Patents by Inventor Curtis S. Copeland

Curtis S. Copeland 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: 11512668
    Abstract: A rocket motor has an electrically operated propellant initiator for a propellant grain that includes an electrode arrangement configured to concentrate an electric field at an ignition electrode for igniting an electrically operated propellant. The rocket motor includes a combustion chamber containing at least one propellant grain and an electrically operated propellant initiator operatively coupled to the propellant grain to initiate combustion of the propellant grain. The electrically operated propellant initiator includes the electrically operated propellant and at least one pair of electrodes configured to ignite the electrically operated propellant. The pair of electrodes includes a ground plane electrode and an ignition electrode. When an electrical input is applied to the electrically operated propellant initiator, the electric field is concentrated at the ignition electrode to ignite the electrically operated propellant at the location where the ignition electrode is arranged.
    Type: Grant
    Filed: November 28, 2020
    Date of Patent: November 29, 2022
    Assignee: Raytheon Company
    Inventors: Frederick B. Koehler, Jacob A. Pinello-Benavides, Curtis S. Copeland, Isaiah M. McNeil, Paul Kadlec, Lauren E. Brunacini, Mark T. Langhenry
  • Publication number: 20220170432
    Abstract: A rocket motor has an electrically operated propellant initiator for a propellant grain that includes an electrode arrangement configured to concentrate an electric field at an ignition electrode for igniting an electrically operated propellant. The rocket motor includes a combustion chamber containing at least one propellant grain and an electrically operated propellant initiator operatively coupled to the propellant grain to initiate combustion of the propellant grain. The electrically operated propellant initiator includes the electrically operated propellant and at least one pair of electrodes configured to ignite the electrically operated propellant. The pair of electrodes includes a ground plane electrode and an ignition electrode. When an electrical input is applied to the electrically operated propellant initiator, the electric field is concentrated at the ignition electrode to ignite the electrically operated propellant at the location where the ignition electrode is arranged.
    Type: Application
    Filed: November 28, 2020
    Publication date: June 2, 2022
    Inventors: Frederick B. Koehler, Jacob A. Pinello-Benavides, Curtis S. Copeland, Isaiah M. McNeil, Paul Kadlec, Lauren E. Brunacini, Mark T. Langhenry
  • Patent number: 7352270
    Abstract: A magnetic assembly including a printed circuit board and a core made from magnetically permeable material positioned on the printed circuit board. Plated through holes are formed in the printed circuit board, a first plated through hole on a first side of the core, a second plated through on a second side of the core and third plated though hole on the first side of the core. A winding lead has a first leg soldered in the first plated through hole and a second leg soldered in the second plated through hole, the winding lead being a discrete electrical conductor separate from the printed circuit board. A conductive trace is formed in the printed circuit board, the conductive trace electrically connected the second plated through hole and the third plated through hole.
    Type: Grant
    Filed: October 27, 2006
    Date of Patent: April 1, 2008
    Assignee: ITT Manufacturing Enterprises, Inc.
    Inventor: Curtis S. Copeland