Patents by Inventor Pascal Tatiossian

Pascal Tatiossian 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: 8662828
    Abstract: A high pressure turbine of a turbomachine such as a turbojet, in which a control box of radial clearances of rotating blades are provided. An annular element including a determined flexibility has one end fixed to an annular support and the other end supported by a simple axial bearing with a given pressure on the upstream side of the control box. Thus, disturbing vibration loads are prevented at the attachment points of the control box with the external casing of turbines, thereby also eliminating the risk of cracks occurring.
    Type: Grant
    Filed: May 25, 2009
    Date of Patent: March 4, 2014
    Assignee: SNECMA
    Inventors: Alain Dominique Gendraud, Delphine Roussin-Leroux, Jean-Luc Le Strat, Pascal Tatiossian
  • Publication number: 20110076135
    Abstract: A high pressure turbine of a turbomachine such as a turbojet, in which a control box of radial clearances of rotating blades are provided. An annular element including a determined flexibility has one end fixed to an annular support and the other end supported by a simple axial bearing with a given pressure on the upstream side of the control box. Thus, disturbing vibration loads are prevented at the attachment points of the control box with the external casing of turbines, thereby also eliminating the risk of cracks occurring.
    Type: Application
    Filed: May 25, 2009
    Publication date: March 31, 2011
    Applicant: SNECMA
    Inventors: Alain Dominique Gendraud, Delphine Leroux, Jean-Luc Le Strat, Pascal Tatiossian