Patents by Inventor Pascal Burek

Pascal Burek 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: 10239241
    Abstract: A compacting and injection mold for a fiber preform is for use in fabricating a turbine engine guide vane out of composite material. The mold includes a shell forming a trough that is to receive the fiber preform and that is closed in leaktight manner by bottom and top covers, compacting blocks arranged inside the trough each having a surface pressing normally against a surface of the fiber preform that is to be compacted, and closure blocks arranged inside the trough. Each closure block has a surface pressing normally against a surface of a compacting block and does not have a surface in contact with the fiber preform.
    Type: Grant
    Filed: August 30, 2017
    Date of Patent: March 26, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Romain Plante, Lise Lacroix, Olivier Patrigeon, Jean-Pierre Cauchois, Pascal Burek
  • Patent number: 9868235
    Abstract: A compacting and injection mold for a fiber preform is for use in fabricating a turbine engine guide vane out of composite material. The mold includes a shell forming a trough that is to receive the fiber preform and that is closed in leaktight manner by bottom and top covers, compacting blocks arranged inside the trough each having a surface pressing normally against a surface of the fiber preform that is to be compacted, and closure blocks arranged inside the trough. Each closure block has a surface pressing normally against a surface of a compacting block and does not have a surface in contact with the fiber preform.
    Type: Grant
    Filed: May 3, 2012
    Date of Patent: January 16, 2018
    Assignee: SNECMA
    Inventors: Romain Plante, Lise Lacroix, Olivier Patrigeon, Jean-Pierre Cauchois, Pascal Burek
  • Publication number: 20170361512
    Abstract: A compacting and injection mold for a fiber preform is for use in fabricating a turbine engine guide vane out of composite material. The mold includes a shell forming a trough that is to receive the fiber preform and that is closed in leaktight manner by bottom and top covers, compacting blocks arranged inside the trough each having a surface pressing normally against a surface of the fiber preform that is to be compacted, and closure blocks arranged inside the trough. Each closure block has a surface pressing normally against a surface of a compacting block and does not have a surface in contact with the fiber preform.
    Type: Application
    Filed: August 30, 2017
    Publication date: December 21, 2017
    Applicant: SNECMA
    Inventors: Romain PLANTE, Lise Lacroix, Olivier Patrigeon, Jean-Pierre Cauchois, Pascal Burek