Patents by Inventor Brian Nelson Cox

Brian Nelson Cox 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: 7811297
    Abstract: An actuable truss with ordered or disordered planar or strut elements or pore walls may be seeded with tissue cells, wherein application of a magnetic field may result in mechanical strain on the cells and increased fluid flow in and out of the truss structure. Modified polymers, such as ?-Fe2O3/PLGA, may be used to form actuable scaffolds suitable for tissue engineering. It is also disclosed a device with a trap-door that may be remotely actuated by applying a magnetic field. Such a device may be employed to deliver and control the release of other micro-devices or materials such as drugs to a specific location inside the body of a human or an animal.
    Type: Grant
    Filed: December 8, 2006
    Date of Patent: October 12, 2010
    Assignee: Teledyne Scientific & Imaging, LLC
    Inventors: Brian Nelson Cox, Julia Jeannine Mack
  • Patent number: 7281688
    Abstract: A self-transpiring hot skin for a hypersonic or reusable space vehicle that can provide protection to the vehicle during short periods of abnormally high heat flux (either planned in the flight profile or an off-nominal event). The hot skin includes a ceramic composite structure having an internal cavity that is coupled either to the insulating layer or directly to the support structure of the hypersonic vehicle. The internal cavity includes a material system that vaporizes, sublimes or decomposes into a gas when the temperature exceeds the upper temperature capability of the composite material. The gas transpires through the outer layer of the composite material to provide cooling to the outer layer below the upper temperature capability. Cooling may occur both by conduction of heat from the composite material to the transpiring gas and by the interaction of the transpiring gas with the boundary layer of hypersonic flow over the outer surface, leading to a reduction of the heat flux entering the surface.
    Type: Grant
    Filed: April 27, 2006
    Date of Patent: October 16, 2007
    Assignee: The Boeing Company
    Inventors: Brian Nelson Cox, Janet B. Davis, Julia Mack, David Bruce Marshall, Peter E. Morgan, Olivier H. Sudre