Patents Represented by Attorney Neil F. Martin
  • Patent number: 4647873
    Abstract: An apparatus and method for generating an output signal having portions thereof being linearly swept in frequency. A controller, responsive to external signals, generates a series of control signals. An oscillator, responsive to each one of the control signals, produces an output signal. The output signal includes a series of output waveforms each linearly swept in frequency and corresponding to a respective one of the control signals. A first servo, responsive to each one of the output waveforms, produces a series of first correction signals each dependent upon the linearity error in a corresponding one of the output waveforms. The first correction signals modify a corresponding control signal as applied to the oscillator so as to correct linearity errors occurring in a corresponding one of the output waveforms. A second servo, responsive to each one of the first correction signals, produces a series of second correction signals each dependent upon the correlations in the first correction signals.
    Type: Grant
    Filed: July 19, 1985
    Date of Patent: March 3, 1987
    Assignee: General Dynamics, Pomona Division
    Inventors: Frederick L. Beckner, Garry N. Hulderman, Darrell K. Ingram
  • Patent number: 4647778
    Abstract: A cooling apparatus for an infrared up-convertor incorporates a transparent heat sink in a conductive heat exchange relationship with a surface of the up-convertor and a Joule-Thomson effect cryostat located outside of the incoming and emitted image paths for cooling the heat sink. In this manner, the cooling apparatus does not obscure the path of the image to or from the up-convertor.
    Type: Grant
    Filed: January 23, 1985
    Date of Patent: March 3, 1987
    Assignee: General Dynamics, Pomona Division
    Inventors: Mark L. Kline, Oakley G. Ross
  • Patent number: 4623564
    Abstract: A rigid packaging material having a coating of heat-sealable, anti-static plastic. A fiberboard sheet substrate is coated with a lamina of polyethylene made electrostatic-free by the addition of an organic anti-static compound. When skin-packaged with a film of heat sealable, anti-static plastic material, a static-sensitive item is completely enclosed by a static-free barrier package.
    Type: Grant
    Filed: December 5, 1985
    Date of Patent: November 18, 1986
    Assignee: General Dynamics, Pomona Division
    Inventors: Stuart G. Long, Michael J. Maciocia
  • Patent number: 4620293
    Abstract: An optical computing system is provided for performing a linear multiplication operation involving a matrix with bipolar values. A plurality of beams representing the values of a N.times.1 column matrix Q illuminate an optical mask having elements disposed in a two-dimensional (M+1).times.N array. Each element of the first M rows of the mask represents the offset of the value of a corresponding element in a known M.times.N matrix by a scalar constant c. Each element of row M+1 of the mask represents the value c. An array of photodetectors collects the light passing through the mask, with the light from each row of elements detected by a respective photodetector. The outputs of the first M photodetectors represent the product of Q and M after M has been offset by c. The output of photodetector M+1 represents the scalar value produced by the multiplication of Q and a row matrix represented by row M+1 of the mask matrix.
    Type: Grant
    Filed: December 23, 1983
    Date of Patent: October 28, 1986
    Assignee: General Dynamics, Pomona Division
    Inventors: Richard S. Schlunt, Hans-Peter Schmid, Donald R. Fetterly
  • Patent number: 4604570
    Abstract: A ballistic comparative ohmmeter for use in testing the resistance between different selected pairs of a plurality of terminals in a test circuit in comparison to the resistance between corresponding pairs of terminals in a reference circuit. the ohmmeter is particularly useful for making resistance tests in circuits included in assembled products. The ohmmeter makes comparative resistance tests during a transient response period following application of the current to the selected pair of terminals as well as under steady state conditions. Solid state stepping switches that are sequentially stepped by pulse counters are utilized to sequentially connect different combinations of terminals in the test circuit and the reference circuit. Protection circuits limit the voltages applied across the test circuit and master circuit terminals. Indicator panels immediately provide a steady state indication of the pair of terminals in the test circuit at which a fault is detected.
