Patents by Inventor André Rolland

André Rolland 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: 7080540
    Abstract: This invention is a device for forming heat exchange elements with corrugated heat exchange surfaces, more particularly inserts, made of a sheet in a formable material, such as metal, between two surfaces, each thus presenting a corrugated profile. This device is of the type comprising at least two plates whose opposing faces present the said corrugated profiles and which are offset from each other so as to define between them a space to take the sheet to be formed (2). The device is distinguished by the fact that the profiles (A and B) are configured in such a way that their displacement in the direction of the thickness of the insert is constant along the corrugations in the space between the profiles. The invention can be used for the production of inserts.
    Type: Grant
    Filed: February 20, 2003
    Date of Patent: July 25, 2006
    Assignee: Societe d'Etudes et de Constructions Aero-Navales
    Inventors: Daniel Taillepied, Catherine Fourmont, André Rolland
  • Publication number: 20040055355
    Abstract: This invention is a device for forming heat exchange elements with corrugated heat exchange surfaces, more particularly inserts, made of a sheet in a formable material, such as metal, between two surfaces, each thus presenting a corrugated profile.
    Type: Application
    Filed: February 20, 2003
    Publication date: March 25, 2004
    Inventors: Daniel Taillepied, Catherine Fourmont, Andre Rolland
  • Patent number: 5826332
    Abstract: A method of manufacturing a hollow machine blade consisting of two skins ining an internal cavity and interconnected by stiffeners comprises:forging and machining the primary components of the blade, including forming a reserve of material in localized regions of the inner faces of the skins, trunnion forming elements at the ends of the components, and locating holes in the components;deposition of diffusion barriers involving application of a mask, cutting the mask to a predetermined pattern using a special-purpose tool, peeling away portions of the mask, deposition of a coating product, peeling away the remainder of the mask, prefiring treatment, cleaning and checking;assembly of the primary components followed by isostatic-pressure diffusion welding; andsubjecting the assembly to inflation under gas pressure and superplastic forming in a mould in order to shape the skins and form the interconnecting stiffeners, including the steps of cold-debonding the primary components, causing flow of the material reser
    Type: Grant
    Filed: September 26, 1996
    Date of Patent: October 27, 1998
    Assignees: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation, Societe Dassault Aviation
    Inventors: Mathieu Philippe Albert Bichon, Xavier Gerard Andre Coudray, Alex Pierre Deblois, Christophe Nicolas Marie Joseph Huon De Kermadec, Jean-Fran.cedilla.ois Georges Julien Lacuisse, Bruno Andre Rolland