved through a fastener having a substantially constant section and received in a first hole formed in the part of a metal material and a second hole formed in the part of a composite material. According to the disclosed embodiments and before assembling the aforementioned parts, the method includes: an expansion step for generating a field of compression stresses at the periphery of the first hole and locally in the material constituting the part of a metal material using an expansion tool; a single boring step for making the first hole and the second hole with a diameter Øfinal substantially larger than the diameter of the fastener in order to leave a gap between the inner walls of the holes and the outer surface of the fastener; and an assembling step for placing the fastener inside the holes for maintaining together the metal part and the composite part.
    Type: Grant
    Filed: May 6, 2008
    Date of Patent: February 25, 2014
    Assignee: Airbus Operations (S.A.S.)
    Inventors: Nicolas Dantou, Stephane Bianco, Christian Godenzi
  • Patent number: 8458885
    Abstract: Process for assembling a first part made of metal material and a second part made of composite material, by an attachment element, which includes: —pre-piercing the parts to form a recess with a diameter D1 in the first and the second parts; —installing an insert having a variable diameter in the direction of the thickness of the parts in the recess, the insert including a main hollow body and at least one flange designed to rest at least partially against the outside surface of a part, the insert being designed to accommodate the attachment element; generating residual compression constraints by radial expansion on the inner wall of the insert by an expansion tool having an outside diameter that works with the inside diameter of the insert in at least one zone of the two parts along the circumference of the insert; —boring the recess of the main body wider so that the insert has a final inside diameter that is significantly greater than the outside diameter of the attachment element to allow play between the
    Type: Grant
    Filed: March 18, 2009
    Date of Patent: June 11, 2013
    Assignee: Airbus Operations (S.A.S.)
    Inventors: Stephane Bianco, Laurent Pinto
  • Publication number: 20110119891
    Abstract: Process for assembling a first part made of metal material and a second part made of composite material, by an attachment element, which includes: —pre-piercing the parts to form a recess with a diameter D1in the first and the second parts; —installing an insert having a variable diameter in the direction of the thickness of the parts in the recess, the insert including a main hollow body and at least one flange designed to rest at least partially against the outside surface of a part, the insert being designed to accommodate the attachment element; generating residual compression constraints by radial expansion on the inner wall of the insert by an expansion tool having an outside diameter that works with the inside diameter of the insert in at least one zone of the two parts along the circumference of the insert; —boring the recess of the main body wider so that the insert has a final inside diameter that is significantly greater than the outside diameter of the attachment element to allow play between the
    Type: Application
    Filed: March 18, 2009
    Publication date: May 26, 2011
    Applicant: AIRBUS OPERATIONS (S.A.S.)
    Inventors: Stephane Bianco, Laurent Pinto
  • Publication number: 20100287776
    Abstract: A method for assembling a part of a metal material and a part of a composite material, the junction of the two parts being achieved through a fastener having a substantially constant section and received in a first hole formed in the part of a metal material and a second hole formed in the part of a composite material. According to the disclosed embodiments and before assembling the aforementioned parts, the method includes: an expansion step for generating a field of compression stresses at the periphery of the first hole and locally in the material constituting the part of a metal material using an expansion tool; a single boring step for making the first hole and the second hole with a diameter Øfinal substantially larger than the diameter of the fastener in order to leave a gap between the inner walls of the holes and the outer surface of the fastener; and an assembling step for placing the fastener inside the holes for maintaining together the metal part and the composite part.
    Type: Application
    Filed: May 6, 2008
    Publication date: November 18, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Nicolas Dantou, Stephane Bianco, Christian Godenzi
  • Patent number: 7739059
    Abstract: A method, system, and computer program product for calculating the residual stress equilibrium of two elastoplastic cylinders coldworked by expansion to obtain interference fit. The deformation state due to an internal expansion load applied to an inner cylinder that will result in interference of the inner cylinder with the outer cylinder can be calculated. The deformation state due to an unloading of the internal expansion load that will result in assembly of the inner cylinder and the outer cylinder can be calculated. The residual stresses, residual displacement and residual strains in the inner cylinder and the outer cylinder, whether they are eventually interference fitted or not, can all be calculated and recorded.
    Type: Grant
    Filed: July 16, 2007
    Date of Patent: June 15, 2010
    Assignee: Airbus France
    Inventors: Stephane Bianco, Romain Canivenc, Marc Sartor
  • Publication number: 20090024335
    Abstract: A method, system, and computer program product for calculating the residual stress equilibrium of two elastoplastic cylinders coldworked by expansion to obtain interference fit. The deformation state due to an internal expansion load applied to an inner cylinder that will result in interference of the inner cylinder with the outer cylinder can be calculated. The deformation state due to an unloading of the internal expansion load that will result in assembly of the inner cylinder and the outer cylinder can be calculated. The residual stresses, residual displacement and residual strains in the inner cylinder and the outer cylinder, whether they are eventually interference fitted or not, can all be calculated and recorded.
    Type: Application
    Filed: July 16, 2007
    Publication date: January 22, 2009
    Applicant: Airbus France
    Inventors: Stephane Bianco, Romain Canivenc, Marc Sartor