    Type: Grant
    Filed: May 29, 1985
    Date of Patent: August 5, 1986
    Assignee: General Dynamics, Pomona Division
    Inventor: Richard W. Thorpe
  • Patent number: 4603942
    Abstract: A flexible waveguide for transmitting waves from a sensor mounted on a gimbal includes a cable comprising an outer flexible sheath and a plurality of flexible polytetrafluoroethylene fibers bundled within the sheath and including a termination flange coupled to at least one end thereof with the flange including a wedge-shaped plug and a tapered cavity engaging the end of the cable.
    Type: Grant
    Filed: October 11, 1983
    Date of Patent: August 5, 1986
    Assignee: General Dynamics, Pomona Division
    Inventors: Yu-Wen Chang, Phillip T. Kan, Oakley G. Ross
  • Patent number: 4602809
    Abstract: A separable electrical isolator for coupling two pieces of conductive tubing carrying high pressure cryogenic gas includes a gas-impervious dielectric spacer with a bore in which the pieces of tubing are sealed axially-aligned in fluid communication with an electrically-nonconductive gap between them. A pair of complementary coupling members are rigidly attached to the pieces of tubing to define outwardly-extending annular flanges that are each sealed about the periphery of a corresponding one of the pieces in a position slightly set back from an end of the piece. Each flange has an annular rib protruding from it toward the end of the piece. The coupling members are separably and nonconductively interconnected with the annular ribs applying compressive force to the spacer to thereby effect the seal.
    Type: Grant
    Filed: November 21, 1984
    Date of Patent: July 29, 1986
    Assignee: General Dynamics, Pomona Division
    Inventors: Oakley G. Ross, Mark L. Kline, Johnny R. Vieyra
  • Patent number: 4601493
    Abstract: A coupler for electrically-isolating two conductive sections of fluid-passing line includes two nonconductively-interconnected pieces of tubing for insertion in the line. The pieces of tubing each have a divergently-flared end, and the flared ends are nonconductively-interconnected within two dielectric wafers. Each wafer has a tapered hole extending through it that matches the flared ends and enlarges to a face on the wafer. The flared ends are each bonded within a separate one of the tapered holes in a position recessed from the face with the flare of the end paralleling the taper of the hole, and the faces are bonded together with the larger ends of the tapered holes aligned and the flared ends sealed in fluid communication with an electrically-nonconductive gap between them.
    Type: Grant
    Filed: April 13, 1984
    Date of Patent: July 22, 1986
    Assignee: General Dynamics, Pomona Division
    Inventors: Oakley G. Ross, Mark L. Kline, Larry D. Wedertz
  • Patent number: 4600218
    Abstract: A separable electrical isolator for coupling two pieces of conductive tubing carrying high pressure cryogenic gas includes a gas-impervious dielectric spacer with a pair of opposing surfaces and a bore extending therebetween in which the pieces of tubing are sealed axially-aligned in fluid communication with an electrically-nonconductive gap between them. A pair of complementary coupling members are rigidly attached to the pieces of tubing to define outwardly-extending annular surfaces that are each sealed about the periphery of a corresponding piece in a position slightly set back from and facing an end of the piece. The coupling members are separably and nonconductively interconnected with the annular surfaces facing the spacer surfaces and O-ring seals in between to apply compressive force to the spacer and seals and thereby effect the seal.
    Type: Grant
    Filed: November 21, 1984
    Date of Patent: July 15, 1986
    Assignee: General Dynamics, Pomona Division
    Inventors: Oakley G. Ross, Mark L. Kline, Larry D. Wedertz
  • Patent number: 4598884
    Abstract: A gimbal-less infrared (IR) target sensor for mounting in an IR transmissive nose cone of a guided missile comprises a fixed, concave, primary mirror mounted coaxially in the base of the nose cone; a fixed, convex, secondary mirror mounted at the focus of the primary mirror; and a plurality of IR sensing units having IR transmissive elements located around the periphery of the primary mirror. A shaped-charge is located aft of the primary mirror. The IR-transmissive elements incorporate IR-conductive fiber optics to transmit the IR signal to detectors aft of the shaped-charge for detection, processing, and missile guidance.
