Patents by Inventor Russell Chan

Russell Chan 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: 20070239418
    Abstract: Systems and methods for parallel, discrete, simulations include functional capabilities to incorporate one or more human operators or actors into the simulation process. Such individuals can be presented situations where one or more decisions are necessary with respect to ongoing events. Entered decisions are incorporated into simulated events and activities being simulated. These in turn influence the behavior of those entities and also initiate the occurrence of other time-based processes. An architecture artifact or product can be automatically created or updated by recording how a sequence of events took place. The creation of sections of the DoDAF OV-6C Operational Event Trace architectural diagram, for the executable architecture model, can be automatically performed to dynamically provide event traces in response to a live exercise.
    Type: Application
    Filed: March 23, 2007
    Publication date: October 11, 2007
    Inventors: Gregory Harrison, Salaheddine Saidi, Russell Chan, Ann McCauslin, Howard Kern, Jeffrey Coffin, David Benjamin, Lawrence Elliott, Christopher Young, Stephen Peckham, Michael Stewart, Mark Barbustiak
  • Patent number: 6206327
    Abstract: A mission configurable modular satellite bus structure composed of several scalable modules, including a propulsion module and one or more stackable space modules, each using standard subsystems or components with common structures and/or interfaces, that can be processed in parallel to minimize nonrecurring and recurring costs. Each stackable space module includes a generally cylindrical central hub having a plurality of radial rib panels extending outwardly therefrom to form a plurality of bays for containing subsystem equipment. The hub includes a hollow center sized to receive the propulsion module as a fully assembled unit. The radial rib panels carry the primary structural load of the spacecraft. Also provided are removable side access panels that form enclosures for the bays. The side access panels include equipment mounts along an inside surface for mounting the subsystem components and radiators along an outside surface to provide thermal cooling for the mounted subsystem equipment.
    Type: Grant
    Filed: March 31, 1999
    Date of Patent: March 27, 2001
    Assignee: Lockheed Martin Corporation
    Inventors: Steven L. Benedetti, Timothy S. Cahill, Russell Chan, Kris D. Forrest