Patents by Inventor Sebastien Quets

Sebastien Quets 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: 6929035
    Abstract: Thin walled compartmented tubular structure and its manufacturing process. The elbow or T-shaped structure, includes an external wall (14)and continuous internal walls (22) made in one piece. This therefore materializes, between the inlet (10) and each outlet (12) of the structure, at least one continuous passage to direct a fluid circulating inside it. The structure according to the invention is manufactured by diffusion welding and superplastic forming, from titanium alloy sheets. One application is for aircraft de-icing circuits.
    Type: Grant
    Filed: June 12, 2002
    Date of Patent: August 16, 2005
    Assignee: Sonaca, S.A.
    Inventors: Stéphane Debaisieux, Dimitri Gueuning, Sébastien Quets
  • Patent number: 6739029
    Abstract: A structure (10) in the shape of an aerodynamic panel in which adjacent cells (20a, 20b) are formed by placing a stack of three metal plates in a mold. After diffusion welding of the plates at the required locations, a first variable pressure is applied in a first series of cells (20a) formed between the outer plate and the intermediate plate and a second independent pressure approximately constant and lower than the first is applied in the other cells (20b) and on the inner face of the stack. Thus, this partially forms the cells and shapes the structure in contact with a complementary surface of the mold. The final conformation of the cells and the structure is obtained by applying a second pressure cycle in the cells and on the inner face of the stack.
    Type: Grant
    Filed: January 10, 2003
    Date of Patent: May 25, 2004
    Assignee: Sonaca S.A.
    Inventors: Stéphane Debaisieux, Christian Overbergh, Sébastien Quets
  • Publication number: 20030136815
    Abstract: A structure (10) in the shape of an aerodynamic panel in which adjacent cells (20a, 20b) are formed by placing a stack of three metal plates in a mould. After diffusion welding of the plates at the required locations, a first variable pressure is applied in a first series of cells (20a) formed between the outer plate and the intermediate plate and a second independent pressure approximately constant and lower than the first is applied in the other cells (20b) and on the inner face of the stack. Thus, this partially forms the cells and shapes the structure in contact with a complementary surface of the mould. The final conformation of the cells and the structure is obtained by applying a second pressure cycle in the cells and on the inner face of the stack.
    Type: Application
    Filed: January 10, 2003
    Publication date: July 24, 2003
    Applicant: Sonaca S.A.
    Inventors: Stephane Debaisieux, Christian Overbergh, Sebastien Quets
  • Publication number: 20020195155
    Abstract: Thin walled compartmented tubular structure and its manufacturing process.
    Type: Application
    Filed: June 12, 2002
    Publication date: December 26, 2002
    Applicant: Sonaca S.A.
    Inventors: Stephane Debaisieux, Dimitri Gueuning, Sebastien Quets