    Type: Grant
    Filed: November 28, 1984
    Date of Patent: July 8, 1986
    Assignee: General Dynamics Pomona Division
    Inventor: Spencer J. Speer
  • Patent number: 4594945
    Abstract: A thin frangible cork barrier conforming to the contour of the burning surface of individual solid propellant grains in a multiple grain rocket motor prevents premature ignition of the protected grain by the heat of combustion of previously ignited adjacent grains and is expelled through the rocket motor nozzle upon ignition of the protected grain. In a second embodiment, the thermal protection afforded by the frangible cork barrier is augmented by bonding to a thermally-protective elastomer layer which is in turn bonded to the propellant grain burning surface. By virtue of the composition and structure of the embodiments, thermal protection is afforded. Upon ignition of a protected grain the thermal barrier breaks up so as to pass readily through the throat of a small motor nozzle.
    Type: Grant
    Filed: November 28, 1984
    Date of Patent: June 17, 1986
    Assignee: General Dynamics, Pomona Division
    Inventor: George Alexandris
  • Patent number: 4590741
    Abstract: A laminated packaging film useful for skin-packaging electrostatic-sensitive items and protecting the items from electrostatic damage during packaging and while the items are vacuumed, contained, and removed from packages. The film includes a pair of sheets of highly resistive, heat-sealable plastic between which is sandwiched a sheet of conductive, heat-sealable plastic. The film resists the buildup of static charges while the item is being packaged and forms a protective Faraday cage while the item is contained in the package.
    Type: Grant
    Filed: July 22, 1985
    Date of Patent: May 27, 1986
    Assignee: General Dynamics Pomona Division
    Inventors: Stuart G. Long, Michael J. Maciocia
  • Patent number: 4586680
    Abstract: A wing support structure for a self-erecting collapsible wing includes a telescoping strut assembly including a leading strut and a trailing strut each pinned at an inner end to fixed pins on a base support structure and pinned to a common pivot pin at the outer end and each strut being telescoping for retraction to a colinear position and spring biased to an outward fully deployed position. Each strut includes inner and outer tubular strut members in which is confined a compression spring with the inner and outer members including an antirotation lock and an anticollapse lock.
    Type: Grant
    Filed: February 10, 1982
    Date of Patent: May 6, 1986
    Assignee: General Dynamics Pomona Division
    Inventors: Anthony DiTommaso, Ronald T. Inglis, Richard C. Worley, Ramon J. Renda
  • Patent number: 4586681
    Abstract: An erectable wing structure for a supersonic airframe that is stowable within the body of the airframe includes a housing defining an elongated cavity in which is mounted a wing supporting strut assembly having an elongated leading edge strut pivoted at one end within the stowable cavity and including a trailing strut that is foldable and pivotally connected at one end to the cavity structure and at the other end to the outer end of the leading edge strut and including a single layer of fabric stretched between the strut and clamped between the strut structure made up of separable, mirror image, strut links.
    Type: Grant
    Filed: June 27, 1983
    Date of Patent: May 6, 1986
    Assignee: General Dynamics Pomona Division
    Inventors: Larry D. Wedertz, David L. Leslie, John A. Karish
  • Patent number: 4584539
    Abstract: A multi-channel frequency synthesizer, including a crystal oscillator circuit that may be selectively operated to provide a reference signal at a selected reference frequency that is one of a given plural number of frequencies; an IF generator for processing the reference signal to provide an IF signal at a selected intermediate frequency that is one of a given plural number of submultiples of the selected reference frequency; a comb generator for processing the reference signal to provide a comb of signals separated from each other by the selected reference frequency; and a phase-locked loop.
