Patents by Inventor Gregory M. Richards

Gregory M. Richards 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).

  • Publication number: 20240111707
    Abstract: An apparatus is provided, comprising a plurality of memory devices and a buffering device that permits memory devices with a variety of physical dimensions and memory formats to be used in an industry-standard memory module format. The buffering device includes memory interface circuitry and at least one first-in first-out (FIFO) or multiplexer circuit. The apparatus further comprises a parallel bus connecting the buffering device to the plurality of memory devices. The parallel bus includes a plurality of independent control lines, each coupling the memory interface circuitry to a corresponding subset of a plurality of first subsets of the plurality of memory devices. The parallel bus further includes a plurality of independent data channels, each coupling the at least one FIFO circuit or multiplexer circuit to a corresponding subset of a plurality of second subsets of the plurality of memory devices.
    Type: Application
    Filed: October 9, 2023
    Publication date: April 4, 2024
    Inventors: Thomas H. Kinsley, George E. Pax, Timothy M. Hollis, Yogesh Sharma, Randon K. Richards, Chan H. Yoo, Gregory A. King, Eric J. Stave
  • Patent number: 10442521
    Abstract: An apparatus, having: a fuselage body section (180) configured to be secured to an aircraft fuselage (16); a pivot column (310) protruding from the fuselage body section; and a center wing section (214) configured to be secured to a center wing panel of a trifold wing (200). The fuselage body section and the center wing section are configured to cooperate with each other to rotate the center wing section relative to the fuselage body section from a stowed position (250) to a deployed position (302). The pivot column comprises a column feature (240) configured to engage with tip features (236) of the trifold wing to hold the trifold wing in a folded configuration when the trifold wing is in the stowed position and to disengage from the tip features as the trifold wing rotates to the deployed position, thereby freeing the trifold wing to unfold.
    Type: Grant
    Filed: December 22, 2016
    Date of Patent: October 15, 2019
    Assignee: LOCKHEED MARTIN CORPORATION
    Inventors: Steven J. Ellzey, James C. Copp, Gregory M. Richards
  • Patent number: 7040210
    Abstract: An apparatus includes a restraint for restraining a first control surface in a stowed configuration and a severing mechanism for parting the restraint to allow the first control surface to move into an operational configuration. A vehicle includes a body, a first control surface rotatably mounted to the body, and a restraint attached to the first control surface for restraining the first control surface in a stowed configuration. The vehicle further includes a severing mechanism for parting the restraint to allow the first control surface to move into an operational configuration. A method includes attaching a restraint to the control surface to restrain the control surface in a stowed configuration and cutting the restraint to allow the control surface to move to an operational configuration.
    Type: Grant
    Filed: February 18, 2003
    Date of Patent: May 9, 2006
    Assignee: Lockheed Martin Corporation
    Inventor: Gregory M. Richards
  • Publication number: 20040159227
    Abstract: An apparatus includes a restraint for restraining a first control surface in a stowed configuration and a severing mechanism for parting the restraint to allow the first control surface to move into an operational configuration. A vehicle includes a body, a first control surface rotatably mounted to the body, and a restraint attached to the first control surface for restraining the first control surface in a stowed configuration. The vehicle further includes a severing mechanism for parting the restraint to allow the first control surface to move into an operational configuration. A method includes attaching a restraint to the control surface to restrain the control surface in a stowed configuration and cutting the restraint to allow the control surface to move to an operational configuration.
    Type: Application
    Filed: February 18, 2003
    Publication date: August 19, 2004
    Applicant: LOCKHEED MARTIN CORPORATION
    Inventor: Gregory M. Richards