Patents by Inventor Thierry Pichon

Thierry Pichon 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: 11035321
    Abstract: A nozzle presents a longitudinal axis, includes both a combustion chamber made of metal material and presenting a downstream end, and a diverging portion made of composite material formed by a wall of conical shape extending between an upstream and a downstream end. The upstream end of the composite material diverging portion is connected to the downstream end of the combustion chamber. The nozzle further includes an annular mount made of metal material including a first portion secured to the combustion chamber and a second portion extending beyond the downstream end of the combustion chamber along the longitudinal axis. The upstream end of the composite material diverging portion is fastened to the second portion of the annular mount by a plurality of fastener members, each including a fastener bolt, each fastener bolt passing through the conically-shaped wall of the composite material diverging portion near the upstream end of the wall.
    Type: Grant
    Filed: June 28, 2017
    Date of Patent: June 15, 2021
    Assignee: ARIANEGROUP SAS
    Inventors: Thierry Pichon, Xavier Zorrilla, Ivan Herraiz, Laurent Longueville
  • Publication number: 20190203662
    Abstract: A nozzle presents a longitudinal axis, includes both a combustion chamber made of metal material and presenting a downstream end, and a diverging portion made of composite material formed by a wall of conical shape extending between an upstream and a downstream end. The upstream end of the composite material diverging portion is connected to the downstream end of the combustion chamber. The nozzle further includes an annular mount made of metal material including a first portion secured to the combustion chamber and a second portion extending beyond the downstream end of the combustion chamber along the longitudinal axis. The upstream end of the composite material diverging portion is fastened to the second portion of the annular mount by a plurality of fastener members, each including a fastener bolt, each fastener bolt passing through the conically-shaped wall of the composite material diverging portion near the upstream end of the wall.
    Type: Application
    Filed: June 28, 2017
    Publication date: July 4, 2019
    Inventors: Thierry PICHON, Xavier ZORRILLA, Ivan HERRAIZ, Laurent LONGUEVILLE
  • Patent number: 6482485
    Abstract: The piece made of composite material comprises a plate and a plurality of stiffeners integrally formed with the plate. A metal wall is fixed to the edges of the stiffeners and is provided with passages for circulating the fluid. The plate exposed to the heat flux radiates towards the metal wall through the gaps between the stiffeners, and it also performs the structural function. The invention can be used with structures that are exposed to very high heat flux: the walls of jet combustion chambers, the walls of space plane vehicles, the walls of nuclear fusion reactors.
    Type: Grant
    Filed: August 12, 1999
    Date of Patent: November 19, 2002
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation-S.N.E.C.M.A.
    Inventor: Thierry Pichon