Patents by Inventor Mario Dipreta

Mario Dipreta 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: 10434687
    Abstract: A composite piece tool used to create a composite piece. The tool includes a substrate having a substrate surface, walls disposed on the substrate and extending from the substrate surface in a thickness direction of the composite piece to define opposite locations of longitudinal composite piece ends and composite piece sides, a tooling surface disposed to occupy an entirety of a space delimited by the walls and on which the composite piece formed and a servo controller coupled to the tooling surface and configured to move the tooling surface upwardly and downwardly relative to the substrate surface and walls to form the composite piece.
    Type: Grant
    Filed: December 10, 2015
    Date of Patent: October 8, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Joshua A. Breon, Mario Dipreta
  • Patent number: 10406763
    Abstract: A blade element is provided and includes courses of bias plies continuously machine-wrapped about leading and trailing edges at an angle relative to a long axis of the blade axis and unidirectional plies interwoven in parallel with the long axis between adjacent courses of the bias plies on upper and lower surfaces to promote respective tangential geometries of the bias plies at the leading and trailing edges, the unidirectional plies not extending into the leading and trailing edges.
    Type: Grant
    Filed: August 10, 2015
    Date of Patent: September 10, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Joshua A. Breon, Mario Dipreta
  • Publication number: 20170282413
    Abstract: A composite piece tool used to create a composite piece. The tool includes a substrate having a substrate surface, walls disposed on the substrate and extending from the substrate surface in a thickness direction of the composite piece to define opposite locations of longitudinal composite piece ends and composite piece sides, a tooling surface disposed to occupy an entirety of a space delimited by the walls and on which the composite piece formed and a servo controller coupled to the tooling surface and configured to move the tooling surface upwardly and downwardly relative to the substrate surface and walls to form the composite piece.
    Type: Application
    Filed: December 10, 2015
    Publication date: October 5, 2017
    Inventors: Joshua A. Breon, Mario Dipreta
  • Publication number: 20170217107
    Abstract: A blade element is provided and includes courses of bias plies continuously machine-wrapped about leading and trailing edges at an angle relative to a long axis of the blade axis and unidirectional plies interwoven in parallel with the long axis between adjacent courses of the bias plies on upper and lower surfaces to promote respective tangential geometries of the bias plies at the leading and trailing edges, the unidirectional plies not extending into the leading and trailing edges.
    Type: Application
    Filed: August 10, 2015
    Publication date: August 3, 2017
    Inventors: Joshua A. Breon, Mario Dipreta