Patents by Inventor James O. Gibson

James O. Gibson 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: 5382309
    Abstract: Improved fiber reinforced composites having near zero coefficients of thermal expansion are described. The improved composites include reinforcing fibers and matrix material in which gap structures which exist within the composite are filled with a bonding agent. The reinforcing fibers can be unidirectionally, bidirectionally or multidirectionally oriented within the matrix material and articles fabricated from the improved composite have reduced coefficients of thermal expansion in directions transverse to the orientations of the fibers. This improvement makes these improved composites useful for fabricating high energy laser mirror substrates.
    Type: Grant
    Filed: May 13, 1993
    Date of Patent: January 17, 1995
    Assignee: Hughes Aircraft Company
    Inventors: Robert W. Seibold, Bruce W. Buller, James O. Gibson
  • Patent number: 5229196
    Abstract: Improved fiber reinforced composites having near zero coefficients of thermal expansion are described. The improved composites include reinforcing fibers and matrix material in which gap structures which exist within the composite are filled with a bonding agent. The reinforcing fibers can be unidirectionally, bidirectionally or multidirectionally oriented within the matrix material and articles fabricated from the improved composite have reduced coefficients of thermal expansion in directions transverse to the orientations of the fibers. This improvement makes these improved composites useful for fabricating high energy laser mirror substrates.
    Type: Grant
    Filed: September 27, 1991
    Date of Patent: July 20, 1993
    Assignee: Hughes Aircraft Company
    Inventors: Robert W. Seibold, Bruce W. Buller, James O. Gibson
  • Patent number: 4805181
    Abstract: A ceramic pump cavity structure for use in solid state lasers wherein the pump cavity comprises sintered alumina having grain sizes of between about 0.3 to 0.5 microns. Sintered alumina pump cavities having grain sizes within this range provide desirable diffuse reflectivity comparable to barium sulfate while at the same time providing a structurally strong cavity which is resistant to cracking and breakage. Combinations of the alumina oxide pump cavity with parasitic light absorbers such as samarium oxide are also disclosed.
    Type: Grant
    Filed: March 21, 1988
    Date of Patent: February 14, 1989
    Assignee: Hughes Aircraft Company
    Inventors: James O. Gibson, Victor C. Gearhart, Steven E. Birrell, Gabriele M. Hawrylow
  • Patent number: 4802186
    Abstract: A ceramic pump cavity structure for use in solid state lasers wherein the pump cavity comprises sintered alumina having grain sizes of between about 0.3 to 0.5 microns. Sintered alumina pump cavities having grain sizes within this range provide desirable diffuse reflectivity comparable to barium sulfate while at the same time providing a structurally strong cavity which is resistant to cracking and breakage. Combinations of the alumina pump cavity with parasitic light absorbers such as samarium oxide are also disclosed.
    Type: Grant
    Filed: July 6, 1987
    Date of Patent: January 31, 1989
    Assignee: Hughes Aircraft Company
    Inventors: James O. Gibson, Victor C. Gearhart, Steven E. Birrell, Gabriele M. Hawrylow
  • Patent number: 4784842
    Abstract: Compositions of matter and method of use of compositions consisting essentially of a mixture, in effective amounts, of (a) a terpene or mixtures thereof, and (b) vitamin E. These compositions are used for treatment of cuts, burns and abrasions of the skin in mammals, particularly humans, to facilitate healing and reduce swelling, bleeding and pain, by applying the mixture to the affected external area of the skin, as by swabbing with an applicator. Alternatively, the treatment mixture can be pressurized by means of a carrier, such as ethylene chloride, for application by spraying.
    Type: Grant
    Filed: September 25, 1987
    Date of Patent: November 15, 1988
    Inventors: Jean London, James O. Gibson
  • Patent number: 4627418
    Abstract: An apparatus and process are disclosed for utilizing solar radiation and the energy contained therein for the carbothermic reduction of a metal oxide to a metal carbide. The apparatus comprises a reflective surface which collects and focuses solar radiation onto a focal mirror which consequentially reflects and focuses the solar light rays into a reaction chamber through a Fresnel lens and a transparent window provided on the chamber. The solar light rays are focused by the reflective surface focal mirror and Fresnel lens such that the energy absorbed by reactants in the reaction chamber is sufficient for the carbothermic reduction of the metal oxide.
    Type: Grant
    Filed: January 16, 1984
    Date of Patent: December 9, 1986
    Assignee: Geruldine Gibson
    Inventors: James O. Gibson, Mark G. Gibson
  • Patent number: 4472367
    Abstract: An apparatus and process are disclosed for utilizing solar radiation and the energy contained therein for the carbothermic reduction of a metal oxide to a metal carbide. The apparatus comprises a reflective surface which collects and focuses solar radiation onto a focal mirror which consequentially reflects and focuses the solar light rays into a reaction chamber through a Fresnel lens and a transparent window provided on the chamber. The solar light rays are focused by the reflective surface focal mirror and Fresnel lens such that the energy absorbed by reactants in the reaction chamber is sufficient for the carbothermic reduction of the metal oxide.
    Type: Grant
    Filed: September 8, 1980
    Date of Patent: September 18, 1984
    Assignee: Geruldine Gibson
    Inventors: James O. Gibson, Mark G. Gibson
  • Patent number: 4278729
    Abstract: Carbon fiber reinforced tantalum carbide composites are produced by vacuum infiltration of omni-weave carbon, e.g. three dimensional graphite, yarn preforms with an aqueous saturated solution containing tantalum fluoride and sucrose. Anhydrous ammonia is added under pressure, forming ammonium fluoride, which is removed by vacuum sublimation by application of heat. The resulting preform containing tantalum pentoxide and partially pyrolyzed sucrose is heated at high temperature and reduced pressure to decompose the sucrose to yield active carbon which reacts with the tantalum pentoxide to yield tantalum carbide and carbon monoxide.
    Type: Grant
    Filed: November 19, 1979
    Date of Patent: July 14, 1981
    Inventors: James O. Gibson, Mark G. Gibson
  • Patent number: 4196230
    Abstract: Carbon fiber reinforced tantalum carbide composites are produced by vacuum infiltration of omni-weave carbon, e.g. three dimensional graphite, yarn preforms with an aqueous saturated solution containing tantalum fluoride and sucrose. Anhydrous ammonia is added under pressure, forming ammonium fluoride, which is removed by vacuum sublimation by application of heat. The resulting preform containing tantalum pentoxide and partially pyrolyzed sucrose is heated at high temperature and reduced pressure to decompose the sucrose to yield active carbon which reacts with the tantalum pentoxide to yield tantalum carbide and carbon monoxide.
    Type: Grant
    Filed: September 15, 1978
    Date of Patent: April 1, 1980
    Inventors: James O. Gibson, Mark G. Gibson