Patents Represented by Attorney S. C. Durant
  • Patent number: 4638320
    Abstract: A two-dimensional, long baseline (D) direction finding interferometer (12) is provided for obtaining unambiguous spatial position of an object. The interferometer comprises four antenna receiving means, (A1, A2, A3, A4) which are arranged in a two-dimensional, planar fashion. Three of the antenna means (A1, A2, A3) are positioned on two orthogonal axes (D, D.sub.2). The remaining antenna (A4) means is positioned on a third axis (D.sup.1) which is arranged asymmetrically and nonorthogonally to the orthogonal axes, whereby the unambiguous spatial position of the object is determined.
    Type: Grant
    Filed: November 5, 1982
    Date of Patent: January 20, 1987
    Assignee: Hughes Aircraft Company
    Inventors: Dennis J. Eggert, Charles E. Hendrix, Barnet Krinsky
  • Patent number: 4623951
    Abstract: Conductive coating (20) is a thorough mixture of 0.03 parts per weight of carbon black together with 0.003 to 0.01 parts per weight of wetting agent and 20 parts of solvent, and further mixing in by low shearing mixing 1/2 to 1 part per weight of thermosetting resin. This is then sprayed into place on the substrate and thermoset. In this particular case, the substrate is exterior face sheet (12) of honeycomb structure (10) which may serve as part of a spacecraft, to electrically conduct away surface charges.
    Type: Grant
    Filed: August 13, 1984
    Date of Patent: November 18, 1986
    Assignee: Hughes Aircraft Company
    Inventors: Preston S. DuPont, Robert E. Ritter, John P. Stafford
  • Patent number: 4600169
    Abstract: A spacecraft is mounted in a cradle secured in the space shuttle by means of a suspension system including four cradle attachment members secured to the upper longeron bridge of the shuttle, in which provision is made for movably mounting one attachment member on the cradle to provide a component of movement substantially normal to the adjacent longeron bridge to accommodate misalignment between the longeron bridges and the attachment members without the need for removing the spacecraft and cradle from the shuttle.
    Type: Grant
    Filed: December 23, 1983
    Date of Patent: July 15, 1986
    Assignee: Hughes Aircraft Company
    Inventors: William G. Koster, Allan B. Byrne
  • Patent number: 4560974
    Abstract: Operating at real-time data rates, the disclosed hardware network generates a signal which closely approximates the Mth-largest of a set of R input data signals. The operational basis of this network is a comparison (121-127) between the input data (101-107) and a monotonically-scanning reference function (110). At that point (140, 150, 160) when the lower (R-M+1) of the inputs have been equaled by an increasing reference, the reference has become the same as the Mth-largest and is used (119b, 165, 170, 175) as the filter output. Analogous operation is achieved with a decreasing reference.When the number R of inputs is odd and M is made equal to ((R+1)/2), the network becomes a real-time median filter.
    Type: Grant
    Filed: January 30, 1984
    Date of Patent: December 24, 1985
    Assignee: Hughes Aircraft Company
    Inventors: Guy B. Coleman, James W. Henderson, Jacob M. Sacks
  • Patent number: 4544237
    Abstract: The invention provides a two-channel liquid crystal light valve image projection system with prepolarization using an oil coupled optical arrangement. A prepolarizing beam splitter is mounted the container in optical alignment with a first surface for splitting and prepolarizing light from a source into first and second beams having first and second polarization states respectively. First and second dichroic separators are mounted within the container for extracting light of a first color from the first beam and light of a second color from the second beam respectively. The separator outputs are recombined by the prepolarizing prism into a single beam which is directed to a second polarizing beam splitter mounted within the container. The second beam splitter splits the single beam and directs light of the first and second polarizations through the second and third apertures, respectively.
    Type: Grant
    Filed: December 28, 1981
    Date of Patent: October 1, 1985
    Assignee: Hughes Aircraft Company
    Inventor: Ralph J. Gagnon
  • Patent number: 4540969
    Abstract: The body of the disclosed fuse includes connective portions having surface-metalization to which corresponding connective portions of the fusible element are respectively bonded.A metalization-conducive ceramic may be more-specifically utilized for the fuse body, while those portions of the body which interface with the fusible element may additionally be contoured so as to lessen the severity of element-severance forces otherwise experienced.When the fuse's connective portions yet-more-specifically comprise the opposite ends of a fuse body which is elongated, end caps may be electrically joined to the surface-metalized fuse ends. An enhanced degree of mechanical stability may also be achieved by further providing stabilizing geometrical expedients for the fuse/cap interface.
    Type: Grant
    Filed: August 23, 1983
    Date of Patent: September 10, 1985
    Assignee: Hughes Aircraft Company
    Inventor: Joseph Sugar