    Type: Grant
    Filed: November 28, 1984
    Date of Patent: April 22, 1986
    Assignee: General Dynamics Pomona Division
    Inventor: John E. Stankey
  • Patent number: 4581977
    Abstract: An apparatus and method for establishing the alignment of heat seeking missiles with the longitudinal axis of a launch pod within which the missiles are contained is disclosed. A housing containing a heat source and collimating optics provides a simulated distant infrared target for the missiles. A tapered probe rigidly attachable to the housing fits securely into a central alignment socket in the launcher pod. The probe is accurately offset from the center line of the alignment socket by the housing to establish the optical axis of the simulated target parallel to the axis of the launcher pod, and in front of the stored missiles. The position of the missile within the launch pod is adjustable to maximize the target signal strength received by the missile from the simulated target to achieve missile alignment with the axis of the launcher pod.
    Type: Grant
    Filed: May 2, 1983
    Date of Patent: April 15, 1986
    Assignee: General Dynamics, Pomona Division
    Inventors: Oakley G. Ross, Larry D. Wedertz, Michael G. Greiner
  • Patent number: 4568044
    Abstract: A self-erecting collapsible wing for an airframe includes a telescoping strut assembly including a leading strut and a trailing strut each pivoted at an inner end to fixed pins on a base support structure of a wing housing within a slot in the airframe for retraction to a colinear position within the housing and spring biased to an outward fully deployed position. A releasable cover conforming to the curvature of the airframe is normally latched in position over the slot when the wing is in the collapsed position within the wing housing and is jettisoned to permit automatic self-erection of the wing.
    Type: Grant
    Filed: August 12, 1983
    Date of Patent: February 4, 1986
    Assignee: General Dynamics, Pomona Division
    Inventors: Anthony DiTommaso, Ronald T. Inglis, Richard C. Worley
  • Patent number: 4568562
    Abstract: A method for electroless overplating of a conductive metal on printed wiring circuitry components mounted upon a plastic substrate which eliminates deposit metal overgrowth upon the plastic substrate and plastic bonding materials. The substrate and printed wiring are treated by exposure to a tetrafluoromethane plasma environment to chemically passivate, or neutralize, the plastic or adhesive substrate surface areas prior to electroless plating of the printed circuitry elements, thus preventing the establishment of catalyzing ions on the plastic or adhesive surfaces and subsequent lay down of the deposited metal thereon.
    Type: Grant
    Filed: November 28, 1984
    Date of Patent: February 4, 1986
    Assignee: General Dynamics, Pomona Division
    Inventor: Eugene Phillips
  • Patent number: 4567782
    Abstract: A compound parallelogram four-bar linkage is provided wherein a first primary link is connected to a second primary link through connector links of substantially the same length and the pivotal angles of the first primary link and second primary link are maintained at substantially ninety degrees as movement is transferred from one primary link to the other so that the resonant frequency of the linkage does not vary and the linkage stiffness is independent of the angle of rotation.
    Type: Grant
    Filed: August 30, 1984
    Date of Patent: February 4, 1986
    Assignee: General Dynamics Pomona Division
    Inventors: John M. Speicher, Allan A. Voigt
  • Patent number: 4558918
    Abstract: A cable shield to connector back shell termination device includes a back shell of a multi-pin cable connector, a plurality of metallic tubes adapted to receive individually the end of a shielded cable such that substantially full circumferential conductive contact is maintained between each cable shield and a tube, and a cluster of such tubes conductively bonded together and shaped to fit the back shell for conductive bonding to the back shell. A second embodiment employs a conductive sleeve for conductive mounting on the cable shield. Ridges or fins extending generally lengthwise on the sleeve frictionally, conductively contact the metal tubes. In this manner an uninterrupted conductive surface is maintained at the connector. The connector enclosure thus provides a shield against the intrusion of electromagnetic energy in the environment in which the electrical or electronic wiring and circuits must operate.
    Type: Grant
    Filed: November 28, 1984
    Date of Patent: December 17, 1985
    Assignee: General Dynamics Pomona Division
    Inventor: Marvin W. Shores