Patents by Inventor Matthew D. Diehl

Matthew D. Diehl 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: 9851188
    Abstract: A vessel, such as a rocket motor tube, comprised of an insert, and a joint that allows the insert to decouple from the vessel to relieve pressure when subjected to excessive temperatures and/or a predetermined temperature or temperature range.
    Type: Grant
    Filed: November 11, 2013
    Date of Patent: December 26, 2017
    Assignee: General Dynamics-OTS, Inc.
    Inventors: Matthew D. Diehl, Eric Michael Schneck, Gregory Norman Bogan
  • Patent number: 8919254
    Abstract: A vessel, such as a rocket motor tube, comprised of an insert, and a joint that allows the insert to decouple from the vessel to relieve pressure when subjected to excessive temperatures and/or a predetermined temperature or temperature range.
    Type: Grant
    Filed: November 11, 2013
    Date of Patent: December 30, 2014
    Assignee: General Dynamics-OTS, Inc.
    Inventors: Matthew D. Diehl, Eric Michael Schneck, Gregory Norman Bogan
  • Publication number: 20140306443
    Abstract: A vessel, such as a rocket motor tube, comprised of an insert, and a joint that allows the insert to decouple from the vessel to relieve pressure when subjected to excessive temperatures and/or a predetermined temperature or temperature range.
    Type: Application
    Filed: November 11, 2013
    Publication date: October 16, 2014
    Applicant: General Dynamics-OTS, Inc.
    Inventors: Matthew D. Diehl, Eric Michael Schneck, Gregory Norman Bogan
  • Publication number: 20140284913
    Abstract: A vessel, such as a rocket motor tube, comprised of an insert, and a joint that allows the insert to decouple from the vessel to relieve pressure when subjected to excessive temperatures and/or a predetermined temperature or temperature range.
    Type: Application
    Filed: November 11, 2013
    Publication date: September 25, 2014
    Applicant: General Dynamics-OTS, Inc.
    Inventors: Matthew D. Diehl, Eric Michael Schneck, Gregory Norman Bogan
  • Patent number: 8807009
    Abstract: A capacitive reactive armor assembly for shielding a vehicle is disclosed herein. The capacitive reactive armor includes, but is not limited to, a first flyer plate, a second flyer plate, and a capacitor positioned between the first flyer plate and the second flyer plate. The capacitor is configured to store an electric charge and to explosively short circuit when the capacitor is penetrated while the capacitor is electrically charged. The explosive release of energy from the capacitor pushes the first and second flyer plates apart interfering with the penetration of a shaped charge jet or ballistic penetrator.
    Type: Grant
    Filed: October 6, 2011
    Date of Patent: August 19, 2014
    Assignee: General Dynamics—OTS, Inc.
    Inventor: Matthew D. Diehl
  • Patent number: 8578855
    Abstract: A vessel, such as a rocket motor tube, comprised of an insert, and a joint that allows the insert to decouple from the vessel to relieve pressure when subjected to excessive temperatures and/or a predetermined temperature or temperature range.
    Type: Grant
    Filed: August 21, 2009
    Date of Patent: November 12, 2013
    Assignee: General Dynamics Armament and Technical Products, Inc.
    Inventors: Matthew D. Diehl, Eric Michael Schneck, Gregory Norman Bogan
  • Publication number: 20130087038
    Abstract: A capacitive reactive armor assembly for shielding a vehicle is disclosed herein. The capacitive reactive armor includes, but is not limited to, a first flyer plate, a second flyer plate, and a capacitor positioned between the first flyer plate and the second flyer plate. The capacitor is configured to store an electric charge and to explosively short circuit when the capacitor is penetrated while the capacitor is electrically charged. The explosive release of energy from the capacitor pushes the first and second flyer plates apart interfering with the penetration of a shaped charge jet or ballistic penetrator.
    Type: Application
    Filed: October 6, 2011
    Publication date: April 11, 2013
    Applicant: GENERAL DYNAMICS ARMAMENT AND TECHNICAL PRODUCTS, INC.
    Inventor: Matthew D. Diehl
  • Publication number: 20110044751
    Abstract: A vessel, such as a rocket motor tube, comprised of an insert, and a joint that allows the insert to decouple from the vessel to relieve pressure when subjected to excessive temperatures and/or a predetermined temperature or temperature range.
    Type: Application
    Filed: August 21, 2009
    Publication date: February 24, 2011
    Applicant: General Dynamics Armament and Technical Products, Inc.
    Inventors: Matthew D. DIEHL, Eric Michael Schneck, Gregory Norman Bogan
  • Patent number: 7040780
    Abstract: A non-lethal laser weapon having a base to which a number of lasers are mounted. The lasers include a first laser oriented to project a first laser beam in a first direction, and a second laser oriented to project a second laser beam generally in the first direction. The first laser beam and the second laser beam overlap at a first distance from the base, to thereby form separate first and second first-order illumination zones before the first distance, and a first second-order illumination zone beyond the first distance. Additional lasers may be included in one-, two-, and three-dimensional patterns to create additional illumination zones.
    Type: Grant
    Filed: February 20, 2004
    Date of Patent: May 9, 2006
    Assignee: General Dynamics Armament And Technical products
    Inventor: Matthew D. Diehl
  • Patent number: 5586579
    Abstract: To provide pressure relief in a fluid line of a fluidic circuit, the ball element of a shutoff valve incorporates a tube that is aligned with a pair of valve ports when the ball is in the closed valve position. A miniature check valve, positioned in the tube, operates, depending on its orientation, to check fluid flow through the tube between the valve ports in one direction and to vent fluid through the tube in the opposite direction in response to excessive fluid pressure. In an alternative embodiment, a pair of tubes are incorporated into the ball valve element, with the check valves therein oriented in opposed directions to provide bidirectional pressure relief between the valve ports.
    Type: Grant
    Filed: November 15, 1995
    Date of Patent: December 24, 1996
    Assignee: Martin Marietta Corporation
    Inventor: Matthew D. Diehl